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公开(公告)号：EP2113459B1
公开(公告)日：2018-06-06
申请号：EP09158283.3
申请日：2009-04-20
发明人： Robbins, Robert , Gomuc, Reha , Kowal, Adam , Schmittenberg, Marc , Harper, Steve , Reese, Larry , Brett, Tony , Doras, Vincent
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213
摘要： An inlet door system (109) including an aft inlet duct mounted door actuator providing RAM air to an auxiliary power unit (APU) (110) contained within an aircraft is provided. The inlet door system includes an inlet duct (120), the aft inlet duct mounted door actuator (134), and a door (130). The inlet duct (120) is configured to extend from the auxiliary power unit (110) to the aircraft housing and has a sidewall (126) that defines a flow passage. The door actuator (134) is mounted to an exterior surface of the aft portion of the inlet duct (120). The door (130) is coupled to the actuator (134). The actuator (134) is configured to selectively rotate the door (130) between at least a first position and a second position.
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公开(公告)号：EP2113459A3
公开(公告)日：2015-12-02
申请号：EP09158283.3
申请日：2009-04-20
发明人： Robbins, Robert , Gomuc, Reha , Kowal, Adam , Schmittenberg, Marc , Harper, Steve , Reese, Larry , Brett, Tony , Doras, Vincent
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213
摘要： An inlet door system (109) including an aft inlet duct mounted door actuator providing RAM air to an auxiliary power unit (APU) (110) contained within an aircraft is provided. The inlet door system includes an inlet duct (120), the aft inlet duct mounted door actuator (134), and a door (130). The inlet duct (120) is configured to extend from the auxiliary power unit (110) to the aircraft housing and has a sidewall (126) that defines a flow passage. The door actuator (134) is mounted to an exterior surface of the aft portion of the inlet duct (120). The door (130) is coupled to the actuator (134). The actuator (134) is configured to selectively rotate the door (130) between at least a first position and a second position.
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公开(公告)号：EP2113459A2
公开(公告)日：2009-11-04
申请号：EP09158283.3
申请日：2009-04-20
发明人： Robbins, Robert , Gomuc, Reha , Kowal, Adam , Schmittenberg, Marc , Harper, Steve , Reese, Larry , Brett, Tony , Doras, Vincent
CPC分类号： B64D41/00 , B64D33/02 , B64D2033/0213
摘要： An inlet door system (109) including an aft inlet duct mounted door actuator providing RAM air to an auxiliary power unit (APU) (110) contained within an aircraft is provided. The inlet door system includes an inlet duct (120), the aft inlet duct mounted door actuator (134), and a door (130). The inlet duct (120) is configured to extend from the auxiliary power unit (110) to the aircraft housing and has a sidewall (126) that defines a flow passage. The door actuator (134) is mounted to an exterior surface of the aft portion of the inlet duct (120). The door (130) is coupled to the actuator (134). The actuator (134) is configured to selectively rotate the door (130) between at least a first position and a second position.
摘要翻译： 提供了一种入口门系统（109），其包括向包含在飞行器内的辅助动力单元（APU）（110）提供RAM空气的后进入管道安装的门致动器。 入口门系统包括入口管道（120），后进入管道安装的门致动器（134）和门（130）。 入口管道（120）构造成从辅助动力单元（110）延伸到飞行器壳体并且具有限定流动通道的侧壁（126）。 门致动器（134）安装到入口管道（120）的后部的外表面。 门（130）联接到致动器（134）。 致动器（134）构造成在至少第一位置和第二位置之间选择性地旋转门（130）。
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