Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising two upper lugs, two lower lugs and a detachable balancer fitting. The balancer fitting...
The central body of an aircraft, to which the wings and tail assembly are attached and which accommodates the crew, passengers, and cargo. [French, fromfuselé,spindle-shaped, from Old Frenchfusel,spindle, from Vulgar Latin*fūsellus, diminutive of Latinfūsus.] ...
A container assembly and aircraft fuselage for air transport of freight. The container assembly includes a spacer layer formed of malleable material. The spacer layer is positioned between and in contact with a bottom plate of the container and the floor of an aircraft. The aircraft fuselage for...
The invention relates to a portion (200) of a fuselage of an aircraft having a longitudinal axis (10), said portion (200) having a ventral beam (206) and a rear lower shell (208), each being made of composite materials of the type comprising fibers (250) and including a portion of ...
The internal wall such as the rear wall in the passenger compartment of a commercial aircraft, and separating compartments which are under different pressure, is rendered safe by providing a wall capturing net on the low pressure side of the wall and fastening that net to the fuselage proper.收...
The present invention relates to an aircraft provided with at least one fixing device of a support member (9) to the fuselage (8) which includes the resilient joints (1) whose rigidity in translation and rotation can be parameterized axially (x), vertically (z) and crosswise (y). In parti...
An aircraft defining a longitudinal direction and a lateral direction is provided. The aircraft includes a fuselage; an engine mounted at a location spaced from the fuselage of the
A foreign object deflector for installation on the lower fuselage of an aircraft forward of equipment, such as antennas and radomes, which are to be protected by the deflector. During takeoff and landing, aircraft landing gear kick up various foreign objects, such as rocks, dirt and debris, ...
A wing/fuselage connection for an aircraft, in which a wing (2) which is arranged in the upper area of the fuselage (1) is connected to the fuselage (1) by means of a number of connections (3, 4, 5, 6) with the connections (3, 4, 5, 6) being intended to absorb forces in ...
United States Patent US3848831 Note: If you have problems viewing the PDF, please make sure you have the latest version of Adobe Acrobat. Back to full textHome Search Services Contact us © 2004-2024 FreePatentsOnline.com. All rights reserved. Privacy Policy & Terms of Use....