发明名称 Tertiary locking assembly for a thrust reverser
摘要 A tertiary locking assembly for a thrust reverser includes a tertiary lock, a primary control line associated with the tertiary lock, and a secondary control line. The primary control line includes a primary electromechanical valve and a primary power supply line connected to the primary electromechanical valve. In addition, the secondary control line has a secondary electromechanical control valve and a secondary power supply line connected to the secondary electromechanical control valve. In particular, the secondary control line is provided with at least one manually controlled switch.
申请公布号 US9458794(B2) 申请公布日期 2016.10.04
申请号 US201314060823 申请日期 2013.10.23
申请人 AIRCELLE 发明人 Hue Corentin;Lerouvreur Mathieu
分类号 F02K1/76;F01D5/00;H01H50/32;H01H3/40;H01H3/42 主分类号 F02K1/76
代理机构 Burris Law, PLLC 代理人 Burris Law, PLLC
主权项 1. A thrust reverser in a nacelle of a turbojet engine comprising a tertiary locking assembly, said tertiary locking assembly comprising: at least one tertiary lock; at least one primary control line associated with the at least one tertiary lock, the at least one primary control line comprising at least one primary electromechanical control means and a primary power supply line connected to said at least one primary electromechanical control means; and at least one secondary control line associated with the at least one tertiary lock, said at least one secondary control line comprising at least one secondary electromechanical control means and a secondary power supply line which is connected to the at least one secondary electromechanical control means and which is separate from the primary power supply line of the at least one primary control line, wherein said at least one secondary control line is provided with at least one manually controlled switch.
地址 Gonfreville l'Orcher unknown