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Category:F01D25/00
Subcategories
This category has the following 12 subcategories, out of 12 total.
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F
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Pages in category "F01D25/00"
The following 16 pages are in this category, out of 16 total.
1
- 18070978. REMOVABLE LAYER TO ADJUST MOUNT STRUCTURE OF A TURBINE VANE FOR RE-STAGGER simplified abstract (Raytheon Technologies Corporation)
- 18278991. TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT simplified abstract (SAFRAN AIRCRAFT ENGINES)
- 18337841. AIRFOIL FOR A TURBINE ENGINE simplified abstract (General Electric Company)
- 18377390. MULTI-PHASE RADIATIVE AND THERMAL BARRIER COATING SYSTEM (RTX Corporation)
- 18454365. AMORPHOUS DUCTILE BRAZE ALLOY COMPOSITIONS, AND RELATED METHODS AND ARTICLES simplified abstract (General Electric Company)
- 18465259. THERMAL SPRAY POWDER AND COATED ARTICLE (RTX CORPORATION)
- 18468189. TURBINE ENGINE INCLUDING A GAS PATH COMPONENT HAVING A HYDROPHOBIC COATING (General Electric Company)
- 18495803. METAL COUPON WITH POROUS REGION FOR COMPONENT AND COMPONENT WITH SAME (GE Infrastructure Technology LLC)
- 18495809. POROUS METAL COUPON WITH CONDUIT FOR REPAIRING COMPONENT, COMPONENT WITH SAME AND RELATED METHOD (GE Infrastructure Technology LLC)
- 18495810. POROUS METAL COUPON WITH THERMAL TRANSFER STRUCTURE FOR COMPONENT AND RELATED COMPONENT (GE Infrastructure Technology LLC)
- 18594065. PASSIVE CONTROL OF GAS TURBINE CLEARANCES USING CERAMIC MATRIX COMPOSITES INSERTS simplified abstract (General Electric Company)
- 18835233. HYBRID METAL/COMPOSITE BLADE WITH TEXTILE ORIENTATION ADAPTED TO MECHANICAL STRESSES (SAFRAN AIRCRAFT ENGINES)
- 18973613. ALUMINUM-CHROMIUM OXIDE COATING AND METHOD THEREFOR (RTX Corporation)