公开(公告)号：US20160152318A1

公开(公告)日：2016-06-02

申请号：US15017462

申请日：2016-02-05

申请人： Commercial Aerospace Plane Pty Limited

发明人： Nick Alexander

IPC分类号： B64C1/26 ,  B64C3/32 ,  B64C5/08 ,  B64C9/00 ,  B64D37/34 ,  B64C25/34 ,  B64C39/12 ,  B64D15/06 ,  B64D27/18 ,  B64C3/10 ,  B64C15/02

CPC分类号： B64D37/34 ,  B64C3/10 ,  B64C3/32 ,  B64C15/02 ,  B64C30/00 ,  B64C39/12 ,  B64D27/18 ,  B64D31/00 ,  B64D2033/022 ,  B64D2033/026 ,  Y02T50/12 ,  Y02T50/44

摘要： An aerospace plane having an elongate body supporting a pair of wings each having at least two angled, trailing edge portions. The pair of wings are adapted to extend away from the elongated body in opposing directions. A landing gear assembly is operatively associated with the elongated body to be moveable from a retracted position where the landing gear assembly is substantially locatable within the elongated body and an extended position where the landing gear assembly extends at least partially away from the elongated body. At least one engine adapted to generate thrust. At least one stabilizer adapted to assist with movement of the aerospace plane during flight. The at least one engine is located at least partially within an intake housing adapted to direct air into said at least one engine. The intake housing having at least one inlet door adapted to move from a fully open position, which allows air to pass into the engine, to a sealingly closed position which prevents air from flowing into the engine, when the engine is shut down during flight.

摘要翻译： 一种具有支撑一对翼的细长主体的航空航天飞机，每个翼具有至少两个成角度的后缘部分。 这对翼适于在相反的方向上延伸离开细长体。 起落架组件可操作地与细长主体相关联，以从起落架组件基本上可定位在细长主体内的缩回位置移动，以及伸出位置，起落架组件至少部分地远离细长主体延伸。 至少一个适于产生推力的发动机。 至少一个稳定器适于在飞行期间协助航空航天飞机的运动。 所述至少一个发动机至少部分地位于适于将空气引导到所述至少一个发动机内的进气室内。 进气壳体具有至少一个入口门，其适于从允许空气进入发动机的完全打开位置移动到密封关闭位置，当发动机在飞行期间关闭时防止空气流入发动机。

公开(公告)号：US10384796B2

公开(公告)日：2019-08-20

申请号：US15017462

申请日：2016-02-05

申请人： Commercial Aerospace Plane Pty Limited

发明人： Nick Alexander

IPC分类号： B64C1/26 ,  B64D37/34 ,  B64C3/10 ,  B64C3/32 ,  B64D27/18 ,  B64C30/00 ,  B64D31/00 ,  B64C15/02 ,  B64C39/12 ,  B64D33/02

摘要： An aerospace plane having an elongate body supporting a pair of wings each having at least two angled, trailing edge portions. The pair of wings are adapted to extend away from the elongated body in opposing directions. A landing gear assembly is operatively associated with the elongated body to be moveable from a retracted position where the landing gear assembly is substantially locatable within the elongated body and an extended position where the landing gear assembly extends at least partially away from the elongated body. At least one engine adapted to generate thrust. At least one stabilizer adapted to assist with movement of the aerospace plane during flight. The at least one engine is located at least partially within an intake housing adapted to direct air into said at least one engine. The intake housing having at least one inlet door adapted to move from a fully open position, which allows air to pass into the engine, to a sealingly closed position which prevents air from flowing into the engine, when the engine is shut down during flight.

公开(公告)号：US20150232204A1

公开(公告)日：2015-08-20

申请号：US14390470

申请日：2013-04-04

申请人： Commercial Aerospace Plane Pty Limited

发明人： Nick Alexander

IPC分类号： B64G1/40 ,  B64D37/00 ,  B64C3/10

CPC分类号： B64G1/40 ,  B64C3/10 ,  B64C15/00 ,  B64C17/10 ,  B64D33/02 ,  B64D37/00 ,  B64D37/34 ,  B64D2033/026 ,  B64G1/002 ,  B64G1/14 ,  B64G1/405 ,  B64G1/58 ,  B64G1/62 ,  Y02T50/44

摘要： An aerospace plane (1) having an elongate body (2) supports a pair of wings (3). The wings are adapted to extend away from said body in opposing directions. A landing gear assembly is operatively associated with said body to be moveable from a retracted position where said assembly is substantially locatable within said body and an extended position were said assembly extends at least partially away from said body. At least one engine (10) is adapted to generate thrust. At least one stabilizer is adapted to assist with movement of said aerospace plane. The at least one engine is locatable at least partially within an intake housing (14) to direct air into said at least one engine. The intake housing having at least one door portion to open or close the intake housing to moderate the amount of air flowing into said intake housing and thereby said engine.

摘要翻译： 具有细长主体（2）的航空航天飞机（1）支撑一对翼（3）。 翼适于在相反方向上远离所述身体延伸。 起落架组件可操作地与所述主体相关联，以便可从所述组件基本上定位在所述主体内的缩回位置移动，并且所述组件的延伸位置至少部分地远离所述主体延伸。 至少一个发动机（10）适于产生推力。 至少一个稳定器适于协助所述航空航天飞机的运动。 所述至少一个发动机至少部分地位于进气室（14）内以将空气引导到所述至少一个发动机中。 进气室具有至少一个门部分，用于打开或关闭进气室，以缓和流入所述进气室的空气量，从而抑制所述发动机。