专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

61. 发明授权

US08359129B2 Method and device for controlling the thrust of a multi-engine aircraft 有权
标题翻译：用于控制多发飞机的推力的方法和装置
公开(公告)号：US08359129B2
公开(公告)日：2013-01-22
申请号：US12162774
申请日：2007-03-08
申请人： Benoît Lemaignan , Gérard Mathieu
发明人： Benoît Lemaignan , Gérard Mathieu
IPC分类号： G05D1/00
CPC分类号： G05D1/0072 , B64D31/10
摘要： A method and device control the thrust of a multi-engine aircraft. At least one engine command is determined by a command determining unit, with the determined command commanding each engine that has not failed to deliver a thrust substantially equal to a reduced thrust value. A command application unit is configured to apply the determined command to each aircraft engine that has not failed. The reduced thrust value is determined, by a weight determining device, according to the current weight of the aircraft and according to a reduced thrust value FOEI, which is calculated by a thrust calculation unit.
摘要翻译：一种方法和装置控制多发飞机的推力。由命令确定单元确定至少一个发动机命令，其中所确定的命令命令每个发动机未失效地将推力基本上等于减小的推力值。命令应用单元被配置为将所确定的命令应用于未失败的每个飞机引擎。减重推力值由重量确定装置根据飞行器的当前重量并根据由推力计算单元计算的减小的推力值FOEI来确定。

62. 发明申请

US20090320445A1 METHOD AND DEVICE FOR THE DETECTION OF A THRUST DISSYMMETRY OF AN AIRCRAFT DURING A BRAKING 失效
标题翻译：用于在制动期间检测飞机的扭矩差速比的方法和装置
公开(公告)号：US20090320445A1
公开(公告)日：2009-12-31
申请号：US12493094
申请日：2009-06-26
申请人： Alain Dupre
发明人： Alain Dupre
IPC分类号： F02K1/54 , G01L5/12
CPC分类号： B64D31/12 , B64D31/10
摘要： According to the invention, under braking of an aircraft (AC) with reverse thrust, that (those) engine(s) (Mc) of said aircraft (AC) the associated control lever (4c) of which is (are) not in a reverse thrust position (I) is (are) set to low idle speed.
摘要翻译：根据本发明，在具有反向推力的飞行器（AC）的制动下，所述飞行器（AC）的那些（一个或多个）发动机（Mc）的相关控制杆（4c）不在反推力位置（I）被设定为低怠速。

63. 发明授权

US4143839A Apparatus for combating rolling movements of aircraft 失效
标题翻译：用于对付飞机滚动运动的装置
公开(公告)号：US4143839A
公开(公告)日：1979-03-13
申请号：US828765
申请日：1977-08-29
申请人： Oleg K. Antonov , Valentin T. Maslov , Alexei F. Voitko
发明人： Oleg K. Antonov , Valentin T. Maslov , Alexei F. Voitko
IPC分类号： B64D31/10 , B64C13/16
CPC分类号： B64D31/10
摘要： The apparatus operates to prevent the rolling of an aircraft having an even number of propulsion units when one of the propulsion units stops operating due to a breakdown. Spoilers are mounted on the outboard wings. Each spoiler has an individual drive connected to a power circuit via a control valve which, in turn, is functionally associated with a failure detector of the propulsion unit disposed on the outboard wing opposite to that on which the respective spoiler is mounted. The apparatus is provided with an apparatus that is brought into action automatically, so as to counteract the rolling tendency of an aircraft when one of its propulsion units fails, or with a manual control for correcting the glidepath during landing, dissipating the lift and applying the aerodynamic braking during the landing roll.
摘要翻译：当其中一个推进单元由于击穿而停止运行时，该装置用于防止具有偶数个推进单元的飞行器的滚动。飞镖安装在外侧翼上。每个扰流器具有通过控制阀连接到电力回路的单独驱动器，该控制阀又与设置在与安装相应扰流器的外侧翼上的外侧翼上的推进单元的故障检测器功能相关联。该装置具有自动启动的装置，以抵消当其推进装置之一发生故障时飞机的滚动倾向，或用于在着陆期间校正滑行道的手动控制，消散电梯和施加着陆卷期间的空气动力学制动。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式