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公开(公告)号：WO2014007875A2
公开(公告)日：2014-01-09
申请号：PCT/US2013033172
申请日：2013-03-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： CHARRON MICHAEL N , LUCAS JAMES L
Abstract: A gas turbine engine thrust reverser system includes a fan nacelle having a fixed portion and a movable portion configured to move relative to the fixed portion between opened and closed positions in response to a command to selectively provide an opening between the fixed and movable portions. A fan case is arranged within the fan nacelle. The fan case includes an integral bull nose adjacent to the opening in the open position and to the movable portion in the closed position. The bull nose has a curved wall sloping radially outward.
Abstract translation: 燃气涡轮发动机推力反向器系统包括具有固定部分的风扇机舱和被构造成响应于选择性地在固定部分和可移动部分之间提供开口的命令而相对于固定部分在打开位置和关闭位置之间移动的可动部分。 风扇机壳安装在风扇机舱内。 风扇壳体包括在打开位置处与开口相邻的整体公牛鼻，并且在关闭位置包括可移动部分。 大鼻子有一个弯曲的壁向外径向倾斜。
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公开(公告)号：SG11201404965WA
公开(公告)日：2014-10-30
申请号：SG11201404965W
申请日：2013-03-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： CHARRON MICHAEL N , LUCAS JAMES L
IPC: F02K1/72
Abstract: A gas turbine engine thrust reverser system includes a fan nacelle having a fixed portion and a movable portion configured to move relative to the fixed portion between opened and closed positions in response to a command to selectively provide an opening between the fixed and movable portions. A fan case is arranged within the fan nacelle. The fan case includes an integral bull nose adjacent to the opening in the open position and to the movable portion in the closed position. The bull nose has a curved wall sloping radially outward.
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公开(公告)号：EP2831402A4
公开(公告)日：2015-12-16
申请号：EP13813553
申请日：2013-03-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor： CHARRON MICHAEL N , LUCAS JAMES L
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