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Category:B64C1/06
Subcategories
This category has the following 11 subcategories, out of 11 total.
C
D
E
F
G
L
M
R
Pages in category "B64C1/06"
The following 42 pages are in this category, out of 42 total.
1
- 18063461. FLEXIBLE GROMMET ASSEMBLY simplified abstract (THE BOEING COMPANY)
- 18152204. SYSTEMS AND METHODS FOR PROTECTING SURFACES OF COMPONENTS WITHIN AN INTERNAL CABIN OF A VEHICLE simplified abstract (The Boeing Company)
- 18159170. Aircraft Cabin Seal simplified abstract (The Boeing Company)
- 18221289. CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE simplified abstract (HYUNDAI MOTOR COMPANY)
- 18221289. CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE simplified abstract (KIA CORPORATION)
- 18223916. Crash Load Distribution Structure of Fuselage simplified abstract (Hyundai Motor Company)
- 18223916. Crash Load Distribution Structure of Fuselage simplified abstract (Kia Corporation)
- 18233524. Dispersion Structure for Impact simplified abstract (HYUNDAI MOTOR COMPANY)
- 18336991. SEGMENTED VACUUM JACKETED TANK SYSTEM AND METHOD OF USING THE SAME (The Boeing Company)
- 18347042. STRUCTURAL SHAPE MODE INFLUENCERS (The Boeing Company)
- 18370187. Battery Load Support Structure of Fuselage simplified abstract (Hyundai Motor Company)
- 18370187. Battery Load Support Structure of Fuselage simplified abstract (Kia Corporation)
- 18375137. DETACHABLE BATTERY STRUCTURE OF FUSELAGE simplified abstract (Hyundai Motor Company)
- 18375137. DETACHABLE BATTERY STRUCTURE OF FUSELAGE simplified abstract (Kia Corporation)
- 18462934. CIRCUMFERENTIAL SKIN JOINTS FOR AEROSPACE STRUCTURES, METHODS OF ASSEMBLING THE JOINTS, AND METHODS OF MANUFACTURING FUSELAGE MEMBERS THAT DEFINE THE JOINTS (The Boeing Company)
- 18472598. Raised Decorative Laminate Panel and Method (The Boeing Company)
- 18516428. WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE simplified abstract (Kia Corporation)
- 18522419. AIRCRAFT WING ASSEMBLY simplified abstract (AIRBUS OPERATIONS LIMITED)
- 18551311. AIRCRAFT CABIN PORTION, AND AIRCRAFT HAVING A FLUID COLLECTOR simplified abstract (Airbus Operations GmbH)
A
- Airbus Operations GmbH (20240375760). INTERIOR MODULE WITH A COMPRESSIBLE SIDE EDGE AND METHOD OF PRODUCING AN INTERIOR MODULE simplified abstract
- Amazon technologies, inc. (20240336345). AERIAL VEHICLE AIRFRAME DESIGN AND MANUFACTURING simplified abstract
- Amazon Technologies, Inc. patent applications on October 10th, 2024
- Audio Technologies patent applications on June 6th, 2024
B
H
- Hyundai motor company (20240199189). Dispersion Structure for Impact simplified abstract
- Hyundai motor company (20240308638). CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE simplified abstract
- Hyundai motor company (20240317383). Crash Load Distribution Structure of Fuselage simplified abstract
- Hyundai motor company (20240322337). Battery Load Support Structure of Fuselage simplified abstract
- Hyundai motor company (20240336347). WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE simplified abstract
- Hyundai motor company (20240339711). DETACHABLE BATTERY STRUCTURE OF FUSELAGE simplified abstract
- HYUNDAI MOTOR COMPANY patent applications on June 20th, 2024
- Hyundai Motor Company patent applications on October 10th, 2024
- HYUNDAI MOTOR COMPANY patent applications on September 19th, 2024
- Hyundai Motor Company patent applications on September 26th, 2024
T
- The boeing company (20240418318). SEGMENTED VACUUM JACKETED TANK SYSTEM AND METHOD OF USING THE SAME
- The boeing company (20250083792). CIRCUMFERENTIAL SKIN JOINTS FOR AEROSPACE STRUCTURES, METHODS OF ASSEMBLING THE JOINTS, AND METHODS OF MANUFACTURING FUSELAGE MEMBERS THAT DEFINE THE JOINTS
- The Boeing Company patent applications on December 19th, 2024
- The Boeing Company patent applications on February 20th, 2025
- The Boeing Company patent applications on March 13th, 2025