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CARLSON, GASKEY & OLDS/PRATT & WHITNEY
BIRMINGHAM, MI US
1. 20110044795 TURBINE VANE PLATFORM LEADING EDGE COOLING HOLES 02-24-20112. 20110040719 FAILURE DETECTION SYSTEM RISK REDUCTION ASSESSMENT 02-17-2011
3. 20110030456 NON-DESTRUCTIVE INSPECTION METHOD FOR METALLIC ALLOYS 02-10-2011
4. 20110020105 NACELLE FLOW ASSEMBLY - nacelle assembly for a turbine engine has a cowl for a turbine engine 01-27-2011
5. 20110016880 RETAINER FOR SUSPENDED THERMAL PROTECTION ELEMENTS IN A GAS TURBINE ENGINE 01-27-2011
6. 20110016879 LOW PROFILE ATTACHMENT HANGER SYSTEM FOR A COOLING LINER WITHIN A GAS TURBINE ENGINE SWIVEL EXHAUST DUCT 01-27-2011
7. 20110014045 FAN EXHAUST NOZZLE FOR TURBOFAN ENGINE - The cross sectional flow area of a fan discharge nozzle on one side of a central plane of an associated gas 01-20-2011
8. 20110000217 MANAGING SPOOL BEARING LOAD USING VARIABLE AREA FLOW NOZZLE 01-06-2011
9. 20100326046 VALVE SYSTEM FOR A GAS TURBINE ENGINE - valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary 12-30-2010
10. 20100325887 REPAIR METHOD FOR GAS TURBINE ENGINE COMPONENTS 12-30-2010
11. 20100323596 NOTCHED GRIND WHEEL AND METHOD TO MANUFACTURE A ROTOR BLADE RETENTION SLOT 12-23-2010
12. 20100320061 TRACK WITH OVERLAPPING LINKS FOR DRY COAL EXTRUSION PUMPS 12-23-2010
13. 20100313639 GAS TURBINE ENGINE DEBRIS MONITORING ARRANGEMENT 12-16-2010
14. 20100310358 INNER DIAMETER SHROUD ASSEMBLY FOR VARIABLE INLET GUIDE VANE STRUCTURE IN A GAS TURBINE ENGINE 12-09-2010
15. 20100307389 REACTOR SYSTEM AND SOLID FUEL COMPOSITE THEREFOR 12-09-2010
16. 20100307367 GUIDED PROJECTILE - non-propulsive projectile and method of maneuvering the non-propulsive projectile 12-09-2010
17. 20100301062 SINGLE BI-TEMPERATURE THERMAL STORAGE TANK FOR APPLICATION IN SOLAR THERMAL PLANT 12-02-2010
18. 20100294128 FUEL DEOXYGENATOR WITH POROUS SUPPORT PLATE 11-25-2010
19. 20100292905 SYSTEM AND METHOD OF ESTIMATING GAS TURBINE ENGINE PERFORMANCE 11-18-2010
20. 20100288874 ENGINE MOUNT BEARING SLEEVE REPAIR - Bearing bores for engine mount components must be periodically repaired 11-18-2010
21. 20100288034 SYSTEM AND METHOD OF ASSESSING THERMAL ENERGY LEVELS OF A GAS TURBINE ENGINE COMPONENT 11-18-2010
22. 20100287907 SYSTEM AND METHOD OF ESTIMATING A GAS TURBINE ENGINE SURGE MARGIN 11-18-2010
23. 20100286959 DEGRADED ACTUATOR DETECTION - actuator control system is disclosed that includes an actuator continuously movable between multiple positions 11-11-2010
24. 20100284816 AIRFOIL ATTACHMENT - rotor blade for a gas turbine engine includes an airfoil that extends in span between a tip and a root opposite from the tip 11-11-2010
25. 20100284793 METHOD OF ELECTRICAL DISCHARGE SURFACE REPAIR OF A VARIABLE VANE TRUNNION 11-11-2010
26. 20100269512 GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE 10-28-2010
27. 20100269486 GAS TURBINE ENGINE HAVING SLIM-LINE NACELLE 10-28-2010
28. 20100269485 INTEGRATED VARIABLE AREA NOZZLE AND THRUST REVERSING MECHANISM 10-28-2010
29. 20100266442 BURN-RESISTANT AND HIGH TENSILE STRENGTH METAL ALLOYS 10-21-2010
30. 20100266401 TURBINE ENGINE ROTATING CAVITY ANTI-VORTEX CASCADE 10-21-2010
31. 20100266391 MECHANICAL ATTACHMENT OF CERAMIC OR METALLIC FOAM MATERIALS 10-21-2010
32. 20100266387 TURBINE ENGINE ROTATING CAVITY ANTI-VORTEX CASCADE 10-21-2010
33. 20100266385 Separation resistant aerodynamic article 10-21-2010
34. 20100265026 PASSIVE ELECTRICAL COMPONENTS WITH INORGANIC DIELECTRIC COATING LAYER 10-21-2010
35. 20100264601 SHROUDED FACE SEAL AND COMPONENTS THEREOF 10-21-2010
36. 20100263497 BOLT HOLDER TOOL - tool includes a base ring which defines a multiple of bores each of the multiple of bores sized to receive one of a multiple of 10-21-2010
37. 20100257841 VARIABLE AREA FAN NOZZLE AND THRUST REVERSER 10-14-2010
38. 20100257839 Hydrocarbon-fueled rocket engine with endothermic fuel cooling 10-14-2010
39. 20100254821 INTERMEDIATE-MANUFACTURED COMPOSITE AIRFOIL AND METHODS FOR MANUFACTURING 10-07-2010
40. 20100254797 ENDWALL WITH LEADING-EDGE HUMP - example airfoil assembly includes a base having an airfoil projecting radially therefrom 10-07-2010
41. 20100247952 CONTROLLED OXIDATION OF BOND COAT - method of processing an article includes heating the article in an atmosphere substantially free of oxygen to an 09-30-2010
42. 20100247809 ELECTRON BEAM VAPOR DEPOSITION APPARATUS FOR DEPOSITING MULTI-LAYER COATING 09-30-2010
43. 20100247306 GAS TURBINE ENGINE WITH 2.5 BLEED DUCT CORE CASE SECTION 09-30-2010
44. 20100247293 VARIABLE AREA TURBINE VANE ARRANGEMENT - ring vane nozzle for a gas turbine engine according to an exemplary aspect of the present disclosure includes a 09-30-2010
45. 20100247291 GAS TURBINE ENGINE ARTICLE HAVING COLUMNAR MICROSTRUCTURE 09-30-2010
46. 20100247284 AIRFLOW INFLUENCING AIRFOIL FEATURE ARRAY 09-30-2010
47. 20100242988 METHOD AND APPARATUS FOR CLEANING A COMPONENT USING MICROWAVE RADIATION 09-30-2010
48. 20100242841 ELECTRON BEAM VAPOR DEPOSITION APPARATUS AND METHOD OF COATING 09-30-2010
49. 20100242736 PRESSURE-BASED DISSOLVED GAS REMOVAL SYSTEM 09-30-2010
50. 20100242496 GAS TURBINE ENGINE WITH STACKED ACCESSORY COMPONENTS 09-30-2010
51. 20100239842 COMPOSITE ARTICLE AND FABRICATION METHOD 09-23-2010
52. 20100239424 SPLIT DISK ASSEMBLY FOR A GAS TURBINE ENGINE 09-23-2010
53. 20100238967 METHOD OF PRODUCING A FINE GRAIN CASTING 09-23-2010
54. 20100236666 SUPERALLOY POWDER, METHOD OF PROCESSING, AND ARTICLE FABRICATED THEREFROM 09-23-2010
55. 20100236332 FLUID PRESSURE OPERATED FIXTURE - fixture includes a housing assembly defined along an axis 09-23-2010
56. 20100236216 TURBOFAN ENGINE WITH VARIABLE AREA FAN NOZZLE AND LOW SPOOL GENERATOR FOR EMERGENCY POWER GENERATION AND METHOD FOR PROVIDING EMERGENCY POWER 09-23-2010
57. 20100232979 BLADE TIP COOLING GROOVE - example turbine blade includes a blade having an airfoil profile extending radially toward a blade tip 09-16-2010
58. 20100232943 BURIED CASING TREATMENT STRIP FOR A GAS TURBINE ENGINE 09-16-2010
59. 20100232929 COOLING ARRANGEMENT FOR A TURBINE ENGINE COMPONENT 09-16-2010
60. 20100226760 TURBINE ENGINE SEALING ARRANGEMENT - example turbine engine sealing arrangement includes a blade array rotatable about an axis 09-09-2010
61. 20100223788 METHOD OF MAINTAINING GAS TURBINE ENGINE COMPONENTS 09-09-2010
62. 20100221102 CORE REFLEX NOZZLE FOR TURBOFAN ENGINE - turbofan engine is provided that includes a core nacelle at least partially surrounded by a fan nacelle 09-02-2010
63. 20100221083 CONTROL OF WHITE-ETCHED LAYER DURING MACHINING 09-02-2010
64. 20100218921 Metal foam heat exchanger - heat exchanger includes one or more passages and one or more metal foam sections adjacent the passage to promote an exchange 09-02-2010
65. 20100218657 CONTROL OF WHITE-ETCHED LAYER DURING MACHINING 09-02-2010
66. 20100215479 GAS TURBINE ENGINE INLET WITH NOISE REDUCTION FEATURES 08-26-2010
67. 20100205975 INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL 08-19-2010
68. 20100196193 NICKEL BRAZE ALLOY COMPOSITION - alloy composition includes a blend of a first alloy and a second alloy the first alloy having a first composition 08-05-2010
69. 20100189929 COATING DEVICE AND DEPOSITION APPARATUS - coating device for use with an electron beam vapor deposition apparatus includes a crucible portion and a 07-29-2010
70. 20100189555 METHOD AND ASSEMBLY FOR GAS TURBINE ENGINE AIRFOILS WITH PROTECTIVE COATING 07-29-2010
71. 20100186419 HEAT TRANSFER AUGMENTATION IN A COMPACT HEAT EXCHANGER PEDESTAL ARRAY 07-29-2010
72. 20100180571 MODULATING FLOW THROUGH GAS TURBINE ENGINE COOLING SYSTEM 07-22-2010
73. 20100178165 WELDING REPAIR METHOD FOR FULL HOOP STRUCTURES 07-15-2010
74. 20100176185 WELDING REPAIR METHOD FOR FULL HOOP STRUCTURES 07-15-2010
75. 20100174392 OPTIMAL DIMENSIONAL AND MECHANICAL PROPERTIES OF LASER SINTERED HARDWARE BY THERMAL ANALYSIS AND PARAMETER OPTIMIZATION 07-08-2010
76. 20100170220 TURBOFAN ENGINE HAVING INNER FIXED STRUCTURE INCLUDING DUCTED PASSAGES 07-08-2010
77. 20100166543 Inlet Guide Vanes and Gas Turbine Engine Systems Involving Such Vanes 07-01-2010
78. 20100164669 PASSIVE ELECTRICAL COMPONENTS WITH INORGANIC DIELECTRIC COATING LAYER 07-01-2010
79. 20100162683 TURBOFAN ENGINE - is provided that includes a fan nacelle surrounding a core nacelle 07-01-2010
80. 20100161287 MEASUREMENT DATA MANAGEMENT SYSTEM - system and process for managing measurement data and generating production and engineering drawings from 06-24-2010
81. 20100160105 OIL BAFFLE FOR GAS TURBINE FAN DRIVE GEAR SYSTEM 06-24-2010
82. 20100155907 SEMICONDUCTOR DEVICE HAVING AN INORGANIC COATING LAYER APPLIED OVER A JUNCTION TERMINATION EXTENSION 06-24-2010
83. 20100154217 OIL BAFFLE FOR GAS TURBINE FAN DRIVE GEAR SYSTEM 06-24-2010
84. 20100150733 AIRFOIL WITH WRAPPED LEADING EDGE COOLING PASSAGE 06-17-2010
85. 20100150729 GAS TURBINE ENGINE AIRFOIL - rotor blade for a gas turbine engine includes an airfoil that extends in span between a root and a tip region 06-17-2010
86. 20100143132 TURBINE BLADE WITH REVERSE COOLING AIR FILM HOLE DIRECTION 06-10-2010
87. 20100139285 THRUST VECTORABLE FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE 06-10-2010
88. 20100139243 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE, NACELLE ASSEMBLY AND METHOD OF VARYING AREA OF A FAN NOZZLE 06-10-2010
89. 20100139240 BLADDER TYPE VARIABLE AREA FAN NOZZLE - variable fan nozzle for use in a gas turbine engine includes a nozzle section such as an inflatable bladder 06-10-2010
90. 20100136296 Densification of coating using laser peening 06-03-2010
91. 20100136258 METHOD FOR IMPROVED CERAMIC COATING - method of manufacturing an article having a ceramic topcoat includes the steps of forming the ceramic topcoat on 06-03-2010
92. 20100126635 MACHINED COMPONENT MANUFACTURING METHOD FOR ENHANCED LOW CYCLE FATIGUE LIFE 05-27-2010
93. 20100122519 ULTRA-LOW SULFUR FUEL AND METHOD FOR REDUCED CONTRAIL FORMATION 05-20-2010
94. 20100119419 TWO PHASE INJECTOR FOR FLUIDIZED BED REACTOR 05-13-2010
95. 20100115914 TRANSLATING CORE COWL HAVING AERODYNAMIC FLAP SECTIONS 05-13-2010
96. 20100113311 Method for quantitatively determining the dye content in dyed oils 05-06-2010
97. 20100112239 METHODS FOR REPAIRING GAS TURBINE ENGINE COMPONENTS 05-06-2010
98. 20100106462 Systems and Methods for Diagnosing Gas Turbine Engine Faults 04-29-2010
99. 20100104773 METHOD FOR USE IN A COATING PROCESS - includes depositing a ceramic coating on a bond coat that is disposed on a substrate 04-29-2010
100. 20100104766 METHOD FOR USE WITH A COATING PROCESS - includes depositing a ceramic coating on a substrate within a coating chamber 04-29-2010
101. 20100101208 Systems and Methods Involving Reduced Thermo-Acoustic Coupling of Gas Turbine Engine Augmentors 04-29-2010
102. 20100098547 TURBINE BLADE INCLUDING MISTAKE PROOF FEATURE 04-22-2010
103. 20100098526 AIRFOIL WITH COOLING PASSAGE PROVIDING VARIABLE HEAT TRANSFER RATE 04-22-2010
104. 20100097132 Systems and Methods for Filtering Signals Corresponding to Sensed Parameters 04-22-2010
105. 20100095650 TRANSLATING CORE COWL FOR A GAS TURBINE ENGINE 04-22-2010
106. 20100092382 GAS GENERATOR AND METHOD THEREFOR - gas generator includes a high pressure gas-generation system that is capable of generating a product gas stream at a 04-15-2010
107. 20100092381 REACTOR SYSTEM AND METHOD THEREFORE - reactor system includes a fluidized bed reactor with a fluidized zone having sorbent particles and catalyst 04-15-2010
108. 20100092379 APPARATUS AND METHOD FOR USE IN CALCINATION 04-15-2010
109. 20100089065 FUEL DELIVERY SYSTEM FOR A TURBINE ENGINE 04-15-2010
110. 20100089030 CONTROLLING THE AERODYNAMIC DRAG OF A GAS TURBINE ENGINE DURING A SHUTDOWN STATE 04-15-2010
111. 20100089028 CORRUGATED CORE COWL FOR A GAS TURBINE ENGINE 04-15-2010
112. 20100086403 LUBRICATION OF WINDMILLING JOURNAL BEARINGS 04-08-2010
113. 20100084106 PROCESS FOR CASTING COLUMNAR GRAIN AIRFOIL WITH PREFERENTIAL PRIMARY ORIENTATION 04-08-2010
114. 20100080711 TURBINE BLADE WITH IMPROVED DURABILITY TIP CAP 04-01-2010
115. 20100077724 CORE COWL AIRFOIL FOR A GAS TURBINE ENGINE 04-01-2010
116. 20100075171 NANO-GRAINED ALUMINUM ALLOY BELLOWS - bellows includes a flexible section including a series of convolutions extending between a first end and a second 03-25-2010
117. 20100074739 PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL 03-25-2010
118. 20100071343 COMPACT CYCLONE COMBUSTION TORCH IGNITER 03-25-2010
119. 20100068417 ELECTRON BEAM VAPOR DEPOSITION APPARATUS AND METHOD 03-18-2010
120. 20100068051 INTEGRATED INLET FAN CASE - fan section of a gas turbine engine includes nacelle inlet and a fan containment case that are integrally formed together as 03-18-2010
121. 20100068039 TURBOFAN ENGINE WITH VARIABLE BYPASS NOZZLE EXIT AREA AND METHOD OF OPERATION 03-18-2010
122. 20100065308 CONDUCTIVE EMISSIONS PROTECTION - According to one non-limiting embodiment a low conductive emission substrate includes a plurality of thin high 03-18-2010
123. 20100062686 NOTCHED GRIND WHEEL AND METHOD TO MANUFACTURE A ROTOR BLADE RETENTION SLOT 03-11-2010
124. 20100058769 FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE WITH DRIVE RING ACTUATION SYSTEM 03-11-2010
125. 20100058735 OPERATIONAL LINE MANAGEMENT OF LOW PRESSURE COMPRESSOR IN A TURBOFAN ENGINE 03-11-2010
126. 20100054953 AIRFOIL WITH LEADING EDGE COOLING PASSAGE 03-04-2010
127. 20100054914 GAS TURBINE ENGINE COMPONENT HAVING DUAL FLOW PASSAGE COOLING CHAMBER FORMED BY SINGLE CORE 03-04-2010
128. 20100054396 METHOD OF CALIBRATION FOR COMPUTED TOMOGRAPHY SCANNERS UTILIZED IN QUALITY CONTROL APPLICATIONS 03-04-2010
129. 20100051594 MICRO-ARC ALLOY CLEANING METHOD AND DEVICE 03-04-2010
130. 20100050936 COATER PLATTER HOMING TOOL - alignment tool is used to ensure proper alignment of a component on a rotating gear relative to a non-rotating platter 03-04-2010
131. 20100050646 Systems and Methods Involving Improved Fuel Atomization in Air-Blast Fuel Nozzles of Gas Turbine Engines 03-04-2010
132. 20100050643 Gas Turbine Engine Systems and Methods Involving Enhanced Fuel Dispersion 03-04-2010
133. 20100050596 THRUST VECTORABLE FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE 03-04-2010
134. 20100050595 GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE 03-04-2010
135. 20100050434 Gas Turbine Airfoil Assemblies and Methods of Repair 03-04-2010
136. 20100050408 Preforms and Related Methods for Repairing Abradable Seals of Gas Turbine Engines 03-04-2010
137. 20100049377 SENSOR AND ANTENNA ARRANGEMENT - exemplary sensor for an aircraft includes a sensor mountable within an aircraft and operative to communicate wirelessly 02-25-2010
138. 20100048202 METHOD OF COMMUNICATING WITH AN AVIONICS BOX VIA TEXT MESSAGING 02-25-2010
139. 20100047474 DEPOSITION APPARATUS HAVING THERMAL HOOD 02-25-2010
140. 20100043394 GAS TURBINE ENGINE FAN VARIABLE AREA NOZZLE WITH SWIVALABLE INSERT SYSTEM 02-25-2010
141. 20100043393 GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE 02-25-2010
142. 20100043391 INJECTOR ASSEMBLY HAVING MULTIPLE MANIFOLDS FOR PROPELLANT DELIVERY 02-25-2010
143. 20100043390 CONTROLLING ICE BUILDUP ON AIRCRAFT ENGINE AND NACELLE STATIC AND ROTATING COMPONENTS 02-25-2010
144. 20100042244 METHOD OF DESIGNING TOOL AND TOOL PATH FOR FORMING A ROTOR BLADE INCLUDING AN AIRFOIL PORTION 02-18-2010
145. 20100040479 Gas Turbine Engine Systems Involving Baffle Assemblies 02-18-2010
146. 20100040478 Cooled Airfoils and Gas Turbine Engine Systems Involving Such Airfoils 02-18-2010
147. 20100040460 Platforms with Curved Side Edges and Gas Turbine Engine Systems Involving Such Platforms 02-18-2010
148. 20100037994 METHOD OF PROCESSING MARAGING STEEL - method of processing a workpiece of maraging steel includes receiving a workpiece of maraging steel that has been 02-18-2010
149. 20100037590 LOW VELOCITY INJECTOR MANIFOLD FOR HYPERGOLIC ROCKET ENGINE 02-18-2010
150. 20100037588 VARIABLE FAN NOZZLE USING SHAPE MEMORY MATERIAL 02-18-2010
151. 20100034644 HYBRID SEAL ASSEMBLY FOR A FAN-TURBINE ROTOR OF A TIP TURBINE ENGINE 02-11-2010
152. 20100032415 Repair Methods Involving Conductive Heat Resistance Welding 02-11-2010
153. 20100031790 CONTROL OF WHITE-ETCHED LAYER DURING MACHINING 02-11-2010
154. 20100031627 Heater Assemblies, Gas Turbine Engine Systems Involving Such Heater Assemblies and Methods for Manufacturing Such Heater Assemblies 02-11-2010
155. 20100030526 AXIAL BOLTED FLANGE DESIGN METHODS AND SYSTEMS 02-04-2010
156. 20100028725 FUEL CELL INSTRUMENTATION SYSTEM - instrumentation system utilizes a single light source collimated through windows through a gas line in communication 02-04-2010
157. 20100025158 Gas Turbine Engine Systems and Methods Involving Oil Flow Management 02-04-2010
158. 20100021716 THERMAL BARRIER SYSTEM AND BONDING METHOD 01-28-2010
159. 20100018213 GAS TURBINE ENGINE WITH ROTATIONALLY OVERLAPPED FAN VARIABLE AREA NOZZLE 01-28-2010
160. 20100017092 HYBRID FAULT ISOLATION SYSTEM UTILIZING BOTH MODEL-BASED AND EMPIRICAL COMPONENTS 01-21-2010
161. 20100017055 SEQUENCE DIAGRAM SYSTEM - method of generating a test sequence diagram includes: linking a first action of the plurality of actions with a second action 01-21-2010
162. 20100011740 TURBOFAN ENGINE OPERATION CONTROL - A turbofan engine is provided that includes a spool 01-21-2010
163. 20100010645 BASEPOINT ESTIMATOR - method of estimating a basepoint includes receiving a plurality of goals wherein each goal has a desired value 01-14-2010
164. 20100008764 GAS TURBINE ENGINE WITH A VARIABLE EXIT AREA FAN NOZZLE, NACELLE ASSEMBLY OF SUCH A ENGINE, AND CORRESPONDING OPERATING METHOD 01-14-2010
165. 20100008761 COOLABLE AIRFOIL TRAILING EDGE PASSAGE - airfoil suitable for use in a gas turbine engine having at least one feed passage at least in part defined 01-14-2010
166. 20100005806 EDUCTOR SYSTEM FOR A GAS TURBINE ENGINE - power plant includes a gas turbine engine contained at least partially within an enclosure 01-14-2010
167. 20100005805 FLOW SLEEVE WITH TABBED DIRECT COMBUSTION LINER COOLING AIR 01-14-2010
168. 20100005803 COMBUSTION LINER FOR A GAS TURBINE ENGINE 01-14-2010
169. 20100005778 FAN VARIABLE AREA NOZZLE WITH CABLE ACTUATOR SYSTEM 01-14-2010
170. 20100005777 DUAL FUNCTION CASCADE INTEGRATED VARIABLE AREA FAN NOZZLE AND THRUST REVERSER 01-14-2010
171. 20100003142 AIRFOIL WITH TAPERED RADIAL COOLING PASSAGE 01-07-2010
172. 20100003123 INLET AIR HEATING SYSTEM FOR A GAS TURBINE ENGINE 01-07-2010
173. 20100003121 VARIABLE AREA FAN NOZZLE FOR ACCOMMODATING A FOREIGN OBJECT STRIKE EVENT 01-07-2010
174. 20100000698 CASTING SYSTEM FOR INVESTMENT CASTING PROCESS 01-07-2010
175. 20100000220 FAN VARIABLE AREA NOZZLE WITH ELECTROMECHANICAL ACTUATOR 01-07-2010
176. 20100000200 IMPINGEMENT COOLING DEVICE - impingement cooling sleeve includes a sleeve body having an inner surface to face a transition duct and an outer surface 01-07-2010
177. 20100000199 MANAGING LOW PRESSURE TURBINE MAXIMUM SPEED IN A TURBOFAN ENGINE 01-07-2010
178. 20090326706 OPTIMAL DIMENSIONAL AND MECHANICAL PROPERTIES OF LASER SINTERED HARDWARE BY THERMAL ANALYSIS AND PARAMETER OPTIMIZATION 12-31-2009
179. 20090325468 ABRASIVE WATERJET MACHINING AND METHOD TO MANUFACTURE A CURVED ROTOR BLADE RETENTION SLOT 12-31-2009
180. 20090324852 Systems and methods for forming components with thermal barrier coatings 12-31-2009
181. 20090320488 GAS TURBINE ENGINE WITH NOISE ATTENUATING VARIABLE AREA FAN NOZZLE 12-31-2009
182. 20090320285 EDM MACHINING AND METHOD TO MANUFACTURE A CURVED ROTOR BLADE RETENTION SLOT 12-31-2009
183. 20090317241 VARIABLE STATOR VANE ASSEMBLY FOR A TURBINE ENGINE 12-24-2009
184. 20090317229 INTEGRATED ACTUATOR MODULE FOR GAS TURBINE ENGINE 12-24-2009
185. 20090317175 SLIDEABLE LINER LINK ASSEMBLY - example engine assembly includes a first attachment structure secured to an engine casing or an engine liner 12-24-2009
186. 20090317029 BEARING SYSTEM - includes an inner ring that surrounds an axis of rotation an outer ring spaced radially outwards from the inner ring 12-24-2009
187. 20090314881 ENGINE MOUNT SYSTEM FOR A TURBOFAN GAS TURBINE ENGINE 12-24-2009
188. 20090313998 AXIALLY SPLIT NOZZLE LINER FOR CONVERGENT NOZZLE 12-24-2009
189. 20090313966 METHOD AND APPARATUS FOR DETERMINING FAILURES OF GAS SHUTOFF VALVES IN GAS TURBINES 12-24-2009
190. 20090313965 RADIAL BALL BEARING - bearing assembly includes an outer race and an inner race with a ball bearing element located between the inner and the outer 12-24-2009
191. 20090313825 GAS TURBINE ENGINE EXHAUST COMPONENT AND MANUFACTURING METHOD OF SAME 12-24-2009
192. 20090308761 RECAST REMOVAL METHOD - method of removing recast from a substrate is disclosed 12-17-2009
193. 20090308077 HOLE PATTERN FOR GAS TURBINE COMBUSTOR - combustor for a turbine engine includes an outer liner having a row of circumferentially distributed outer 12-17-2009
194. 20090307000 METHOD AND SYSTEM FOR GLOBALLY MONITORING AIRCRAFT COMPONENTS 12-10-2009
195. 20090304516 PLATFORM MATE FACE CONTOURS FOR TURBINE AIRFOILS 12-10-2009
196. 20090301095 PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL 12-10-2009
197. 20090301093 SLIDEABLE LINER ANCHORING ASSEMBLY - example gas turbine engine includes an engine casing and an engine liner within the engine casing 12-10-2009
198. 20090297999 IGNITER/THRUSTER WITH CATALYTIC DECOMPOSITION CHAMBER 12-03-2009
199. 20090297357 PROPFAN ASSEMBLY - includes a plurality of blades that each include an internal cavity containing a noise attenuation structure 12-03-2009
200. 20090297350 HOOP SNAP SPACER - mount interface between two rotating gas turbine engine components includes a rigid ring to provide radial deflection restraint 12-03-2009
201. 20090297338 VARIABLE AREA NOZZLE ASSISTED NOISE CONTROL OF A GAS TURBINE ENGINE 12-03-2009
202. 20090297334 GAS TURBINE ENGINE HAVING CONTROLLABLE INLET GUIDE VANES 12-03-2009
203. 20090295796 METHOD OF UPDATING A MODEL - example method of updating a model includes locating points on a part establishing a reference dimension using the point 12-03-2009
204. 20090293498 PIVOTING LINER HANGER - example turbine engine assembly includes a first attachment structure secured to an engine casing or an engine liner 12-03-2009
205. 20090293497 GAS TURBINE ENGINE ASSEMBLY - includes an inlet lip assembly, a fan containment case, and a front flange 12-03-2009
206. 20090293496 GAS TURBINE ENGINES GENERATING ELECTRICITY BY COOLING COOLING AIR 12-03-2009
207. 20090293489 COMBUSTOR LINER CAP ASSEMBLY - liner cap assembly is disclosed for use in a gas turbine engine combustor 12-03-2009
208. 20090293254 INTEGRATED WASH UNIT FOR A TURBINE ENGINE 12-03-2009
209. 20090292437 Systems and Methods Involving Multiplexed Engine Control Signals 11-26-2009
210. 20090291205 METHOD FOR A REPAIR PROCESS - includes the steps of subjecting a substrate coated with at least one protective metallic coating to a nitric acid 11-26-2009
211. 20090288796 METHOD OF PRODUCING A CASTABLE HIGH TEMPERATURE ALUMINUM ALLOY BY CONTROLLED SOLIDIFICATION 11-26-2009
212. 20090288387 GAS TURBINE ENGINE BIFURCATION LOCATED IN A FAN VARIABLE AREA NOZZLE 11-26-2009
213. 20090288386 TRI-BODY VARIABLE AREA FAN NOZZLE AND THRUST REVERSER 11-26-2009
214. 20090287458 BROACH TOOL DESIGN METHODOLOGY AND SYSTEMS 11-19-2009
215. 20090286003 METHOD OF COATING A TURBINE ENGINE COMPONENT USING A LIGHT CURABLE MASK 11-19-2009
216. 20090285690 AXIAL BLADE SLOT PRESSURE FACE WITH UNDERCUT 11-19-2009
217. 20090285647 METHOD OF MACHINING INTEGRAL BLADED ROTORS FOR A GAS TURBINE ENGINE 11-19-2009
218. 20090281641 MULTIVARIABLE CONTROL SYSTEM - method for controlling a multivariable system according to one non-limiting embodiment includes receiving a plurality of 11-12-2009
219. 20090281640 BASEPOINT ESTIMATOR - method of estimating a basepoint includes receiving a plurality of goals wherein each goal has a desired value 11-12-2009
220. 20090277325 ELECTROSTATIC PARTICULATE SEPARATION FOR EMISSION TREATMENT SYSTEMS 11-12-2009
221. 20090276387 HYBRID FAULT REASONING AND GUIDED TROUBLESHOOTING SYSTEM 11-05-2009
222. 20090276136 METHOD FOR CALCULATING CONFIDENCE ON PREDICTION IN FAULT DIAGNOSIS SYSTEMS 11-05-2009
223. 20090274848 IMPINGEMENT PART COOLING - This disclosure relates to a thermal spray coating system including a table that is configured to support a component 11-05-2009
224. 20090274556 GAS TURBINE ENGINE CASE WITH REPLACED FLANGE AND METHOD OF REPAIRING THE SAME USING COLD METAL TRANSFER 11-05-2009
225. 20090274553 REPAIRED INTERNAL HOLDING STRUCTURES FOR GAS TURBINE ENGINE CASES AND METHOD OF REPAIRING THE SAME 11-05-2009
226. 20090272123 Gas Turbine Engine Systems and Related Methods Involving Thermally Isolated Retention 11-05-2009
227. 20090271984 METHOD FOR REPAIRING A GAS TURBINE ENGINE COMPONENT 11-05-2009
228. 20090271983 METHOD TO WELD REPAIR BLADE OUTER AIR SEALS 11-05-2009
229. 20090269208 REPAIR METHOD AND REPAIRED ARTICLE - method of repairing an article includes removing an undesirable section of the article attaching a repair section 10-29-2009
230. 20090269184 Gas Turbine Engine Systems Involving Turbine Blade Platforms with Cooling Holes 10-29-2009
231. 20090266912 FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE WITH SLIDING ACTUATION SYSTEM 10-29-2009
232. 20090266446 NICKEL BRAZE ALLOY COMPOSITION - includes a blend of a first nickel alloy and a second nickel alloy 10-29-2009
233. 20090266150 SENSOR CRITICALITY DETERMINATION PROCESS 10-29-2009
234. 20090263622 REPAIR OF COMPOSITE SANDWICH STRUCTURES WITH UNEVEN BOND SURFACES 10-22-2009
235. 20090263574 METHOD OF RESTORING AN ARTICLE - method for restoring an article includes removing an outer portion of a metallic substrate of an initial article having 10-22-2009
236. 20090263251 REDUCED WEIGHT BLADE FOR A GAS TURBINE ENGINE 10-22-2009
237. 20090260994 ELECTRO CHEMICAL GRINDING (ECG) QUILL AND METHOD TO MANUFACTURE A ROTOR BLADE RETENTION SLOT 10-22-2009
238. 20090260345 FAN VARIABLE AREA NOZZLE WITH ADAPTIVE STRUCTURE 10-22-2009
239. 20090259379 REDUCED TAKE-OFF FIELD LENGTH USING VARIABLE NOZZLE 10-15-2009
240. 20090258579 FORM TRANSFER GRINDING METHOD - method of form transfer grinding a three-dimensional shape utilizes a form transfer tool over which a belt is driven 10-15-2009
241. 20090257877 ASYMMETRICAL ROTOR BLADE FIR-TREE ATTACHMENT 10-15-2009
242. 20090257875 PLATFORMLESS TURBINE BLADE - turbine blade rotor assembly is disclosed for a gas turbine engine 10-15-2009
243. 20090255269 Gas Turbine Engine Systems Involving Variable Nozzles with Sliding Doors 10-15-2009
244. 20090255110 PHOTO-ETCHED EDM ELECTRODE - electrical discharge machining electrode includes a body and one or more shaped teeth 10-15-2009
245. 20090252600 ACTUATION OF A TURBOFAN ENGINE BIFURCATION TO CHANGE AN EFFECTIVE NOZZLE EXIT AREA 10-08-2009
246. 20090252597 VALVE SYSTEM FOR A GAS TURBINE ENGINE - valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary 10-08-2009
247. 20090249603 COLD DEPOSITION REPAIR OF CASTING POROSITY 10-08-2009
248. 20090248366 WIRELESS SENSOR ASSEMBLY FOR AN AIRCRAFT COMPONENT 10-01-2009
249. 20090248363 METHOD OF MULTI-LEVEL FAULT ISOLATION DESIGN 10-01-2009
250. 20090246031 METHOD OF RESTORING AN AIRFOIL BLADE - method of repairing an airfoil blade involves the steps of providing an airfoil blade have a leading edge, a 10-01-2009
251. 20090246023 CHAMBERED AIRFOIL COOLING - airfoil assembly includes an airfoil with at least one cavity that is in communication with a source of cooling air 10-01-2009
252. 20090245997 METHOD AND DEVICE TO AVOID TURBO INSTABILITY IN A GAS TURBINE ENGINE 10-01-2009
253. 20090243854 WIRELESS AIRCRAFT MAINTENANCE LOG - method of aircraft maintenance involves storing part information relating to an aircraft part on the aircraft part 10-01-2009
254. 20090243220 FLUID BARRIERS WITH FLEXIBLE BACKING MATERIAL AND METHODS OF REPAIRING AND MANUFACTURING THE SAME 10-01-2009
255. 20090241550 Gas Turbine Engine Systems Involving Variable Nozzles with Flexible Panels 10-01-2009
256. 20090241509 TURBINE ENGINE INLET STRUT DEICING - gas turbine engine is disclosed that includes an inlet case having circumferentially spaced, radially extending 10-01-2009
257. 20090241339 METHOD FOR REPAIRING AN AIRFOIL - example method of repairing an airfoil includes the steps of securing additional material to a worn airfoil and 10-01-2009
258. 20090240471 METHOD OF SYSTEM DESIGN FOR FAILURE DETECTABILITY 09-24-2009
259. 20090240373 ESTABLISHING A USE CYCLE USING A CONTAINER CONDITION 09-24-2009
260. 20090238678 COLD AIR BUFFER SUPPLY TUBE - for a gas turbine engine includes a tube body having a first tube end and a second tube end 09-24-2009
261. 20090236469 MOUNTING SYSTEM FOR A GAS TURBINE ENGINE 09-24-2009
262. 20090235643 VALVE SYSTEM FOR A GAS TURBINE ENGINE - valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary 09-24-2009
263. 20090235642 VALVE SYSTEM FOR A GAS TURBINE ENGINE - valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary 09-24-2009
264. 20090235638 VARIABLE AREA NOZZLE ASSISTED GAS TURBINE ENGINE RESTARTING 09-24-2009
265. 20090235630 NON-INTERRUPTED OIL SUPPLY FOR GAS TURBINE ENGINE 09-24-2009
266. 20090232650 TIP TURBINE ENGINE AND CORRESPONDING OPERATING METHOD 09-17-2009
267. 20090232643 Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method 09-17-2009
268. 20090230628 FACE SEAL FOR GAS TURBINE ENGINE - face seal for a gas turbine engine comprises a seal body that has a contact face to engage a rotating surface 09-17-2009
269. 20090230213 METAL INJECTION MOLDING ATTACHMENT HANGER SYSTEM FOR A COOLING LINER WITHIN A GAS TURBINE ENGINE SWIVEL EXHAUST DUCT 09-17-2009
270. 20090218771 BRISTLE AND PLATE SUBASSEMBLY FIXTURE AND MANUFACTURING METHOD 09-03-2009
271. 20090214351 METHOD OF GENERATING A CURVED BLADE RETENTION SLOT IN A TURBINE DISK 08-27-2009
272. 20090214329 FILTER SYSTEM FOR BLADE OUTER AIR SEAL - gas turbine engine component having a filter mounted adjacent an impingement cavity to filter particles out of 08-27-2009
273. 20090214147 Hydrodynamic Tapered Roller Bearings and Gas Turbine Engine Systems Involving Such Bearings 08-27-2009
274. 20090211091 NON-METALLIC COVER FOR A FIXTURE - assembly includes a fixture including an opening shaped to receive a portion of a turbine engine component 08-27-2009
275. 20090208330 SEALING ASSEMBLY FOR A TURBINE ENGINE - has a brush configured to provide an air seal between an outer air seal segment and a blade 08-20-2009
276. 20090208328 GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE BLADDER SYSTEM 08-20-2009
277. 20090208325 LARGE FILLET AIRFOIL WITH FANNED COOLING HOLE ARRAY 08-20-2009
278. 20090208322 Gas turbine engine systems and methods involving blade outer air seals 08-20-2009
279. 20090208151 BEARING SYSTEM AND METHOD FOR LUBRICATION 08-20-2009
280. 20090205800 Systems and Methods for Reducing the Potential for Riser Backfilling During Investment Casting 08-20-2009
281. 20090205341 GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX 08-20-2009
282. 20090202357 COOLED PUSHER PROPELLER SYSTEM - propulsion system and method includes an annular exhaust nozzle about an axis radially outboard of the annular cooling 08-13-2009
283. 20090193789 VARIABLE AREA FAN NOZZLE THRUST REVERSER 08-06-2009
284. 20090191045 LOW PRESSURE TURBINE WITH COUNTER-ROTATING DRIVES FOR SINGLE SPOOL 07-30-2009
285. 20090188234 SHARED FLOW THERMAL MANAGEMENT SYSTEM - thermal management system includes at least two of a multiple of heat exchangers arranged in an at least 07-30-2009
286. 20090188232 THERMAL MANAGEMENT SYSTEM INTEGRATED PYLON 07-30-2009
287. 20090186238 BRAZED NANO-GRAINED ALUMINUM STRUCTURES - method of processing a brazed article includes forming a braze joint with an aluminum component comprising a 07-23-2009
288. 20090184475 FACE SEAL FOR GAS TURBINE ENGINE - face seal for a gas turbine engine comprises a seal body that has a contact face to engage a rotating surface 07-23-2009
289. 20090184197 PYLON AND ENGINE MOUNT CONFIGURATION - mounting arrangement for a gas turbine engine includes a pylon mount structure that has a fore mount portion and 07-23-2009
290. 20090183512 MOUNTING SYSTEM FOR A GAS TURBINE ENGINE 07-23-2009
291. 20090180861 COOLING ARRANGEMENT FOR TURBINE COMPONENTS 07-16-2009
292. 20090178383 RECOATABLE EXHAUST LINER COOLING ARRANGEMENT 07-16-2009
293. 20090173418 AIRFOIL MASK, AIRFOIL AND MASK SYSTEM, AND MASKING METHOD FOR EDGE PROFILE FINISHING 07-09-2009
294. 20090169386 ANNULAR TURBINE RING ROTOR - fan-turbine rotor assembly includes one or more turbine ring rotors 07-02-2009
295. 20090169385 FAN-TURBINE ROTOR ASSEMBLY WITH INTEGRAL INDUCER SECTION FOR A TIP TURBINE ENGINE 07-02-2009
296. 20090169359 HEAT EXCHANGER ARRANGEMENT FOR TURBINE ENGINE 07-02-2009
297. 20090166001 Endothermic cracking aircraft fuel system 07-02-2009
298. 20090162189 Systems and Methods Involving Variable Throat Area Vanes 06-25-2009
299. 20090162187 COUNTER-ROTATING COMPRESSOR CASE AND ASSEMBLY METHOD FOR TIP TURBINE ENGINE 06-25-2009
300. 20090162156 MACHINE ALIGNMENT SYSTEM - is disclosed that includes a support member 06-25-2009
301. 20090159754 ROTARY WING SYSTEM WITH ION FIELD FLOW CONTROL 06-25-2009
302. 20090158742 METHOD AND APPARATUS FOR MIXING SUBSTANCES 06-25-2009
303. 20090158703 SLIDING RAMP NOZZLE SYSTEM FOR A GAS TURBINE ENGINE 06-25-2009
304. 20090155083 METHOD FOR REPAIRING AN AIRFOIL - example method of repairing an airfoil includes securing a cap to an end portion of a worn airfoil and securing 06-18-2009
305. 20090155079 STACKED ANNULAR COMPONENTS FOR TURBINE ENGINES 06-18-2009
306. 20090155072 FAN NACELLE FLOW CONTROL - This disclosure relates to a gas turbine engine including a core engine that drives a fan 06-18-2009
307. 20090155067 NACELLE ASSEMBLY WITH TURBULATORS - nacelle assembly for a turbine engine has a cowl 06-18-2009
308. 20090155057 COMPRESSOR VARIABLE STAGE REMOTE ACTUATION FOR TURBINE ENGINE 06-18-2009
309. 20090155046 NACELLE ASSEMBLY HAVING INLET BLEED - nacelle assembly for a turbine engine has a cowl 06-18-2009
310. 20090148299 AIRFOIL LEADING EDGE SHAPE TAILORING TO REDUCE HEAT LOAD 06-11-2009
311. 20090148297 FAN-TURBINE ROTOR ASSEMBLY FOR A TIP TURBINE ENGINE 06-11-2009
312. 20090148296 METHOD OF MACHINING A TURBINE DISK - method of manufacturing a turbine disk involves machining to an initial form a slot in a turbine disk using a firm 06-11-2009
313. 20090148292 AXIAL COMPRESSOR FOR TIP TURBINE ENGINE - tip turbine engine according to the present invention provides at least one gear coupling rotation of a bypass 06-11-2009
314. 20090148287 FAN BLADE WITH INTEGRAL DIFFUSER SECTION AND TIP TURBINE BLADE SECTION FOR A TIP TURBINE ENGINE 06-11-2009
315. 20090148282 3D CONTOURED VANE ENDWALL FOR VARIABLE AREA TURBINE VANE ARRANGEMENT 06-11-2009
316. 20090148276 SEAL ASSEMBLY FOR A FAN ROTOR OF A TIP TURBINE ENGINE 06-11-2009
317. 20090148273 COMPRESSOR INLET GUIDE VANE FOR TIP TURBINE ENGINE AND CORRESPONDING CONTROL METHOD 06-11-2009
318. 20090148272 TIP TURBINE ENGINE AND OPERATING METHOD WITH REVERSE CORE AIRFLOW 06-11-2009
319. 20090148269 Gas Turbine Engines and Related Systems Involving Air-Cooled Vanes 06-11-2009
320. 20090146341 Systems and Methods Involving Pattern Molds 06-11-2009
321. 20090145136 TIP TURBINE ENGINE WITH MULTIPLE FAN AND TURBINE STAGES 06-11-2009
322. 20090145135 TURBINE BLOW DOWN STARTER FOR TURBINE ENGINE 06-11-2009
323. 20090145133 EXHAUST LINER ATTACHMENT ARRANGEMENT - turbine engine exhaust nozzle is disclosed that includes an exhaust liner having a first attachment structure 06-11-2009
324. 20090145105 REMOTE ENGINE FUEL CONTROL AND ELECTRONIC ENGINE CONTROL FOR TURBINE ENGINE 06-11-2009
325. 20090145101 PARTICLE SEPARATOR FOR TIP TURBINE ENGINE 06-11-2009
326. 20090142188 SEAL ASSEMBLY FOR A FAN-TURBINE ROTOR OF A TIP TURBINE ENGINE 06-04-2009
327. 20090142184 VECTORING TRANSITION DUCT FOR TURBINE ENGINE 06-04-2009
328. 20090142182 Gas Turbine Engines and Related Systems Involving Offset Turbine Frame Struts 06-04-2009
329. 20090142181 Gas Turbine Engine Systems Involving Mechanically Alterable Vane Throat Areas 06-04-2009
330. 20090140497 FLEXIBLE SEAL FOR GAS TURBINE ENGINE SYSTEM 06-04-2009
331. 20090139243 GAS TURBINE ENGINE WITH PYLON MOUNTED ACCESSORY DRIVE 06-04-2009
332. 20090139221 METERING SHEET AND ISO-GRID ARRANGEMENT FOR A NON AXI-SYMMETRIC SHAPED COOLING LINER WITHIN A GAS TURBINE ENGINE EXHAUST DUCT 06-04-2009
333. 20090136740 ARTICLE HAVING COMPOSITE LAYER - composite article includes a substrate and a layer attached to the substrate 05-28-2009
334. 20090136345 SEGMENTED CERAMIC LAYER FOR MEMBER OF GAS TURBINE ENGINE 05-28-2009
335. 20090133401 COMBUSTOR FOR TURBINE ENGINE - turbine engine includes an annular combustor having a combustion chamber defined between an annular outer wall and an 05-28-2009
336. 20090133376 COMBINED GEARBOX BREATHER AND DRAIN MAST FOR JET AIRCRAFT ENGINE 05-28-2009
337. 20090132697 INTEGRATION OF PASSENGER AND FLIGHT OPERATION COMMUNICATIONS 05-21-2009
338. 20090130446 HIGH TEMPERATURE REFRACTORY COATINGS FOR CERAMIC SUBSTRATES 05-21-2009
339. 20090130424 CLOSED PORE CERAMIC COMPOSITE ARTICLE - composite article includes a substrate and a thermal barrier secured to the substrate 05-21-2009
340. 20090129922 ACCESS DOOR FOR GAS TURBINE ENGINE COMPONENTS 05-21-2009
341. 20090127401 ION FIELD FLOW CONTROL DEVICE - boundary layer control apparatus and method for controlling and adjusting the boundary layer of a fluid flowing over a 05-21-2009
342. 20090126337 RETROFIT DIRT SEPARATOR FOR GAS TURBINE ENGINE 05-21-2009
343. 20090125554 STATISTICAL PROCESS CONTROL RESOURCE TRACKER 05-14-2009
344. 20090123274 SPLIT GEARBOX AND NACELLE ARRANGEMENT - gas turbine engine is disclosed that includes at least first and second gearboxes rotationally coupled to at 05-14-2009
345. 20090123271 FAN SHAFT RETENTION - retention system for a fan in a gas turbine engine includes a shaft that is rotatable relative to a bearing support structure 05-14-2009
346. 20090123266 AIR SEALING ELEMENT - turbine blade outer air seal segment assembly has a first turbine blade outer air seal segment with a first end portion 05-14-2009
347. 20090121441 DUAL CONFIGURATION SEAL ASSEMBLY FOR A ROTATIONAL ASSEMBLY 05-14-2009
348. 20090121083 Nacelle Flow Assembly - nacelle assembly for a turbine engine has a cowl for a turbine engine 05-14-2009
349. 20090120102 TURBINE ENGINE FRAME HAVING AN ACTUATED EQUILIBRATING CASE 05-14-2009
350. 20090120101 Organic Matrix Composite Components, Systems Using Such Components, and Methods for Manufacturing Such Components 05-14-2009
351. 20090120100 Starter Generator System for a Tip Turbine Engine 05-14-2009
352. 20090120058 Tip Turbine Engine Integral Fan, Combustor, and Turbine Case 05-14-2009
353. 20090117429 DIRECT CARBON FUEL CELL HAVING A SEPARATION DEVICE 05-07-2009
354. 20090116953 Turbine airfoil with platform cooling - Convective cooling of gas turbine engine airfoil platforms is enhanced by grooving the interface of the 05-07-2009
355. 20090116951 METHOD AND APPARATUS FOR FAN SHAFT BEARING LUBRICATION 05-07-2009
356. 20090114740 NOZZLE ASSEMBLY WITH FLOW CONDUITS - nozzle assembly for a turbine engine has a convergent portion for converging fluid flow from a turbine engine core 05-07-2009
357. 20090112354 METHOD OF DETERMINING OPTIMAL PARAMETERS FOR MACHINING A WORKPIECE 04-30-2009
358. 20090112340 METHOD OF ANIMATING STRUCTURAL VIBRATION UNDER OPERATIONAL CONDITIONS 04-30-2009
359. 20090110831 METHOD OF SPRAYING A TURBINE ENGINE COMPONENT 04-30-2009
360. 20090110545 Systems and Methods for Controlling Seal Clearance In A Turbine Engine 04-30-2009
361. 20090110544 INFLATABLE BLEED VALVE FOR A TURBINE ENGINE 04-30-2009
362. 20090110537 Gas Turbine Engine Systems Involving Integrated Fluid Conduits 04-30-2009
363. 20090107211 AIRFOIL SHOT PEENING TEST STRIPS - shot peening operation is developed utilizing a test strip and test strip holder 04-30-2009
364. 20090099796 AEROELASTIC MODEL USING THE PRINCIPAL SHAPES OF MODES (AMPS) 04-16-2009
365. 20090097983 METHOD FOR RESTORING AIRFOIL TIP CONTOUR 04-16-2009
366. 20090097967 GAS TURBINE ENGINE WITH VARIABLE GEOMETRY FAN EXIT GUIDE VANE SYSTEM 04-16-2009
367. 20090097965 SINGLE ACTUATOR CONTROLLED ROTATIONAL FLOW BALANCE SYSTEM 04-16-2009
368. 20090096174 BLADE OUTER AIR SEAL FOR A GAS TURBINE ENGINE 04-16-2009
369. 20090095083 ACOUSTIC METHOD AND APPARATUS FOR FRACTURE DETECTION OF BALL BEARINGS 04-16-2009
370. 20090095043 CONFORMABLE TOOLING FOR LOCALIZED SHOT PEENING 04-16-2009
371. 20090094961 THRUST REVERSING VARIABLE AREA NOZZLE - gas turbine engine system includes a first nozzle section associated with a gas turbine engine bypass passage 04-16-2009
372. 20090094831 METHOD FOR RESTORING AIRFOIL CONTOUR ON INTEGRALLY BLADED ROTORS 04-16-2009
373. 20090094828 METHOD AND APPARATUS FOR HOLE CRACK REMOVAL 04-16-2009
374. 20090092842 ARTICLE AND METHOD FOR EROSION RESISTANT COMPOSITE 04-09-2009
375. 20090092485 SEAL ASSEMBLY RETENTION FEATURE AND ASSEMBLY METHOD 04-09-2009
376. 20090092480 GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE 04-09-2009
377. 20090081039 GAS TURBINE ENGINE FRONT ARCHITECTURE MODULARITY 03-26-2009
378. 20090081035 GAS TURBINE ENGINE COMPRESSOR CASE MOUNTING ARRANGEMENT 03-26-2009
379. 20090081025 SEGMENTED COOLING AIR CAVITY FOR TURBINE COMPONENT 03-26-2009
380. 20090075115 MULTI-LAYERED THERMAL BARRIER COATING - thermal barrier coating system includes a substrate a first transition metal layer on the substrate 03-19-2009
381. 20090074644 REDUCED TEMPERATURE CALCINING METHOD FOR HYDROGEN GENERATION 03-19-2009
382. 20090074575 COOLING CIRCUIT FLOW PATH FOR A TURBINE SECTION AIRFOIL 03-19-2009
383. 20090074570 Local application of a protective coating on a shrouded gas turbine engine component 03-19-2009
384. 20090074568 VARIABLE FAN INLET GUIDE VANE ASSEMBLY, TURBINE ENGINE WITH SUCH AN ASSEMBLY AND CORRESPONDING CONTROLLING METHOD 03-19-2009
385. 20090074565 TURBINE ENGINE WITH DIFFERENTIAL GEAR DRIVEN FAN AND COMPRESSOR 03-19-2009
386. 20090074563 SEAL FOR GAS TURBINE ENGINE COMPONENT - gas turbine engine component includes a pressurized fluid source an airfoil and a seal member for selectively 03-19-2009
387. 20090072490 Convergent Divergent Nozzle with Edge Cooled Divergent Seals 03-19-2009
388. 20090072044 Convergent Divergent Nozzle With Slot Cooled Nozzle Liner 03-19-2009
389. 20090071162 PERIPHERAL COMBUSTOR FOR TIP TURBINE ENGINE 03-19-2009
390. 20090071121 COUNTER-ROTATING GEARBOX FOR TIP TURBINE ENGINE 03-19-2009
391. 20090068349 METHOD OF REPAIRING A TURBINE ENGINE COMPONENT 03-12-2009
392. 20090067999 EXTENDED IMPINGEMENT COOLING DEVICE AND METHOD 03-12-2009
393. 20090067997 Gas turbine engine with canted pocket and canted knife edge seal 03-12-2009
394. 20090067993 COATED VARIABLE AREA FAN NOZZLE - variable area fan nozzle for use with a gas turbine engine system includes a nozzle section that is movable between a 03-12-2009
395. 20090067978 VARIABLE AREA TURBINE VANE ARRANGEMENT - turbine section of a gas turbine engine includes a ring of turbine nozzle segments each having paired turbine 03-12-2009
396. 20090065168 LOST WAX INVESTMENT CASTING GATING FIXTURES 03-12-2009
397. 20090064659 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONAL VALVE SYSTEM 03-12-2009
398. 20090064500 METHOD OF REPAIRING A TURBINE ENGINE COMPONENT 03-12-2009
399. 20090061075 METHOD AND APPARATUS FOR MEASURING COATING THICKNESS WITH A LASER 03-05-2009
400. 20090060747 ORIENTED FIBER CERAMIC MATRIX COMPOSITE ABRADABLE THERMAL BARRIER COATING 03-05-2009
401. 20090060741 TURBINE ENGINE BLADE COOLING - blade is provided for a turbine engine that includes an exterior surface 03-05-2009
402. 20090060733 OVERLAP INTERFACE FOR A GAS TURBINE ENGINE COMPOSITE ENGINE CASE 03-05-2009
403. 20090060704 ACTIVE FLOW CONTROL FOR NACELLE INLET - The disclosed turbine engine includes a fan nacelle surrounding a fan and including an inlet arranged upstream 03-05-2009
404. 20090056343 ENGINE MOUNTING CONFIGURATION FOR A TURBOFAN GAS TURBINE ENGINE 03-05-2009
405. 20090056306 GAS TURBINE ENGINE FRONT ARCHITECTURE - turbine engine is disclosed that includes a fan case surrounding a fan 03-05-2009
406. 20090056096 METHOD OF REPAIRING A TURBINE ENGINE COMPONENT 03-05-2009
407. 20090053554 THERMAL BARRIER COATING SYSTEM FOR THERMAL MECHANICAL FATIGUE RESISTANCE 02-26-2009
408. 20090053422 MASKING FIXTURE FOR A COATING PROCESS - masking fixture for use in a coating process includes a first fixture plate for supporting a first work piece 02-26-2009
409. 20090053058 GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE 02-26-2009
410. 20090053043 ATTACHMENT INTERFACE FOR A GAS TURBINE ENGINE COMPOSITE DUCT STRUCTURE 02-26-2009
411. 20090053041 GAS TURBINE ENGINE CASE FOR CLEARANCE CONTROL 02-26-2009
412. 20090050183 INTEGRATED WASH UNIT FOR A TURBINE ENGINE 02-26-2009
413. 20090049794 HEAT EXCHANGER PANEL AND MANUFACTURING METHOD THEREOF USING TRANSIENT LIQUID PHASE BONDING AGENT AND VACUUM COMPRESSION BRAZING 02-26-2009
414. 20090049689 METHOD REPAIR OF TURBINE BLADE TIP - method of repair of a turbine blade involves inspecting a turbine blade having an internal cavity and a cap 02-26-2009
415. 20090045620 DAMPER ROOT RING - damper that provides damping to the motion caused by flow induced vibration of a bellows type expansion joint 02-19-2009
416. 20090045045 PUCK FOR CATHODIC ARC COATING WITH CONTINUOUS GROOVE TO CONTROL ARC 02-19-2009
417. 20090044512 DIRT SEPARATOR FOR COMPRESSOR DIFFUSER IN GAS TURBINE ENGINE 02-19-2009
418. 20090038151 METHOD FOR ESTABLISHING A LOCATION OF AN ELEVATED STRESS REGION 02-12-2009
419. 20090035601 ZIRCONIUM MODIFIED PROTECTIVE COATING - protective coating system includes a nickel-aluminum-zirconium alloy coating having at least one phase selected 02-05-2009
420. 20090030142 PRECERAMIC SILAZANE POLYMER FOR CERAMIC MATERIALS 01-29-2009
421. 20090028714 METHOD OF DESIGNING TOOL AND TOOL PATH FOR FORMING A ROTOR BLADE INCLUDING AN AIRFOIL PORTION 01-29-2009
422. 20090028702 BLADE COOLING PASSAGE FOR A TURBINE ENGINE 01-29-2009
423. 20090022579 BURN RESISTANT ORGANIC MATRIX COMPOSITE MATERIAL 01-22-2009
424. 20090020013 MEMBRANE BASED DEOXYGENATOR FOR PROCESSING FLUIDS 01-22-2009
425. 20090019858 TIP TURBINE ENGINE WITH ASPIRATED COMPRESSOR 01-22-2009
426. 20090013693 INTEGRATED FUEL NOZZLE WITH FEEDBACK CONTROL FOR A GAS TURBINE ENGINE 01-15-2009
427. 20090010751 ANGLED ON-BOARD INJECTOR - secondary flow system provides a compact injector cooling structure for turbine blades which includes an Angled On-board 01-08-2009
428. 20090008508 VARIABLE CONTOUR NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE 01-08-2009
429. 20090004013 TURBINE BLADE NESTED SEAL AND DAMPER ASSEMBLY 01-01-2009
430. 20090003997 VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE 01-01-2009
431. 20090000453 TOOL ALIGNMENT FIXTURE - example apparatus for aligning a pressure tapping tool includes a base having an engagement portion 01-01-2009
432. 20090000272 TANGENTIAL ANTI-SWIRL AIR SUPPLY - turbofan flow delivery system includes a fan case housing a fan 01-01-2009
433. 20080317588 MANAGING SPOOL BEARING LOAD USING VARIABLE AREA FLOW NOZZLE 12-25-2008
434. 20080317587 VARIABLE-SHAPE VARIABLE-STAGGER INLET GUIDE VANE FLAP 12-25-2008
435. 20080315529 EASE OF ASSEMBLY AID FOR BRUSH SEAL - brush seal assembly is formed of a bristle array receiving at least one housing member 12-25-2008
436. 20080310956 VARIABLE GEOMETRY GAS TURBINE ENGINE NACELLE ASSEMBLY WITH NANOELECTROMECHANICAL SYSTEM 12-18-2008
437. 20080308684 NACELLE WITH ARTICULATING LEADING EDGE SLATES 12-18-2008
438. 20080308048 COMPOSITE DUCT ASSEMBLY - carbon composite duct assembly has a duct body having an opening 12-18-2008
439. 20080304958 GAS TURBINE ENGINE WITH AIR AND FUEL COOLING SYSTEM 12-11-2008
440. 20080302907 Fan Variable Area Nozzle Positional Measurement System 12-11-2008
441. 20080302335 Injector assembly having multiple manifolds for propellant delivery 12-11-2008
442. 20080299504 RESONANCE DRIVEN GLOW PLUG TORCH IGNITER AND IGNITION METHOD 12-04-2008
443. 20080298950 NACELLE COMPARTMENT PLENUM FOR BLEED AIR FLOW DELIVERY SYSTEM 12-04-2008
444. 20080296440 FLOW DISTRIBUTION SYSTEM FOR INLET FLOW CONTROL 12-04-2008
445. 20080296439 INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL 12-04-2008
446. 20080295481 Fluidic vectoring for exhaust nozzle - exhaust nozzle assembly provides fluidic thrust vectoring of the primary stream to enhance aircraft 12-04-2008
447. 20080289254 METHOD AND APPARATUS FOR A COAL GASIFIER 11-27-2008
448. 20080286995 TWO-PLUG ELECTRICAL OUTLET WITH DUAL VOLTAGE 11-20-2008
449. 20080286094 VARIABLE GEOMETRY NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE 11-20-2008
450. 20080283676 VARIABLE CONTRACTION RATIO NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE 11-20-2008
451. 20080276763 NO MESS OIL FILTER REMOVAL TOOL - oil filter removal tool includes a member for providing a reservoir to capture leakage oil as the oil filter is 11-13-2008
452. 20080273963 Impingement skin core cooling for gas turbine engine blade 11-06-2008
453. 20080273961 FLUTTER SENSING AND CONTROL SYSTEM FOR A GAS TURBINE ENGINE 11-06-2008
454. 20080268709 FULLY SHIELDED BACKSHELL FOR ELECTRICAL CONNECTOR 10-30-2008
455. 20080267762 NACELLE ASSEMBLY HAVING INLET AIRFOIL FOR A GAS TURBINE ENGINE 10-30-2008
456. 20080264035 COOLANT FLOW SWIRLER FOR A ROCKET ENGINE 10-30-2008
457. 20080260523 GAS TURBINE ENGINE WITH INTEGRATED ABRADABLE SEAL 10-23-2008
458. 20080260522 GAS TURBINE ENGINE WITH INTEGRATED ABRADABLE SEAL AND MOUNT PLATE 10-23-2008
459. 20080258016 NACELLE ASSEMBLY WITHOUT LOWER BI-FI SPLITTER 10-23-2008
460. 20080253882 TURBINE ENGINE VARIABLE STATOR VANE - includes a platform having a circumference adjoining opposing surfaces 10-16-2008
461. 20080249828 Method and System for Workscope Management and Control 10-09-2008
462. 20080245075 HOODED AIR/FUEL SWIRLER FOR A GAS TURBINE ENGINE 10-09-2008
463. 20080237454 STACKABLE HELIOSTAT FRAME STRUCTURE - heliostat includes a pedestal, a transmission system, a frame assembly, and a mirror assembly 10-02-2008
464. 20080236136 LINKAGE SYSTEM WITH WEAR REDUCTION - linkage system includes a pivot bias assembly at each pivot which removes internal clearances and resultant 10-02-2008
465. 20080234850 MODEL BASED DEFINITION INSTALLATION AND ASSEMBLY DRAWING PROCESS 09-25-2008
466. 20080230629 MODE STRUT AND DIVERGENT FLAP INTERFACE - In one example, a gas turbine engine includes an exhaust nozzle 09-25-2008
467. 20080226462 CAST FEATURES FOR A TURBINE ENGINE AIRFOIL 09-18-2008
468. 20080226453 Balanced Turbine Rotor Fan Blade for a Tip Turbine Engine 09-18-2008
469. 20080220240 Composite article and fabrication method 09-11-2008
470. 20080219854 TURBINE COMPONENT WITH AXIALLY SPACED RADIALLY FLOWING MICROCIRCUIT COOLING CHANNELS 09-11-2008
471. 20080219835 ABRADABLE COMPONENT FOR A GAS TURBINE ENGINE 09-11-2008
472. 20080219833 Inducer for a Fan Blade of a Tip Turbine Engine 09-11-2008
473. 20080219832 SMALL RADIAL PROFILE SHROUD FOR VARIABLE VANE STRUCTURE IN A GAS TURBINE ENGINE 09-11-2008
474. 20080216585 CONSTANT MOMENT TESTING DEVICE FOR ELONGATED MEMBERS 09-11-2008
475. 20080206056 Modular Tip Turbine Engine - tip turbine engine assembly includes a compressor module and a fan module located aft of the compressor module 08-28-2008