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CARLSON, GASKEY & OLDS/PRATT & WHITNEY
BIRMINGHAM, MI US
1. 20090292437 Systems and Methods Involving Multiplexed Engine Control Signals 11-26-20092. 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
3. 20090288796 METHOD OF PRODUCING A CASTABLE HIGH TEMPERATURE ALUMINUM ALLOY BY CONTROLLED SOLIDIFICATION 11-26-2009
4. 20090288387 GAS TURBINE ENGINE BIFURCATION LOCATED IN A FAN VARIABLE AREA NOZZLE 11-26-2009
5. 20090288386 TRI-BODY VARIABLE AREA FAN NOZZLE AND THRUST REVERSER 11-26-2009
6. 20090287458 BROACH TOOL DESIGN METHODOLOGY AND SYSTEMS 11-19-2009
7. 20090286003 METHOD OF COATING A TURBINE ENGINE COMPONENT USING A LIGHT CURABLE MASK 11-19-2009
8. 20090285690 AXIAL BLADE SLOT PRESSURE FACE WITH UNDERCUT 11-19-2009
9. 20090285647 METHOD OF MACHINING INTEGRAL BLADED ROTORS FOR A GAS TURBINE ENGINE 11-19-2009
10. 20090281641 MULTIVARIABLE CONTROL SYSTEM - method for controlling a multivariable system according to one non-limiting embodiment includes receiving a plurality of 11-12-2009
11. 20090281640 BASEPOINT ESTIMATOR - method of estimating a basepoint includes receiving a plurality of goals wherein each goal has a desired value 11-12-2009
12. 20090277325 ELECTROSTATIC PARTICULATE SEPARATION FOR EMISSION TREATMENT SYSTEMS 11-12-2009
13. 20090276387 HYBRID FAULT REASONING AND GUIDED TROUBLESHOOTING SYSTEM 11-05-2009
14. 20090276136 METHOD FOR CALCULATING CONFIDENCE ON PREDICTION IN FAULT DIAGNOSIS SYSTEMS 11-05-2009
15. 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
16. 20090274556 GAS TURBINE ENGINE CASE WITH REPLACED FLANGE AND METHOD OF REPAIRING THE SAME USING COLD METAL TRANSFER 11-05-2009
17. 20090274553 REPAIRED INTERNAL HOLDING STRUCTURES FOR GAS TURBINE ENGINE CASES AND METHOD OF REPAIRING THE SAME 11-05-2009
18. 20090272123 Gas Turbine Engine Systems and Related Methods Involving Thermally Isolated Retention 11-05-2009
19. 20090271984 METHOD FOR REPAIRING A GAS TURBINE ENGINE COMPONENT 11-05-2009
20. 20090271983 METHOD TO WELD REPAIR BLADE OUTER AIR SEALS 11-05-2009
21. 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
22. 20090269184 Gas Turbine Engine Systems Involving Turbine Blade Platforms with Cooling Holes 10-29-2009
23. 20090266912 FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE WITH SLIDING ACTUATION SYSTEM 10-29-2009
24. 20090266446 NICKEL BRAZE ALLOY COMPOSITION - includes a blend of a first nickel alloy and a second nickel alloy 10-29-2009
25. 20090266150 SENSOR CRITICALITY DETERMINATION PROCESS 10-29-2009
26. 20090263622 REPAIR OF COMPOSITE SANDWICH STRUCTURES WITH UNEVEN BOND SURFACES 10-22-2009
27. 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
28. 20090263251 REDUCED WEIGHT BLADE FOR A GAS TURBINE ENGINE 10-22-2009
29. 20090260994 ELECTRO CHEMICAL GRINDING (ECG) QUILL AND METHOD TO MANUFACTURE A ROTOR BLADE RETENTION SLOT 10-22-2009
30. 20090260345 FAN VARIABLE AREA NOZZLE WITH ADAPTIVE STRUCTURE 10-22-2009
31. 20090259379 REDUCED TAKE-OFF FIELD LENGTH USING VARIABLE NOZZLE 10-15-2009
32. 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
33. 20090257877 ASYMMETRICAL ROTOR BLADE FIR-TREE ATTACHMENT 10-15-2009
34. 20090257875 PLATFORMLESS TURBINE BLADE - turbine blade rotor assembly is disclosed for a gas turbine engine 10-15-2009
35. 20090255269 Gas Turbine Engine Systems Involving Variable Nozzles with Sliding Doors 10-15-2009
36. 20090255110 PHOTO-ETCHED EDM ELECTRODE - electrical discharge machining electrode includes a body and one or more shaped teeth 10-15-2009
37. 20090252600 ACTUATION OF A TURBOFAN ENGINE BIFURCATION TO CHANGE AN EFFECTIVE NOZZLE EXIT AREA 10-08-2009
38. 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
39. 20090249603 COLD DEPOSITION REPAIR OF CASTING POROSITY 10-08-2009
40. 20090248366 WIRELESS SENSOR ASSEMBLY FOR AN AIRCRAFT COMPONENT 10-01-2009
41. 20090248363 METHOD OF MULTI-LEVEL FAULT ISOLATION DESIGN 10-01-2009
42. 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
43. 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
44. 20090245997 METHOD AND DEVICE TO AVOID TURBO INSTABILITY IN A GAS TURBINE ENGINE 10-01-2009
45. 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
46. 20090243220 FLUID BARRIERS WITH FLEXIBLE BACKING MATERIAL AND METHODS OF REPAIRING AND MANUFACTURING THE SAME 10-01-2009
47. 20090241550 Gas Turbine Engine Systems Involving Variable Nozzles with Flexible Panels 10-01-2009
48. 20090241509 TURBINE ENGINE INLET STRUT DEICING - gas turbine engine is disclosed that includes an inlet case having circumferentially spaced, radially extending 10-01-2009
49. 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
50. 20090240471 METHOD OF SYSTEM DESIGN FOR FAILURE DETECTABILITY 09-24-2009
51. 20090240373 ESTABLISHING A USE CYCLE USING A CONTAINER CONDITION 09-24-2009
52. 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
53. 20090236469 MOUNTING SYSTEM FOR A GAS TURBINE ENGINE 09-24-2009
54. 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
55. 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
56. 20090235638 VARIABLE AREA NOZZLE ASSISTED GAS TURBINE ENGINE RESTARTING 09-24-2009
57. 20090235630 NON-INTERRUPTED OIL SUPPLY FOR GAS TURBINE ENGINE 09-24-2009
58. 20090232650 TIP TURBINE ENGINE AND CORRESPONDING OPERATING METHOD 09-17-2009
59. 20090232643 Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method 09-17-2009
60. 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
61. 20090230213 METAL INJECTION MOLDING ATTACHMENT HANGER SYSTEM FOR A COOLING LINER WITHIN A GAS TURBINE ENGINE SWIVEL EXHAUST DUCT 09-17-2009
62. 20090218771 BRISTLE AND PLATE SUBASSEMBLY FIXTURE AND MANUFACTURING METHOD 09-03-2009
63. 20090214351 METHOD OF GENERATING A CURVED BLADE RETENTION SLOT IN A TURBINE DISK 08-27-2009
64. 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
65. 20090214147 Hydrodynamic Tapered Roller Bearings and Gas Turbine Engine Systems Involving Such Bearings 08-27-2009
66. 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
67. 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
68. 20090208328 GAS TURBINE ENGINE WITH VARIABLE AREA FAN NOZZLE BLADDER SYSTEM 08-20-2009
69. 20090208325 LARGE FILLET AIRFOIL WITH FANNED COOLING HOLE ARRAY 08-20-2009
70. 20090208322 Gas turbine engine systems and methods involving blade outer air seals 08-20-2009
71. 20090208151 BEARING SYSTEM AND METHOD FOR LUBRICATION 08-20-2009
72. 20090205800 Systems and Methods for Reducing the Potential for Riser Backfilling During Investment Casting 08-20-2009
73. 20090205341 GAS TURBINE ENGINE WITH TWIN TOWERSHAFT ACCESSORY GEARBOX 08-20-2009
74. 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
75. 20090193789 VARIABLE AREA FAN NOZZLE THRUST REVERSER 08-06-2009
76. 20090191045 LOW PRESSURE TURBINE WITH COUNTER-ROTATING DRIVES FOR SINGLE SPOOL 07-30-2009
77. 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
78. 20090188232 THERMAL MANAGEMENT SYSTEM INTEGRATED PYLON 07-30-2009
79. 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
80. 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
81. 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
82. 20090183512 MOUNTING SYSTEM FOR A GAS TURBINE ENGINE 07-23-2009
83. 20090180861 COOLING ARRANGEMENT FOR TURBINE COMPONENTS 07-16-2009
84. 20090178383 RECOATABLE EXHAUST LINER COOLING ARRANGEMENT 07-16-2009
85. 20090173418 AIRFOIL MASK, AIRFOIL AND MASK SYSTEM, AND MASKING METHOD FOR EDGE PROFILE FINISHING 07-09-2009
86. 20090169386 ANNULAR TURBINE RING ROTOR - fan-turbine rotor assembly includes one or more turbine ring rotors 07-02-2009
87. 20090169385 FAN-TURBINE ROTOR ASSEMBLY WITH INTEGRAL INDUCER SECTION FOR A TIP TURBINE ENGINE 07-02-2009
88. 20090169359 HEAT EXCHANGER ARRANGEMENT FOR TURBINE ENGINE 07-02-2009
89. 20090166001 Endothermic cracking aircraft fuel system 07-02-2009
90. 20090162189 Systems and Methods Involving Variable Throat Area Vanes 06-25-2009
91. 20090162187 COUNTER-ROTATING COMPRESSOR CASE AND ASSEMBLY METHOD FOR TIP TURBINE ENGINE 06-25-2009
92. 20090162156 MACHINE ALIGNMENT SYSTEM - is disclosed that includes a support member 06-25-2009
93. 20090159754 ROTARY WING SYSTEM WITH ION FIELD FLOW CONTROL 06-25-2009
94. 20090158742 METHOD AND APPARATUS FOR MIXING SUBSTANCES 06-25-2009
95. 20090158703 SLIDING RAMP NOZZLE SYSTEM FOR A GAS TURBINE ENGINE 06-25-2009
96. 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
97. 20090155079 STACKED ANNULAR COMPONENTS FOR TURBINE ENGINES 06-18-2009
98. 20090155072 FAN NACELLE FLOW CONTROL - This disclosure relates to a gas turbine engine including a core engine that drives a fan 06-18-2009
99. 20090155067 NACELLE ASSEMBLY WITH TURBULATORS - nacelle assembly for a turbine engine has a cowl 06-18-2009
100. 20090155057 COMPRESSOR VARIABLE STAGE REMOTE ACTUATION FOR TURBINE ENGINE 06-18-2009
101. 20090155046 NACELLE ASSEMBLY HAVING INLET BLEED - nacelle assembly for a turbine engine has a cowl 06-18-2009
102. 20090148299 AIRFOIL LEADING EDGE SHAPE TAILORING TO REDUCE HEAT LOAD 06-11-2009
103. 20090148297 FAN-TURBINE ROTOR ASSEMBLY FOR A TIP TURBINE ENGINE 06-11-2009
104. 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
105. 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
106. 20090148287 FAN BLADE WITH INTEGRAL DIFFUSER SECTION AND TIP TURBINE BLADE SECTION FOR A TIP TURBINE ENGINE 06-11-2009
107. 20090148282 3D CONTOURED VANE ENDWALL FOR VARIABLE AREA TURBINE VANE ARRANGEMENT 06-11-2009
108. 20090148276 SEAL ASSEMBLY FOR A FAN ROTOR OF A TIP TURBINE ENGINE 06-11-2009
109. 20090148273 COMPRESSOR INLET GUIDE VANE FOR TIP TURBINE ENGINE AND CORRESPONDING CONTROL METHOD 06-11-2009
110. 20090148272 TIP TURBINE ENGINE AND OPERATING METHOD WITH REVERSE CORE AIRFLOW 06-11-2009
111. 20090148269 Gas Turbine Engines and Related Systems Involving Air-Cooled Vanes 06-11-2009
112. 20090146341 Systems and Methods Involving Pattern Molds 06-11-2009
113. 20090145136 TIP TURBINE ENGINE WITH MULTIPLE FAN AND TURBINE STAGES 06-11-2009
114. 20090145135 TURBINE BLOW DOWN STARTER FOR TURBINE ENGINE 06-11-2009
115. 20090145133 EXHAUST LINER ATTACHMENT ARRANGEMENT - turbine engine exhaust nozzle is disclosed that includes an exhaust liner having a first attachment structure 06-11-2009
116. 20090145105 REMOTE ENGINE FUEL CONTROL AND ELECTRONIC ENGINE CONTROL FOR TURBINE ENGINE 06-11-2009
117. 20090145101 PARTICLE SEPARATOR FOR TIP TURBINE ENGINE 06-11-2009
118. 20090142188 SEAL ASSEMBLY FOR A FAN-TURBINE ROTOR OF A TIP TURBINE ENGINE 06-04-2009
119. 20090142184 VECTORING TRANSITION DUCT FOR TURBINE ENGINE 06-04-2009
120. 20090142182 Gas Turbine Engines and Related Systems Involving Offset Turbine Frame Struts 06-04-2009
121. 20090142181 Gas Turbine Engine Systems Involving Mechanically Alterable Vane Throat Areas 06-04-2009
122. 20090140497 FLEXIBLE SEAL FOR GAS TURBINE ENGINE SYSTEM 06-04-2009
123. 20090139243 GAS TURBINE ENGINE WITH PYLON MOUNTED ACCESSORY DRIVE 06-04-2009
124. 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
125. 20090136740 ARTICLE HAVING COMPOSITE LAYER - composite article includes a substrate and a layer attached to the substrate 05-28-2009
126. 20090136345 SEGMENTED CERAMIC LAYER FOR MEMBER OF GAS TURBINE ENGINE 05-28-2009
127. 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
128. 20090133376 COMBINED GEARBOX BREATHER AND DRAIN MAST FOR JET AIRCRAFT ENGINE 05-28-2009
129. 20090132697 INTEGRATION OF PASSENGER AND FLIGHT OPERATION COMMUNICATIONS 05-21-2009
130. 20090130446 HIGH TEMPERATURE REFRACTORY COATINGS FOR CERAMIC SUBSTRATES 05-21-2009
131. 20090130424 CLOSED PORE CERAMIC COMPOSITE ARTICLE - composite article includes a substrate and a thermal barrier secured to the substrate 05-21-2009
132. 20090129922 ACCESS DOOR FOR GAS TURBINE ENGINE COMPONENTS 05-21-2009
133. 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
134. 20090126337 RETROFIT DIRT SEPARATOR FOR GAS TURBINE ENGINE 05-21-2009
135. 20090125554 STATISTICAL PROCESS CONTROL RESOURCE TRACKER 05-14-2009
136. 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
137. 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
138. 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
139. 20090121441 DUAL CONFIGURATION SEAL ASSEMBLY FOR A ROTATIONAL ASSEMBLY 05-14-2009
140. 20090121083 Nacelle Flow Assembly - nacelle assembly for a turbine engine has a cowl for a turbine engine 05-14-2009
141. 20090120102 TURBINE ENGINE FRAME HAVING AN ACTUATED EQUILIBRATING CASE 05-14-2009
142. 20090120101 Organic Matrix Composite Components, Systems Using Such Components, and Methods for Manufacturing Such Components 05-14-2009
143. 20090120100 Starter Generator System for a Tip Turbine Engine 05-14-2009
144. 20090120058 Tip Turbine Engine Integral Fan, Combustor, and Turbine Case 05-14-2009
145. 20090117429 DIRECT CARBON FUEL CELL HAVING A SEPARATION DEVICE 05-07-2009
146. 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
147. 20090116951 METHOD AND APPARATUS FOR FAN SHAFT BEARING LUBRICATION 05-07-2009
148. 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
149. 20090112354 METHOD OF DETERMINING OPTIMAL PARAMETERS FOR MACHINING A WORKPIECE 04-30-2009
150. 20090112340 METHOD OF ANIMATING STRUCTURAL VIBRATION UNDER OPERATIONAL CONDITIONS 04-30-2009
151. 20090110831 METHOD OF SPRAYING A TURBINE ENGINE COMPONENT 04-30-2009
152. 20090110545 Systems and Methods for Controlling Seal Clearance In A Turbine Engine 04-30-2009
153. 20090110544 INFLATABLE BLEED VALVE FOR A TURBINE ENGINE 04-30-2009
154. 20090110537 Gas Turbine Engine Systems Involving Integrated Fluid Conduits 04-30-2009
155. 20090107211 AIRFOIL SHOT PEENING TEST STRIPS - shot peening operation is developed utilizing a test strip and test strip holder 04-30-2009
156. 20090099796 AEROELASTIC MODEL USING THE PRINCIPAL SHAPES OF MODES (AMPS) 04-16-2009
157. 20090097983 METHOD FOR RESTORING AIRFOIL TIP CONTOUR 04-16-2009
158. 20090097967 GAS TURBINE ENGINE WITH VARIABLE GEOMETRY FAN EXIT GUIDE VANE SYSTEM 04-16-2009
159. 20090097965 SINGLE ACTUATOR CONTROLLED ROTATIONAL FLOW BALANCE SYSTEM 04-16-2009
160. 20090096174 BLADE OUTER AIR SEAL FOR A GAS TURBINE ENGINE 04-16-2009
161. 20090095083 ACOUSTIC METHOD AND APPARATUS FOR FRACTURE DETECTION OF BALL BEARINGS 04-16-2009
162. 20090095043 CONFORMABLE TOOLING FOR LOCALIZED SHOT PEENING 04-16-2009
163. 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
164. 20090094831 METHOD FOR RESTORING AIRFOIL CONTOUR ON INTEGRALLY BLADED ROTORS 04-16-2009
165. 20090094828 METHOD AND APPARATUS FOR HOLE CRACK REMOVAL 04-16-2009
166. 20090092842 ARTICLE AND METHOD FOR EROSION RESISTANT COMPOSITE 04-09-2009
167. 20090092485 SEAL ASSEMBLY RETENTION FEATURE AND ASSEMBLY METHOD 04-09-2009
168. 20090092480 GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE 04-09-2009
169. 20090081039 GAS TURBINE ENGINE FRONT ARCHITECTURE MODULARITY 03-26-2009
170. 20090081035 GAS TURBINE ENGINE COMPRESSOR CASE MOUNTING ARRANGEMENT 03-26-2009
171. 20090081025 SEGMENTED COOLING AIR CAVITY FOR TURBINE COMPONENT 03-26-2009
172. 20090075115 MULTI-LAYERED THERMAL BARRIER COATING - thermal barrier coating system includes a substrate a first transition metal layer on the substrate 03-19-2009
173. 20090074644 REDUCED TEMPERATURE CALCINING METHOD FOR HYDROGEN GENERATION 03-19-2009
174. 20090074575 COOLING CIRCUIT FLOW PATH FOR A TURBINE SECTION AIRFOIL 03-19-2009
175. 20090074570 Local application of a protective coating on a shrouded gas turbine engine component 03-19-2009
176. 20090074568 VARIABLE FAN INLET GUIDE VANE ASSEMBLY, TURBINE ENGINE WITH SUCH AN ASSEMBLY AND CORRESPONDING CONTROLLING METHOD 03-19-2009
177. 20090074565 TURBINE ENGINE WITH DIFFERENTIAL GEAR DRIVEN FAN AND COMPRESSOR 03-19-2009
178. 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
179. 20090072490 Convergent Divergent Nozzle with Edge Cooled Divergent Seals 03-19-2009
180. 20090072044 Convergent Divergent Nozzle With Slot Cooled Nozzle Liner 03-19-2009
181. 20090071162 PERIPHERAL COMBUSTOR FOR TIP TURBINE ENGINE 03-19-2009
182. 20090071121 COUNTER-ROTATING GEARBOX FOR TIP TURBINE ENGINE 03-19-2009
183. 20090068349 METHOD OF REPAIRING A TURBINE ENGINE COMPONENT 03-12-2009
184. 20090067999 EXTENDED IMPINGEMENT COOLING DEVICE AND METHOD 03-12-2009
185. 20090067997 Gas turbine engine with canted pocket and canted knife edge seal 03-12-2009
186. 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
187. 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
188. 20090065168 LOST WAX INVESTMENT CASTING GATING FIXTURES 03-12-2009
189. 20090064659 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE HAVING A ROTATIONAL VALVE SYSTEM 03-12-2009
190. 20090064500 METHOD OF REPAIRING A TURBINE ENGINE COMPONENT 03-12-2009
191. 20090061075 METHOD AND APPARATUS FOR MEASURING COATING THICKNESS WITH A LASER 03-05-2009
192. 20090060747 ORIENTED FIBER CERAMIC MATRIX COMPOSITE ABRADABLE THERMAL BARRIER COATING 03-05-2009
193. 20090060741 TURBINE ENGINE BLADE COOLING - blade is provided for a turbine engine that includes an exterior surface 03-05-2009
194. 20090060733 OVERLAP INTERFACE FOR A GAS TURBINE ENGINE COMPOSITE ENGINE CASE 03-05-2009
195. 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
196. 20090056343 ENGINE MOUNTING CONFIGURATION FOR A TURBOFAN GAS TURBINE ENGINE 03-05-2009
197. 20090056306 GAS TURBINE ENGINE FRONT ARCHITECTURE - turbine engine is disclosed that includes a fan case surrounding a fan 03-05-2009
198. 20090056096 METHOD OF REPAIRING A TURBINE ENGINE COMPONENT 03-05-2009
199. 20090053554 THERMAL BARRIER COATING SYSTEM FOR THERMAL MECHANICAL FATIGUE RESISTANCE 02-26-2009
200. 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
201. 20090053058 GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE 02-26-2009
202. 20090053043 ATTACHMENT INTERFACE FOR A GAS TURBINE ENGINE COMPOSITE DUCT STRUCTURE 02-26-2009
203. 20090053041 GAS TURBINE ENGINE CASE FOR CLEARANCE CONTROL 02-26-2009
204. 20090050183 INTEGRATED WASH UNIT FOR A TURBINE ENGINE 02-26-2009
205. 20090049794 HEAT EXCHANGER PANEL AND MANUFACTURING METHOD THEREOF USING TRANSIENT LIQUID PHASE BONDING AGENT AND VACUUM COMPRESSION BRAZING 02-26-2009
206. 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
207. 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
208. 20090045045 PUCK FOR CATHODIC ARC COATING WITH CONTINUOUS GROOVE TO CONTROL ARC 02-19-2009
209. 20090044512 DIRT SEPARATOR FOR COMPRESSOR DIFFUSER IN GAS TURBINE ENGINE 02-19-2009
210. 20090038151 METHOD FOR ESTABLISHING A LOCATION OF AN ELEVATED STRESS REGION 02-12-2009
211. 20090035601 ZIRCONIUM MODIFIED PROTECTIVE COATING - protective coating system includes a nickel-aluminum-zirconium alloy coating having at least one phase selected 02-05-2009
212. 20090030142 PRECERAMIC SILAZANE POLYMER FOR CERAMIC MATERIALS 01-29-2009
213. 20090028714 METHOD OF DESIGNING TOOL AND TOOL PATH FOR FORMING A ROTOR BLADE INCLUDING AN AIRFOIL PORTION 01-29-2009
214. 20090028702 BLADE COOLING PASSAGE FOR A TURBINE ENGINE 01-29-2009
215. 20090022579 BURN RESISTANT ORGANIC MATRIX COMPOSITE MATERIAL 01-22-2009
216. 20090020013 MEMBRANE BASED DEOXYGENATOR FOR PROCESSING FLUIDS 01-22-2009
217. 20090019858 TIP TURBINE ENGINE WITH ASPIRATED COMPRESSOR 01-22-2009
218. 20090013693 INTEGRATED FUEL NOZZLE WITH FEEDBACK CONTROL FOR A GAS TURBINE ENGINE 01-15-2009
219. 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
220. 20090008508 VARIABLE CONTOUR NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE 01-08-2009
221. 20090004013 TURBINE BLADE NESTED SEAL AND DAMPER ASSEMBLY 01-01-2009
222. 20090003997 VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBINE ENGINE 01-01-2009
223. 20090000453 TOOL ALIGNMENT FIXTURE - example apparatus for aligning a pressure tapping tool includes a base having an engagement portion 01-01-2009
224. 20090000272 TANGENTIAL ANTI-SWIRL AIR SUPPLY - turbofan flow delivery system includes a fan case housing a fan 01-01-2009
225. 20080317588 MANAGING SPOOL BEARING LOAD USING VARIABLE AREA FLOW NOZZLE 12-25-2008
226. 20080317587 VARIABLE-SHAPE VARIABLE-STAGGER INLET GUIDE VANE FLAP 12-25-2008
227. 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
228. 20080310956 VARIABLE GEOMETRY GAS TURBINE ENGINE NACELLE ASSEMBLY WITH NANOELECTROMECHANICAL SYSTEM 12-18-2008
229. 20080308684 NACELLE WITH ARTICULATING LEADING EDGE SLATES 12-18-2008
230. 20080308048 COMPOSITE DUCT ASSEMBLY - carbon composite duct assembly has a duct body having an opening 12-18-2008
231. 20080304958 GAS TURBINE ENGINE WITH AIR AND FUEL COOLING SYSTEM 12-11-2008
232. 20080302907 Fan Variable Area Nozzle Positional Measurement System 12-11-2008
233. 20080302335 Injector assembly having multiple manifolds for propellant delivery 12-11-2008
234. 20080299504 RESONANCE DRIVEN GLOW PLUG TORCH IGNITER AND IGNITION METHOD 12-04-2008
235. 20080298950 NACELLE COMPARTMENT PLENUM FOR BLEED AIR FLOW DELIVERY SYSTEM 12-04-2008
236. 20080296440 FLOW DISTRIBUTION SYSTEM FOR INLET FLOW CONTROL 12-04-2008
237. 20080296439 INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL 12-04-2008
238. 20080295481 Fluidic vectoring for exhaust nozzle - exhaust nozzle assembly provides fluidic thrust vectoring of the primary stream to enhance aircraft 12-04-2008
239. 20080289254 METHOD AND APPARATUS FOR A COAL GASIFIER 11-27-2008
240. 20080286995 TWO-PLUG ELECTRICAL OUTLET WITH DUAL VOLTAGE 11-20-2008
241. 20080286094 VARIABLE GEOMETRY NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE 11-20-2008
242. 20080283676 VARIABLE CONTRACTION RATIO NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE 11-20-2008
243. 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
244. 20080273963 Impingement skin core cooling for gas turbine engine blade 11-06-2008
245. 20080273961 FLUTTER SENSING AND CONTROL SYSTEM FOR A GAS TURBINE ENGINE 11-06-2008
246. 20080268709 FULLY SHIELDED BACKSHELL FOR ELECTRICAL CONNECTOR 10-30-2008
247. 20080267762 NACELLE ASSEMBLY HAVING INLET AIRFOIL FOR A GAS TURBINE ENGINE 10-30-2008
248. 20080264035 COOLANT FLOW SWIRLER FOR A ROCKET ENGINE 10-30-2008
249. 20080260523 GAS TURBINE ENGINE WITH INTEGRATED ABRADABLE SEAL 10-23-2008
250. 20080260522 GAS TURBINE ENGINE WITH INTEGRATED ABRADABLE SEAL AND MOUNT PLATE 10-23-2008
251. 20080258016 NACELLE ASSEMBLY WITHOUT LOWER BI-FI SPLITTER 10-23-2008
252. 20080253882 TURBINE ENGINE VARIABLE STATOR VANE - includes a platform having a circumference adjoining opposing surfaces 10-16-2008
253. 20080249828 Method and System for Workscope Management and Control 10-09-2008
254. 20080245075 HOODED AIR/FUEL SWIRLER FOR A GAS TURBINE ENGINE 10-09-2008
255. 20080237454 STACKABLE HELIOSTAT FRAME STRUCTURE - heliostat includes a pedestal, a transmission system, a frame assembly, and a mirror assembly 10-02-2008
256. 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
257. 20080234850 MODEL BASED DEFINITION INSTALLATION AND ASSEMBLY DRAWING PROCESS 09-25-2008
258. 20080230629 MODE STRUT AND DIVERGENT FLAP INTERFACE - In one example, a gas turbine engine includes an exhaust nozzle 09-25-2008
259. 20080226462 CAST FEATURES FOR A TURBINE ENGINE AIRFOIL 09-18-2008
260. 20080226453 Balanced Turbine Rotor Fan Blade for a Tip Turbine Engine 09-18-2008
261. 20080220240 Composite article and fabrication method 09-11-2008
262. 20080219854 TURBINE COMPONENT WITH AXIALLY SPACED RADIALLY FLOWING MICROCIRCUIT COOLING CHANNELS 09-11-2008
263. 20080219835 ABRADABLE COMPONENT FOR A GAS TURBINE ENGINE 09-11-2008
264. 20080219833 Inducer for a Fan Blade of a Tip Turbine Engine 09-11-2008
265. 20080219832 SMALL RADIAL PROFILE SHROUD FOR VARIABLE VANE STRUCTURE IN A GAS TURBINE ENGINE 09-11-2008
266. 20080216585 CONSTANT MOMENT TESTING DEVICE FOR ELONGATED MEMBERS 09-11-2008
267. 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