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Category:F01D5/28
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This category has the following 45 subcategories, out of 45 total.
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Pages in category "F01D5/28"
The following 77 pages are in this category, out of 77 total.
1
- 17973085. EROSION-SHIELDED TURBINE BLADES AND METHODS OF MANUFACTURING THE SAME simplified abstract (GENERAL ELECTRIC COMPANY)
- 18071060. MACHINABLE COATING FOR CMC AND METAL INTERFACE IN A TURBINE SECTION simplified abstract (Raytheon Technologies Corporation)
- 18088957. COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION simplified abstract (GENERAL ELECTRIC COMPANY)
- 18088990. COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION simplified abstract (GENERAL ELECTRIC COMPANY)
- 18104452. COMPONENT WITH SPAR ASSEMBLY FOR A TURBINE ENGINE simplified abstract (GENERAL ELECTRIC COMPANY)
- 18131696. MACHINABLE COATING WITH ENVIRONMENTAL BARRIER PROPERTIES simplified abstract (Raytheon Technologies Corporation)
- 18171533. TURBINE ENGINE WITH COMPOSITE AIRFOILS simplified abstract (General Electric Company)
- 18171938. TURBINE ENGINE AIRFOIL WITH A WOVEN CORE AND WOVEN LAYER simplified abstract (General Electric Company)
- 18172723. TURBINE ENGINE WITH A BLADE HAVING WOVEN CORE AND TOUGHENED REGION simplified abstract (General Electric Company)
- 18182559. TURBINE ENGINE AIRFOIL WITH A WOVEN CORE simplified abstract (General Electric Company)
- 18221677. SPRAY NOZZLE DEVICE FOR DELIVERING A RESTORATIVE COATING THROUGH A HOLE IN A CASE OF A TURBINE ENGINE simplified abstract (General Electric Company)
- 18236263. LOCALIZED THICKENING PLY REINFORCEMENT WITHIN CERAMIC MATRIX COMPOSITE AIRFOIL CAVITY (RTX Corporation)
- 18296633. METHOD FOR MANUFACTURING MULTIPLE SEAL ARC SEGMENTS simplified abstract (Raytheon Technologies Corporation)
- 18298409. WEAR RESISTANT ARTICLE AND METHOD OF MAKING simplified abstract (GENERAL ELECTRIC COMPANY)
- 18317310. COMPOSITE AIRFOIL ASSEMBLIES AND METHOD FOR MANUFACTURING THE SAME simplified abstract (General Electric Company)
- 18333743. A COMPOSITE AIRFOIL ASSEMBLY AND METHOD OF FORMING A COMPOSITE AIRFOIL ASSEMBLY (General Electric Company)
- 18336933. REPAIR PROCESS USING PLASMA ETCHING (Raytheon Technologies Corporation)
- 18348438. COMPOSITE AIRFOIL ASSEMBLY FOR A TURBINE ENGINE (General Electric Company)
- 18364875. COATED ARTICLE FOR HOT HYDROCARBON FLUID AND METHOD OF PREVENTING FUEL THERMAL DEGRADATION DEPOSITS simplified abstract (General Electric Company)
- 18377080. COOLING PASSAGE EXIT OPENING CROSS-SECTIONAL AREA REDUCTION FOR TURBINE SYSTEM COMPONENT simplified abstract (GENERAL ELECTRIC COMPANY)
- 18418909. TURBOMACHINE COOLING TRENCH simplified abstract (GENERAL ELECTRIC COMPANY)
- 18452901. CMC VANE WITH ROTATABLE BAFFLE DESIGN TO ACCOMMODATE RE-STAGGER (RTX Corporation)
- 18452912. BATHTUB SEAL INTEGRATED INTO CMC VANE LOAD PATH (RTX Corporation)
- 18453564. COMPOSITE COMPONENT HAVING AN ADDITIVELY PRINTED INNER PORTION (General Electric Company)
- 18454365. AMORPHOUS DUCTILE BRAZE ALLOY COMPOSITIONS, AND RELATED METHODS AND ARTICLES simplified abstract (General Electric Company)
- 18455265. RADIAL SEAL BETWEEN CMC VANE AND VANE SUPPORT (RTX Corporation)
- 18455293. TILTED CMC VANE ARC SEGMENT (RTX Corporation)
- 18455308. CMC VANE ARC SEGMENTS WITH FRICTION DAMPER (RTX Corporation)
- 18456159. CMC VANE WITH DETUNED PLATFORM (RTX Corporation)
- 18468189. TURBINE ENGINE INCLUDING A GAS PATH COMPONENT HAVING A HYDROPHOBIC COATING (General Electric Company)
- 18480692. CMC AIRFOIL WITH CIRCUMVENTING COOLING PASSAGE (RTX Corporation)
- 18483581. METHOD OF FORMING COMPOSITE COMPONENTS WITH CAVITIES (General Electric Company)
- 18485103. EROSION COMPENSATED VANE GEOMETRY (RTX Corporation)
- 18489533. TURBINE ENGINE WITH A PRIMARY STAGE OF AIRFOILS AND A SUBSIDIARY STAGE OF AIRFOILS (General Electric Company)
- 18496267. CMC Airfoil with Closed-Circuit Cooling Passage in Platform (RTX CORPORATION)
- 18586711. COATING SYSTEMS INCLUDING INFILTRATION COATINGS AND REACTIVE PHASE SPRAY FORMULATION COATINGS simplified abstract (General Electric Company)
- 18602946. CMAS-RESISTANT BARRIER COATINGS simplified abstract (ROLLS-ROYCE plc)
- 18672309. BATHTUB SEAL FOR DAMPING CMC VANE PLATFORM (RTX Corporation)
- 18722026. CMC MATERIALS WITH INTEGRATED THERMOCOUPLE (SAFRAN)
- 18746851. DISCRETE MACROSCOPIC METAMATERIAL SYSTEMS simplified abstract (Massachusetts Institute of Technology)
- 18835233. HYBRID METAL/COMPOSITE BLADE WITH TEXTILE ORIENTATION ADAPTED TO MECHANICAL STRESSES (SAFRAN AIRCRAFT ENGINES)
- 18888810. Internal Aluminization of Coated Substrates (RTX Corporation)
- 18966717. TURBINE ENGINE WITH A BLADE HAVING WOVEN CORE AND TOUGHENED REGION (General Electric Company)
- 18973613. ALUMINUM-CHROMIUM OXIDE COATING AND METHOD THEREFOR (RTX Corporation)
- 18987428. METHOD OF FORMING A COMPOSITE AIRFOIL ASSEMBLY (General Electric Company)
- 19000468. Multi-Zone Blade Fabrication (RTX CORPORATION)
- 19013045. TURBINE INCORPORATING SPLITTERS (General Electric Company)
2
- 20240018873. METHOD FOR MANUFACTURING A COMPOSITE GUIDE VANE HAVING A METALLIC LEADING EDGE simplified abstract (Pratt & Whitney Canada Corp.)
- 20240044254. AIRFOIL ASSEMBLY WITH AN INTERNAL REINFORCEMENT STRUCTURE simplified abstract (General Electric Company)
- 20240044256. INTERNAL ALUMINIDE COATING FOR VANES AND BLADES AND METHOD OF MANUFACTURE simplified abstract (RTX Corporation)
3
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- General electric company (20240247378). COATING SYSTEMS INCLUDING INFILTRATION COATINGS AND REACTIVE PHASE SPRAY FORMULATION COATINGS simplified abstract
- General electric company (20240280024). TURBINE ENGINE WITH COMPOSITE AIRFOILS simplified abstract
- General electric company (20240280026). TURBINE ENGINE WITH A BLADE HAVING WOVEN CORE AND TOUGHENED REGION simplified abstract
- General electric company (20240280027). TURBINE ENGINE AIRFOIL WITH A WOVEN CORE AND WOVEN LAYER simplified abstract
- General Electric Company patent applications on August 22nd, 2024
- General Electric Company patent applications on July 25th, 2024
R
- Rtx corporation (20250067182). BATHTUB SEAL INTEGRATED INTO CMC VANE LOAD PATH
- Rtx corporation (20250067183). BATHTUB SEAL FOR DAMPING CMC VANE PLATFORM
- Rtx corporation (20250067184). LOCALIZED THICKENING PLY REINFORCEMENT WITHIN CERAMIC MATRIX COMPOSITE AIRFOIL CAVITY
- Rtx corporation (20250067185). CMC VANE WITH ROTATABLE BAFFLE DESIGN TO ACCOMMODATE RE-STAGGER
- Rtx corporation (20250067187). RADIAL SEAL BETWEEN CMC VANE AND VANE SUPPORT
- Rtx corporation (20250067188). TILTED CMC VANE ARC SEGMENT
- Rtx corporation (20250067189). CMC VANE ARC SEGMENTS WITH FRICTION DAMPER
- Rtx corporation (20250067190). CMC VANE WITH DETUNED PLATFORM
- RTX Corporation patent applications on February 27th, 2025