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公开(公告)号：US08256707B2
公开(公告)日：2012-09-04
申请号：US11832107
申请日：2007-08-01
IPC分类号： B64D27/00
CPC分类号： F02C7/20 , B64D27/18 , B64D27/26 , B64D2027/268 , Y02T50/44 , Y10T29/49826
摘要： An engine mounting configuration reacts engine thrust at an aft mount. The engine mounting configuration reduces backbone bending of the engine, intermediate case distortion and frees-up space within the core nacelle.
摘要翻译： 发动机安装配置可使发动机推力在后方安装。 发动机安装配置减少了发动机的主干弯曲，中间壳失真和内部机舱内的释放空间。
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公开(公告)号：US20090183512A1
公开(公告)日：2009-07-23
申请号：US12016337
申请日：2008-01-18
摘要： A mounting system for a gas turbine engine includes a thrust ring and a linkage assembly. The linkage assembly is at least partially received by the thrust ring. The linkage assembly reacts at least a side load and a thrust load communicated from the thrust ring.
摘要翻译： 用于燃气涡轮发动机的安装系统包括推力环和连杆组件。 连杆组件至少部分地被推力环接收。 连杆组件至少反作用于从止推环传递的侧向载荷和推力载荷。
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公开(公告)号：US20090056343A1
公开(公告)日：2009-03-05
申请号：US11832107
申请日：2007-08-01
CPC分类号： F02C7/20 , B64D27/18 , B64D27/26 , B64D2027/268 , Y02T50/44 , Y10T29/49826
摘要： An engine mounting configuration reacts engine thrust at an aft mount. The engine mounting configuration reduces backbone bending of the engine, intermediate case distortion and frees-up space within the core nacelle.
摘要翻译： 发动机安装配置可使发动机推力在后方安装。 发动机安装配置减少了发动机的主干弯曲，中间壳失真和内部机舱内的释放空间。
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公开(公告)号：US4527391A
公开(公告)日：1985-07-09
申请号：US431474
申请日：1982-09-30
申请人： Jon A. Marx , Wendell R. Loso
发明人： Jon A. Marx , Wendell R. Loso
CPC分类号： F02K1/72 , F02K1/76 , Y10T74/18992
摘要： For a long dual mixer nacelle housing a fan-jet engine powering aircraft, a pair of concentric sleeves sandwiching the cascades to effectuate thrust reversal are synchronously deployed axially to communicate the fan discharge air in the duct with ambient through the cascades. A rack and gear connection between sleeves permits the independent linear motion of each of the sleeves so that the actuation of one automatically actuates the other without the necessity of attaching both to each other.
摘要翻译： 对于一个装有喷气发动机供电飞机的长双重混合器机舱，一对夹着级联以实现推力反转的同心套筒同时轴向地展开，以将管道中的风扇排放空气与环境通过级联连通。 袖子之间的齿条和齿轮连接允许每个套筒的独立线性运动，使得一个的致动自动地致动另一个，而不需要彼此附接。
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公开(公告)号：US08118251B2
公开(公告)日：2012-02-21
申请号：US12016337
申请日：2008-01-18
摘要： A mounting system for a gas turbine engine includes a thrust ring and a linkage assembly. The linkage assembly is at least partially received by the thrust ring. The linkage assembly reacts at least a side load and a thrust load communicated from the thrust ring.
摘要翻译： 用于燃气涡轮发动机的安装系统包括推力环和连杆组件。 连杆组件至少部分地被推力环接收。 连杆组件至少反作用于从止推环传递的侧向载荷和推力载荷。
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公开(公告)号：US3979087A
公开(公告)日：1976-09-07
申请号：US592440
申请日：1975-07-02
申请人： Paul A. Boris , Jon A. Marx
发明人： Paul A. Boris , Jon A. Marx
摘要： The loads manifested by and imposed on the engine are transmitted through a mounting formed on a single plane with a three point attachment permitting the engine to be cantilever mounted although not limited thereto, and allows for the engine to project considerably forward of an airfoil section to which it is attached.
摘要翻译： 发动机表现并施加在发动机上的负载通过三点附件形成在单个平面上的安装件传递，允许发动机悬臂安装，但不限于此，并且允许发动机在翼型部分向前突出到 它是附加的。
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