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Category:CPC F01D9/041
Pages in category "CPC F01D9/041"
The following 27 pages are in this category, out of 27 total.
1
- 17970918. TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER simplified abstract (GENERAL ELECTRIC COMPANY)
- 18086112. OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE simplified abstract (GENERAL ELECTRIC COMPANY)
- 18334799. GAS TURBINE ENGINE HAVING OUTLET GUIDE VANES (General Electric Company)
- 18335591. Circumferential Row of Vanes for a Gas Turbine Engine and Having Non-Uniform Vane Spacing (General Electric Company)
- 18357410. GAS TURBINE ENGINE DEFINING A ROTOR CAVITY (General Electric Company)
- 18467846. INSTRUMENTED STATOR WITH EXTENDED INTERNAL PASSAGES (RTX Corporation)
- 18603682. STEAM TURBINE simplified abstract (MITSUBISHI HEAVY INDUSTRIES, LTD.)
- 18674010. OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE simplified abstract (General Electric Company)
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- RAYTHEON TECHNOLOGIES CORPORATION Patent Application Trends in 2024
- Raytheon Technologies Corporation Patent Application Trends in 2025
- RAYTHEON TECHNOLOGIES CORPORATION Patent Application Trends in 2025
- Rolls-Royce North American Technologies Inc. Patent Application Trends in 2025
- Rolls-Royce plc Patent Application Trends in 2024
- ROLLS-ROYCE PLC Patent Application Trends in 2024
- RTX Corporation Patent Application Trends in 2024