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Category:F02C7/232
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This category has the following 15 subcategories, out of 15 total.
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Pages in category "F02C7/232"
The following 18 pages are in this category, out of 18 total.
1
- 17805986. MULTI-TEMPERATURE FUEL INJECTORS FOR A GAS TURBINE ENGINE simplified abstract (General Electric Company)
- 17836681. MONITORING SYSTEMS FOR HYDROGEN FUELED AIRCRAFT simplified abstract (General Electric Company)
- 17959400. HYDROGEN FUEL SYSTEM FOR A VEHICLE simplified abstract (GENERAL ELECTRIC COMPANY)
- 18054177. GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES simplified abstract (Honeywell International Inc.)
- 18092106. SYSTEM AND METHOD HAVING FLUID INJECTORS FOR ISOTHERMAL EXPANSION IN TURBINE STAGE OF GAS TURBINE ENGINE simplified abstract (General Electric Company)
- 18244362. ENGINE AUGMENTOR FUEL PUMPS POWERED BY AUXILIARY POWER UNIT (APU) (Hamilton Sundstrand Corporation)
- 18337531. AIRCRAFT FUEL SYSTEM simplified abstract (ROLLS-ROYCE plc)
- 18337699. CONTROL OF FUEL TEMPERATURE simplified abstract (ROLLS-ROYCE plc)
- 18469187. GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR (General Electric Company)
- 18936280. OVER-PRESSURE VENT SYSTEM FOR AN AIRCRAFT FUEL TANK (THE BOEING COMPANY)
- 18977350. REGENERATIVE FUEL HEATING SYSTEM (GENERAL ELECTRIC COMPANY)