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Category:B64D33/02
Subcategories
This category has the following 22 subcategories, out of 22 total.
B
C
D
E
H
J
K
M
R
S
V
Pages in category "B64D33/02"
The following 26 pages are in this category, out of 26 total.
1
- 18171554. Inlet Outer Barrel Segmented Attach Flange simplified abstract (The Boeing Company)
- 18211075. AIRCRAFT AIR SYSTEM WITH DEDICATED COMPRESSOR(S) (PRATT & WHITNEY CANADA CORP.)
- 18243480. AIRCRAFT ENGINE ASSEMBLY FOR CONTROLLING ENGINE OIL FLOW DURING FIRE CONDITIONS AND METHOD FOR USING SAME (PRATT & WHITNEY CANADA CORP.)
- 18377186. CIRCUMFERENTIALLY TAILORED INLET GUARD FOR AN AIRCRAFT ENGINE INLET (Pratt & Whitney Canada Corp.)
- 18393851. ICE PROTECTION SYSTEM FOR AN AIRCRAFT (THE BOEING COMPANY)
- 18413303. SYSTEM AND METHOD FOR FORMING A COMPONENT (THE BOEING COMPANY)
- 18481737. VARIABLE INLET GUARD SCREEN FOR AN INLET OF AN AIRCRAFT ENGINE (Pratt & Whitney Canada Corp.)
- 18942928. ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE (General Electric Company)
2
B
T
- The boeing company (20240253800). VARIABLE COMPRESSION AIR INTAKES FOR AIRCRAFT PROPULSION SYSTEMS AND METHODS FOR VARYING COMPRESSION OF AN AIR INTAKE simplified abstract
- The boeing company (20240278924). Inlet Outer Barrel Segmented Attach Flange simplified abstract
- The boeing company (20240295363). HEAT TRANSFER DEVICE WITH NESTED LAYERS OF HELICAL FLUID CHANNELS simplified abstract
- The boeing company (20250108929). Two Piece Nested Air Intake Scoop for Engine Cowl
- The boeing company (20250121534). SYSTEM AND METHOD FOR FORMING A COMPONENT
- The boeing company (20250121943). ICE PROTECTION SYSTEM FOR AN AIRCRAFT
- THE BOEING COMPANY patent applications on April 17th, 2025
- The Boeing Company patent applications on April 3rd, 2025
- THE BOEING COMPANY patent applications on August 1st, 2024
- The Boeing Company patent applications on August 22nd, 2024
- The Boeing Company patent applications on September 5th, 2024