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BACHMAN & LAPOINTE, P.C. (P&W)
NEW HAVEN, CT US
1. 20110033284 STRUCTURALLY DIVERSE THERMAL BARRIER COATINGS 02-10-20112. 20110027573 Lubricated Abradable Coating - coated article has a metallic substrate 02-03-2011
3. 20110027569 Fastener - has a metallic member and a nonmetallic cap member 02-03-2011
4. 20110020115 REFRACTORY METAL CORE INTEGRALLY CAST EXIT TRENCH 01-27-2011
5. 20100305742 System and Method for an Integrated Additive Manufacturing Cell for Complex Components 12-02-2010
6. 20100304037 Thermal Barrier Coatings and Application Methods 12-02-2010
7. 20100285330 Vapor Deposition of Dissimilar Materials 11-11-2010
8. 20100276103 Metallic Coated Cores to Facilitate Thin Wall Casting 11-04-2010
9. 20100263590 Vapor Deposition Electron Beam Current Control 10-21-2010
10. 20100260613 Process for preventing the formation of secondary reaction zone in susceptible articles, and articles manufactured using same 10-14-2010
11. 20100247328 Microcircuit cooling for blades - turbine engine component such as a turbine blade includes at least one cooling circuit having a plurality of legs 09-30-2010
12. 20100247323 Erosion barrier for thermal barrier coatings 09-30-2010
13. 20100229529 Timing control system for pulse detonation engines 09-16-2010
14. 20100226762 Structural members in a pedestal array - turbine engine component has a flow path wall and a support wall 09-09-2010
15. 20100221098 Peripheral Microcircuit Serpentine Cooling for Turbine Airfoils 09-02-2010
16. 20100219325 METALLIC COATED CORES TO FACILITATE THIN WALL CASTING 09-02-2010
17. 20100218483 CONTROLLED FAN STREAM FLOW BYPASS - turbine engine component of a turbofan engine fitted with a bypass air valve includes at least one turbine engine 09-02-2010
18. 20100218478 Turbine engine compressor - counter-rotating blade stage in lieu of a stator stage may compensate for relatively low rotational speed of a gas turbine 09-02-2010
19. 20100206512 Process and Refractory Metal Core For Creating Varying Thickness Microcircuits For Turbine Engine Components 08-19-2010
20. 20100200549 Microplasma Spray Apparatus and Method for Coating Articles Using Same 08-12-2010
21. 20100199494 METHOD AND APPARATUS FOR MICROPLASMA SPRAY COATING A PORTION OF A COMPRESSOR BLADE IN A GAS TURBINE ENGINE 08-12-2010
22. 20100196728 OXIDE COATING FOUNDATION FOR PROMOTING TBC ADHERENCE 08-05-2010
23. 20100196684 Turbine Element Repair - Ion-enhanced physical vapor deposition is utilized to deposit repair material on Ti alloy turbine parts 08-05-2010
24. 20100196663 Segmented Abradable Coatings and Process(es) for Applying the Same 08-05-2010
25. 20100196605 Yttria-Stabilized Zirconia Coating with a Molten Silicate Resistant Outer Layer 08-05-2010
26. 20100196160 COOLED TURBINE BLADE SHROUD - turbine blade for use in high temperature applications includes an as-cast airfoil portion and an as-cast outer tip shroud 08-05-2010
27. 20100196149 Apparatus and Method for Preventing Cracking of Turbine Engine Cases 08-05-2010
28. 20100189911 Bond Coating and Thermal Barrier Compositions, Processes for Applying Both, and Their Coated Articles 07-29-2010
29. 20100159149 APPARATUS FOR REDUCING STRESS WHEN APPLYING COATINGS, PROCESSES FOR APPLYING THE SAME AND THEIR COATED ARTICLES 06-24-2010
30. 20100158695 Superalloy Compositions, Articles, and Methods of Manufacture 06-24-2010
31. 20100158669 MICROCIRCUITS FOR SMALL ENGINES - turbine engine component for use in a small engine application has an airfoil portion having a root portion 06-24-2010
32. 20100155251 HARD ANODIZE OF COLD SPRAY ALUMINUM LAYER 06-24-2010
33. 20100155224 Multi-Component Deposition - Ion-enhanced physical vapor deposition is augmented by sputtering to deposit multi-component materials 06-24-2010
34. 20100154590 PROCESS FOR PRODUCING REFRACTORY METAL ALLOY POWDERS 06-24-2010
35. 20100154425 STRAIN TOLERANT THERMAL BARRIER COATING SYSTEM 06-24-2010
36. 20100151230 PROCESS FOR CONTROLLING FATIGUE DEBIT OF A COATED ARTICLE 06-17-2010
37. 20100150735 Multi-Peripheral Serpentine Microcircuits For High Aspect Ratio Blades 06-17-2010
38. 20100150711 APPARATUS AND METHOD FOR PREVENTING CRACKING OF TURBINE ENGINE CASES 06-17-2010
39. 20100136241 SILICATE RESISTANT THERMAL BARRIER COATING WITH ALTERNATING LAYERS 06-03-2010
40. 20100135846 LOWER COST HIGH STRENGTH SINGLE CRYSTAL SUPERALLOYS WITH REDUCED RE AND RU CONTENT 06-03-2010
41. 20100129217 Castings, Casting Cores, and Methods - gas turbine engine component has a leading edge and a trailing edge and a pressure side and a suction side 05-27-2010
42. 20100129195 Castings, Casting Cores, and Methods - The pattern has a pattern material and a casting core combination 05-27-2010
43. 20100129194 Castings, Casting Cores, and Methods - The pattern has a pattern material and a casting core combination 05-27-2010
44. 20100126960 Serpentine Microcircuit Vortex Turbulators for Blade Cooling 05-27-2010
45. 20100126177 Augmentor Pilot - gas turbine engine augmenter has a gas flowpath 05-27-2010
46. 20100124495 Turbine Engine Rotor Hub - rotor has a central shaft having a central longitudinal axis 05-20-2010
47. 20100122789 Investment Casting Cores and Methods - investment casting core combination includes a metallic casting core and a ceramic feedcore 05-20-2010
48. 20100119718 Dense protective coatings, methods for their preparation and coated articles 05-13-2010
49. 20100119375 Pre-Coating Burnishing of Erosion Coated Parts 05-13-2010
50. 20100116452 Investment casting cores and methods - method involves forming a core assembly 05-13-2010
51. 20100108206 Preferential hardening of single crystal blades 05-06-2010
52. 20100107971 CONVERGENT SPRAY NOZZLE APPARATUS - convergent spray nozzle for food applications is disclosed 05-06-2010
53. 20100104859 BOND COATING AND THERMAL BARRIER COMPOSITIONS, PROCESSES FOR APPLYING BOTH, AND THEIR COATED ARTICLES 04-29-2010
54. 20100101232 COMPLIANT METAL SUPPORT FOR CERAMIC COMBUSTOR LINER IN A GAS TURBINE ENGINE 04-29-2010
55. 20100098923 Segmented abradable coatings and process (ES) for applying the same 04-22-2010
56. 20100098865 DURABLE REACTIVE THERMAL BARRIER COATINGS 04-22-2010
57. 20100096368 Deposition apparatus and methods - Microspray apparatus and methods involve injecting powdered material into a plasma gas stream 04-22-2010
58. 20100086411 MODERATE DENSITY, LOW DENSITY, AND EXTREMELY LOW DENSITY SINGLE CRYSTAL ALLOYS FOR HIGH AN2 APPLICATIONS 04-08-2010
59. 20100084107 Method for preventing formation of cellular gamma prime in cast nickel superalloys 04-08-2010
60. 20100080707 Blade Outer Air Seals, Cores, and Manufacture Methods 04-01-2010
61. 20100047075 Thermal Barrier Coating Compositions, Processes for Applying Same and Articles Coated with Same 02-25-2010
62. 20100046319 Acoustic Acceleration of Fluid Mixing in Porous Materials 02-25-2010
63. 20100028549 Dispersion Strengthened Rare Earth Stabilized Zirconia 02-04-2010
64. 20100023366 Process and apparatus for comprehensive configuration valid bill of material planning and auditing 01-28-2010
65. 20100021290 Ceramic matrix composite turbine engine vane 01-28-2010
66. 20100014102 Cooled Wall Thickness Control - casting includes a wall thickness check feature for measuring thickness of a wall second aside an in-wall cooling 01-21-2010
67. 20100009092 ECONOMIC OXIDATION AND FATIGUE RESISTANT METALLIC COATING 01-14-2010
68. 20100008790 Superalloy compositions, articles, and methods of manufacture 01-14-2010
69. 20100008758 LEADING EDGE COOLING WITH MICROCIRCUIT ANTI-CORIOLIS DEVICE 01-14-2010
70. 20100005637 Turbine Element Repair Fixture - blade processing fixture has first and second jaws 01-14-2010
71. 20090324425 PARTICLE RESISTANT IN-WALL COOLING PASSAGE INLET 12-31-2009
72. 20090320287 Compressor blade flow form technique for repair 12-31-2009
73. 20090317227 AIRFOIL EMBODYING MIXED LOADING CONVENTIONS 12-24-2009
74. 20090314202 Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engine 12-24-2009
75. 20090308733 Thermal Barrier Coating Compositions, Processes for Applying Same and Articles Coated with Same 12-17-2009
76. 20090305866 Reduced Thermal Conductivity Thermal Barrier Coating by Electron Beam-Physical Vapor Deposition Process 12-10-2009
77. 20090301680 BLADE OUTER AIR SEAL CORES AND MANUFACTURE METHODS 12-10-2009
78. 20090293488 Combustor - gas turbine engine combustor has forward bulkhead extending between inboard and outboard walls and cooperating therewith to define a 12-03-2009
79. 20090286056 COATING METHODS AND APPARATUS USING PRE-FORMED CERAMIC MASK 11-19-2009
80. 20090260365 Augmentor Spray Bar Mounting - gas turbine engine augmentor has a centerbody within a gas flowpath from upstream to downstream 10-22-2009
81. 20090258165 PLATINUM-MODIFIED CATHODIC ARC COATING - process for coating a part comprises the steps of providing a chamber which is electrically connected as an 10-15-2009
82. 20090238695 FULL COVERAGE TRAILING EDGE MICROCIRCUIT WITH ALTERNATING CONVERGING EXITS 09-24-2009
83. 20090238694 RADIAL SPLIT SERPENTINE MICROCIRCUITS - turbine engine component, such as a turbine blade has an airfoil portion with an airfoil mean line, a pressure 09-24-2009
84. 20090238675 AIRFOIL THERMAL MANAGEMENT WITH MICROCIRCUIT COOLING 09-24-2009
85. 20090208752 LOW TRANSIENT AND STEADY STATE THERMAL STRESS DISK SHAPED COMPONENTS 08-20-2009
86. 20090208662 Methods for Repairing a Workpiece - method for repairing a workpiece includes the steps of providing an unstripped coated workpiece comprising a surface 08-20-2009
87. 20090208343 SERPENTINE MICROCIRCUITS FOR HOT GAS MIGRATION 08-20-2009
88. 20090208339 BLADE ROOT STRESS RELIEF - gas turbine engine, a stress relief is formed along a blade root and disk slot junction 08-20-2009
89. 20090200275 Solid state additive manufacturing system 08-13-2009
90. 20090197075 COATINGS AND COATING PROCESSES FOR MOLYBDENUM SUBSTRATES 08-06-2009
91. 20090178618 MULTILAYERED BORON NITRIDE/SILICON NITRIDE FIBER COATINGS 07-16-2009
92. 20090169368 BLADE OUTER AIR SEAL - turbine engine blade outer air seal segment has a body having a base portion 07-02-2009
93. 20090159517 Effluent collection unit for engine washing 06-25-2009
94. 20090117369 Anodic-cathodic corrosion inhibitor-conductive polymer composite 05-07-2009
95. 20090116956 MANUFACTURABLE AND INSPECTABLE COOLING MICROCIRCUITS FOR BLADE-OUTER-AIR-SEALS 05-07-2009
96. 20090107109 Variable bypass turbine fan - engine for powering a vehicle, such as a military aircraft or a commercial aircraft, is provided 04-30-2009
97. 20090104035 ADVANCED TURBULATOR ARRANGEMENTS FOR MICROCIRCUITS 04-23-2009
98. 20090097977 SERPENTINE MICROCIRCUIT COOLING WITH PRESSURE SIDE FEATURES 04-16-2009
99. 20090095435 MACHINING OF PARTS HAVING HOLES - Removing of a casting core from a metal casting leaves at least one opening in a surface of the metal 04-16-2009
100. 20090088038 MULTILAYERED BORON NITRIDE/SILICON NITRIDE FIBER COATINGS 04-02-2009
101. 20090087306 BLADE OUTER AIR SEALS, CORES, AND MANUFACTURE METHODS 04-02-2009
102. 20090075564 SUPERABRASIVE TOOL AND MACHINING METHODS 03-19-2009
103. 20090067994 Blade outer air seal - turbine engine blade outer air seal segment has a body having a base portion 03-12-2009
104. 20090061184 Processes for Applying a Conversion Coating with Conductive Additive(S) and the Resultant Coated Articles 03-05-2009
105. 20090060828 Fluorine Extraction Process For Fluoro-Refractory Coatings And Articles Manufactured According To Said Process 03-05-2009
106. 20090049837 GAS TURBINE ENGINE AIR VALVE ASSEMBLY - has first and second valving elements 02-26-2009
107. 20090035473 Conversion Coatings With Conductive Additives, Processes For Applying Same And Their Coated Articles 02-05-2009
108. 20090028703 Airfoil mini-core plugging devices - turbine engine component such as a high pressure turbine vane has an airfoil portion and at least one coolant 01-29-2009
109. 20090028697 LOW TRANSIENT THERMAL STRESS TURBINE ENGINE COMPONENTS 01-29-2009
110. 20090017205 Apparatus and method for coating internal surfaces of a turbine engine component 01-15-2009
111. 20090011123 Corrosion protective coating through cold spray 01-08-2009
112. 20090007882 Compound cycle rotary engine - compound cycle engine system has a rotary engine, which rotary engine generates exhaust gas 01-08-2009
113. 20090003993 Ceramic matrix composite turbine engine vane 01-01-2009
114. 20090000754 Investment casting cores and methods - method involves forming a core assembly 01-01-2009
115. 20080313058 Process And System For Identifying Demand For Inventory 12-18-2008
116. 20080277090 Investment casting cores and methods - investment casting core combination includes a metallic casting core and a ceramic feedcore 11-13-2008
117. 20080271685 Detonative cleaning apparatus - apparatus is provided for cleaning a surface within a vessel 11-06-2008
118. 20080267769 GAS TURBINE ENGINE BLADE TIP CLEARANCE APPARATUS AND METHOD 10-30-2008
119. 20080264357 CONTROL OF DETONATIVE CLEANING APPARATUS 10-30-2008
120. 20080253885 Gas turbine engine vane - has first and second members 10-16-2008
121. 20080248300 Processes for repairing erosion resistant coatings 10-09-2008
122. 20080236244 Method for checking surface condition after cleaning 10-02-2008
123. 20080234979 Process and system for multi-objective global optimization of maintenance schedules 09-25-2008
124. 20080230156 Dual process nickel alloy crack repair - process for repairing cracks in a workpiece such as a turbine engine component comprises the steps of: 09-25-2008
125. 20080221835 Process and methodology for root cause identification in gas turbine engine performance tracking 09-11-2008
126. 20080211192 Blade outer air seal - turbine engine blade outer air seal segment has a body having a base portion 09-04-2008
127. 20080210340 REPAIR PROCESS - In accordance with the present invention, a process for repairing metal workpieces, such as turbine engine components, is provided 09-04-2008
128. 20080201008 System and method for an integrated additive manufacturing cell for complex components 08-21-2008
129. 20080199317 Local indented trailing edge heat transfer devices 08-21-2008
130. 20080198539 Avionics enclosure - enclosure for compact computer boards is described that allows a user to easily configure or reconfigure 08-21-2008
131. 20080196414 Strut cavity pilot and fuel injector assembly 08-21-2008