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Category:F02C7/24
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Pages in category "F02C7/24"
The following 20 pages are in this category, out of 20 total.
1
- 17956881. GAS TURBINE ENGINE INCLUDING FLOW PATH FLEX SEAL AND HEAT SHIELD simplified abstract (Raytheon Technologies Corporation)
- 17958536. CIRCUMFERENTIALLY VARYING FAN CASING TREATMENTS FOR REDUCING FAN NOISE EFFECTS simplified abstract (GENERAL ELECTRIC COMPANY)
- 17958549. CIRCUMFERENTIALLY VARYING FAN CASING TREATMENTS FOR REDUCING FAN NOISE EFFECTS simplified abstract (General Electric Company)
- 18147861. RADIATION SHIELD FOR A GASEOUS FUEL CIRCUIT simplified abstract (General Electric Company)
- 18147874. RADIATION SHIELD FOR A GASEOUS FUEL CIRCUIT simplified abstract (General Electric Company)
- 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.)
- 18333597. THERMAL INSULATION ASSEMBLY simplified abstract (General Electric Company)
- 18625749. TURBINE ENGINE WITH SHOCKWAVE ATTENUATION simplified abstract (General Electric Company)
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- General electric company (20240247614). TURBINE ENGINE WITH SHOCKWAVE ATTENUATION simplified abstract
- General electric company (20240280054). THERMAL INSULATION ASSEMBLY simplified abstract
- General Electric Company patent applications on August 22nd, 2024
- General Electric Company patent applications on July 25th, 2024
