COMPONENT WHICH CAN BE REMOVED OR PIVOTED, FOR LINING (CLADDING) OPENINGS IN THE FUSELAGE OF AN AIRCRAFT,申请号AT19880000398-传众专利搜索

首页产品黄页商标征信

会员服务注册登录

法人/股东/高管

发明名称	COMPONENT WHICH CAN BE REMOVED OR PIVOTED, FOR LINING (CLADDING) OPENINGS IN THE FUSELAGE OF AN AIRCRAFT
摘要
申请公布号	AT390771(B)	申请公布日期	1990.06.25
申请号	AT19880000398	申请日期	1988.02.19
申请人	FISCHER GESELLSCHAFT M.B.H.	发明人
分类号	B64C1/14	主分类号	B64C1/14
代理机构		代理人
主权项
地址

您可能感兴趣的专利

Using source taint analysis to reduce false positives in an advanced persistent threat (APT) protection solution

Method and system for partitioning a verification testbench

Generating intertwined pseudo-random circuit paths referenced to an area

Automating configuration and migrating configurations of assets in a storage area network

Interleaved channels in a solid-state drive

Three-dimensional user input

Magnetically coupled waterproof hinge with integrated multi-stage button and state detection

Micro-architected materials for heat exchanger applications

Apparatus and method for configuring heliostat fields

Elastomeric, hydrogen-resistant biopolymer and its use in oil and gas refining, and in the storage and transport of hydrogen gas

Interlock braking system

Multi-grade aluminum laser welded clutch components

Thermal release of a self-opening cover

System and method of constructing a composite assembly

Control system for work vehicle, control method, and work vehicle

Case made from dissimilar materials

Paint can rim cover

Method and system for making an alpaca bonded fiber pad

Skateboard assembly including a fluid-filled chamber

Adaptable buckle system