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Method and a device for performing a check on the state of health of a turbine engine of a twin-engined rotorcraft

机译：用于检查双引擎旋翼飞机的涡轮发动机的健康状态的方法和装置

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摘要

The present invention relates to a method and to a device (D) enabling a health check to be performed on at least a first turbine engine (M1) of a rotorcraft, the rotorcraft being provided with first and second turbine engines (M1 and M2) controlled respectively by first and second control means (MC1 and MC2). The device is remarkable in that it comprises check means (C) provided with main means (C1), the main means (C1) controlling the first and second control means (MC1 and MC2) so that the surveillance parameters of the first and second turbine engines (M1 and M2) respectively reach the real first and second final values (V1f and V2f) as determined in accordance with the method of the invention.

机译：本发明涉及一种能够对旋翼飞机的至少第一涡轮发动机（M 1 ）执行健康检查的方法和装置（D），该旋翼飞机具有第一和第二实施方式。第一和第二控制装置（MC 1 和MC 2 1 和M 2 ） B>）。该装置的显着之处在于，它包括具有主装置（C 1 ）的检查装置（C），主装置（C 1 ）控制第一和第二控制装置（MC 1 和MC 2 ），以便第一和第二涡轮发动机的监视参数（M 1 和M 2 < / B>）分别达到实际的第一和第二最终值（V 1 f 和V 2 f ）根据本发明的方法确定。 展开▼

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公开/公告号US7769521B2

专利类型

公开/公告日2010-08-03

原文格式PDF

申请/专利权人 FRANCOIS-XAVIER GAULMIN;LIONEL IRAUDO;
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申请/专利号US20070730835

发明设计人 FRANCOIS-XAVIER GAULMIN;LIONEL IRAUDO;
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申请日2007-04-04

分类号G06F19/00;G06G7/70;

国家 US

入库时间 2022-08-21 18:48:56

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