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Category:F02C6/20
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Pages in category "F02C6/20"
The following 16 pages are in this category, out of 16 total.
1
- 17932748. PROPELLER SHAFT ASSEMBLY FOR AIRCRAFT ENGINE simplified abstract (PRATT & WHITNEY CANADA CORP.)
- 18181159. COMPONENTS HAVING COATING SYSTEMS DEFINED BY TILES SECURED THERETO, METHODS OF PRODUCING THE COMPONENTS, AND AIRCRAFT COMPRISING THE COMPONENTS simplified abstract (Honeywell International Inc.)
- 18337491. GAS TURBINE ENGINE simplified abstract (ROLLS-ROYCE plc)
- 18455137. Object Direction Mechanism for Turbofan Engine simplified abstract (GENERAL ELECTRIC COMPANY)
- 18513916. Propulsion System for an Aircraft simplified abstract (GENERAL ELECTRIC COMPANY)
- 18817394. GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY (General Electric Company)
