发明名称 ANGLE OF ATTACK DISPLAY
摘要 An aircraft safety system includes a Stall/Spin Warning & Recovery Computer, an angle of attack sensor, a side slip sensor and an angle of attack display. The Stall/Spin Warning and Recovery Computer detects whether the aircraft is in a safe condition or an unsafe condition. The angle of attack display includes a first configuration that displays information indicative of safe aircraft condition when the orientation detector detects a safe condition and a second configuration that displays information indicative of unsafe aircraft condition when the computer detects an unsafe condition. The display may transition from the first configuration to the second configuration when the orientation detector detects an unsafe condition and then to a third configuration, which may include visual control-input instructions that enable recovery to a safe condition.
申请公布号 US2015084792(A1) 申请公布日期 2015.03.26
申请号 US201314032840 申请日期 2013.09.20
申请人 Safe Flight Instrument Corporation 发明人 BARTH Arthur C.;GREENE Randall A.;SIMONS Louis;TAILLIE Darren
分类号 B64D43/02 主分类号 B64D43/02
代理机构 代理人
主权项 1. An aircraft angle of attack display, comprising: a first configuration that displays information indicative of safe aircraft condition, a second configuration that displays information indicative of unsafe aircraft condition, and a third configuration that provides visual control-input instructions to a pilot when the condition deteriorates further.
地址 White Plains NY US