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 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...
WING-FUSELAGE SECTION OF AN AIRCRAFT 专利名称：WING-FUSELAGE SECTION OF AN AIRCRAFT 发明人：PAHL, Günter 申请号：EP2008054820 申请日：20080421 公开号：WO08/132087P1 公开日：20081106 专利内容由知识产权出版社提供 摘要：A wing-fuselage section of an aircraft, which wing-fuselage section comprises a...
Fuselage of an old military amphibious aircraft,站酷海洛,一站式正版视觉内容平台,站酷旗下品牌.授权内容包含正版商业图片、艺术插画、矢量、视频、音乐素材、字体等,已先后为阿里巴巴、京东、亚马逊、小米、联想、奥美、盛世长城、百度、360、招商银行、工商银行等数万
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
Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position The turbojet according to the invention is designed to be fixed onto the upper part of the aft section of the fuselage of an aircraft using at least one coat hanger, the turbojet comprising...
The cracks at the joint bolt for the wing and fuselage of an aircraft were observed,when the aircraft was experienced a field maintenance,as a result of analyzing the relevant macroscopic and microscopic features of the fracture,measuring the change of chemical compositions around cracks,as well as...
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....