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Category:F02C7/36
Subcategories
This category has the following 16 subcategories, out of 16 total.
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F
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Pages in category "F02C7/36"
The following 55 pages are in this category, out of 55 total.
1
- 17806574. DIFFERENTIAL GEARBOX ASSEMBLY FOR A TURBINE ENGINE simplified abstract (General Electric Company)
- 17959336. SHAFT COUPLING FOR A GAS TURBINE ENGINE simplified abstract (GENERAL ELECTRIC COMPANY)
- 17987299. GAS TURBINE ENGINE WITH THIRD STREAM simplified abstract (General Electric Company)
- 18085728. ELECTRIC MACHINE ASSEMBLY simplified abstract (GENERAL ELECTRIC COMPANY)
- 18243346. DUAL BYPASS TURBOFAN GAS TURBINE ENGINE (PRATT & WHITNEY CANADA CORP.)
- 18337519. AIRCRAFT HEAT MANAGEMENT simplified abstract (ROLLS-ROYCE plc)
- 18337546. COMBUSTION OF FUEL simplified abstract (ROLLS-ROYCE plc)
- 18348649. Midshaft Rating for Turbomachine Engines simplified abstract (GENERAL ELECTRIC COMPANY)
- 18370515. FAN DRIVE GEAR SYSTEM ROTATING OIL BAFFLE (RTX Corporation)
- 18372493. AIR INTAKE FOR AN AIRCRAFT PROPULSION SYSTEM ENGINE ASSEMBLY (PRATT & WHITNEY CANADA CORP.)
- 18400762. DIFFERENTIAL GEARBOX ASSEMBLY FOR A TURBINE ENGINE simplified abstract (GENERAL ELECTRIC COMPANY)
- 18406967. POWER TRANSFER SYSTEMS AND METHODS FOR AIRCRAFT ENGINES simplified abstract (The Boeing Company)
- 18430269. TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract (General Electric Company)
- 18430283. TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract (General Electric Company)
- 18430317. TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract (General Electric Company)
- 18481597. MIDSHAFT RATING FOR TURBOMACHINE ENGINES simplified abstract (General Electric Company)
- 18486523. MIDSHAFT RATING FOR TURBOMACHINE ENGINES simplified abstract (General Electric Company)
- 18561811. TURBOMACHINE COMPRISING A REAR INTEGRATED ELECTRICAL MACHINE simplified abstract (SAFRAN AIRCRAFT ENGINES)
- 18580890. SLEEVE MOUNTED ONTO A LOW-PRESSURE SHAFT IN A TURBOMACHINE simplified abstract (SAFRAN AIRCRAFT ENGINES)
- 18649822. TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract (General Electric Company)
- 18671084. SYSTEM AND METHOD FOR DETECTING AND REDUCING TORQUE IN A TURBINE ENGINE (General Electric Company)
- 18695477. MODULE FOR AN AIRCRAFT TURBINE ENGINE (SAFRAN AIRCRAFT ENGINES)
- 18817394. GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY (General Electric Company)
- 18959834. GAS TURBINE ENGINE BEARING AND GEARBOX ARRANGEMENT (RTX CORPORATION)
- 18990397. REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE (General Electric Company)
- 18990439. REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE (General Electric Company)
- 18990617. GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO (General Electric Company)
- 18990685. GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO (General Electric Company)
- 18990706. GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO (General Electric Company)
2
B
G
- General electric company (20240280055). TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract
- General electric company (20240280056). TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract
- General electric company (20240280057). TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract
- General electric company (20240280058). TURBOMACHINERY ENGINES WITH HIGH-SPEED LOW-PRESSURE TURBINES simplified abstract
- General electric company (20250122830). REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
- General electric company (20250122831). REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
- General electric company (20250122835). GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO
- General electric company (20250122836). GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO
- General electric company (20250122842). GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO
- General Electric Company patent applications on April 17th, 2025
- General Electric Company patent applications on August 22nd, 2024
- General Electric Company patent applications on February 6th, 2025
R
U
- US Patent Application 18107126. GAS TURBINE ENGINE WITH POWER DENSITY RANGE simplified abstract
- US Patent Application 18202727. SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM simplified abstract
- US Patent Application 18202734. SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM simplified abstract
- US Patent Application 18202736. SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM simplified abstract