Flight unit control system, flight control device

专利名称：Flight unit control system, flight control

device including such a system, and use ofsuch a system

发明人：Franck Bouillot,Cédric Milord申请号：US13101369申请日：20110505公开号：US08820172B2公开日：20140902

专利附图：

摘要：A flight unit control system having at least one instrumented fastening boltconnecting an aircraft carrier structure and a load path, the instrumented bolt having at

least one measurement area for detecting that the load path is under load and includinga fastener for locking the instrumented bolt in a position relative to the aircraft carrierstructure and load path and wherein the measurement area has two cavities and at leastone strain gauge and wherein the fastener includes a plate which is positioned at athreaded end of the instrumented bolt which bears against one of the aircraft carrierstructure and the load path and which extends perpendicularly to an axis of the bolt anda nut which is placed at the threaded end of the instrumented bolt to immobilize theinstrumented bolt relative to the aircraft structure or the load path.

申请人：Franck Bouillot,Cédric Milord

地址：Valence FR,Marches FR

国籍：FR,FR

代理机构：Dowell & Dowell PC

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