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1. 发明授权

US5417056A Axially translating screen suppressor for a gas turbine engine augmentor 失效
标题翻译：用于燃气轮机发动机增压器的轴向翻转屏幕抑制器
公开(公告)号：US5417056A
公开(公告)日：1995-05-23
申请号：US228790
申请日：1994-04-18
申请人： Kenneth L. Johnson , Donald M. Corsmeier , William L. Weaver , Eric H. Lewis
发明人： Kenneth L. Johnson , Donald M. Corsmeier , William L. Weaver , Eric H. Lewis
IPC分类号： F02C7/28 , F02C9/16 , F02C9/18 , F02K3/075 , F02K3/02 , F02C7/24
CPC分类号： F02K3/075 , F05D2250/34
摘要： An augmentor screech suppressor for a gas turbine engine includes a screech suppressor liner mounted on a screech housing and an actuator for translating the screech suppressor liner axially forward and aft, with the actuator located outside the outer duct of the engine. In a preferred embodiment in a variable cycle gas turbine engine, a variable area bypass injector (VABI) valve with a circumferentially conical surface slopes into the screech suppressor liner surface and inner and outer crank arms transfer linear motion from the actuator through the outer duct wall, cooperating with idler arms to translate the screech suppressor housing, and thus the VABI valve and screech suppressor linear, axially between open and closed valve position.
摘要翻译：用于燃气涡轮发动机的增压器爆震抑制器包括安装在尖头壳体上的尖头抑制器衬套和用于使所述尖头抑制器衬套轴向向前和向后平移的致动器，致动器位于发动机外管外部。在可变循环燃气涡轮发动机的优选实施例中，具有周向圆锥形表面的可变区域旁路喷射器（VABI）阀门倾斜到尖叫抑制器衬套表面中，并且内部和外部曲柄臂从致动器传递线性运动通过外部管道壁，与惰轮配合来翻转尖啸抑制器壳体，从而使VABI阀和尖叫抑制器线性，轴向位于打开和关闭的阀门位置之间。

2. 发明授权

US5343697A Variable area bypass injector 失效
标题翻译：可变区域旁路注射器
公开(公告)号：US5343697A
公开(公告)日：1994-09-06
申请号：US98994
申请日：1993-07-29
申请人： Kenneth L. Johnson , Donald M. Corsmeier , William L. Weaver , Eric H. Lewis
发明人： Kenneth L. Johnson , Donald M. Corsmeier , William L. Weaver , Eric H. Lewis
IPC分类号： F02C7/28 , F02C9/16 , F02C9/18 , F02K3/075 , F02K3/02
CPC分类号： F02K3/075 , F05D2250/34
摘要： A variable area bypass injector (VABI) for a variable cycle gas turbine engine includes a circumferentially continuous valve with a conical surface sloping into a screech suppressor surface, a circumferentially segmented seal attached to the diffuser, and a valve actuator located outside the outer duct of the engine. Each seal segment is spring loaded to allow for different axial movement between circumferentially adjacent segments, and has a seat portion complimentary to the valve conical surface for sealingly engaging the valve when in closed position. Additionally, the seal segments are shaped with a low aerodynamic profile and cooperate with the VABI conical surface, when the valve is in an open position, to provide an annular conic channel that keeps the bypass flow attached to the VABI valve and core flowpath walls as it is injected into the core gas stream. Inner and outer crank arms transfer linear motion from the actuator through the outer duct wall, cooperating with idler arms to translate the valve and screech suppressor axially between open and closed valve positions.
摘要翻译：用于可变循环燃气涡轮发动机的可变区旁路喷射器（VABI）包括周向连续的阀，其具有倾斜成尖锐抑制器表面的锥形表面，附接到扩散器的周向分段密封件，以及位于外部管道外侧的阀致动器引擎。每个密封段被弹簧加载以允许在周向相邻的段之间的不同的轴向运动，并且具有与阀锥形表面互补的座部分，用于在处于关闭位置时密封地接合阀。另外，当阀处于打开位置时，密封段成形为具有低空气动力学轮廓并与VABI锥形表面配合，以提供环形圆锥通道，其将旁路流量保持在VABI阀和芯流路壁上，如将其注入到核心气流中。内部和外部曲柄臂从致动器通过外部管道壁传递线性运动，与空转臂配合，以在打开和关闭的阀门位置之间轴向平移阀门和尖叫抑制器。

3. 发明授权

US5287697A Variable area bypass injector seal 失效
标题翻译：可变区域旁路喷油器密封
公开(公告)号：US5287697A
公开(公告)日：1994-02-22
申请号：US816694
申请日：1992-01-02
申请人： Kenneth L. Johnson , Donald M. Corsmeier , William L. Weaver , Eric H. Lewis
发明人： Kenneth L. Johnson , Donald M. Corsmeier , William L. Weaver , Eric H. Lewis
IPC分类号： F02C7/28 , F02C9/16 , F02C9/18 , F02K3/075 , F02K3/02
CPC分类号： F02K3/075 , F05D2250/34
摘要： A variable area bypass injector (VABI) seal for a variable cycle gas turbine engine includes a circumferentially segmented seal attached to the diffuser. Each seal segment is spring loaded to allow for different axial movement between circumferentially adjacent segments, and has a seat portion complimentary to a VABI valve conical surface for sealingly engaging the VABI valve when the VABI valve is in closed position. Additionally, the seal segments are shaped with a low aerodynamic profile and cooperate with the VABI valve conical surface, when the valve is in an open position, to provide an annular conic channel that keeps the bypass flow attached to the VABI valve and core flowpath walls as it is injected into the core gas stream.
摘要翻译：用于可变循环燃气涡轮发动机的可变区域旁路喷射器（VABI）密封件包括附接到扩散器的周向分段的密封件。每个密封段是弹簧加载的，以允许周向相邻的段之间的不同的轴向运动，并且具有与VABI阀锥形表面互补的座部分，用于当VABI阀处于关闭位置时密封地接合VABI阀。此外，当阀处于打开位置时，密封段成形为具有低空气动力学特性并与VABI阀锥形表面配合，以提供环形圆锥通道，其保持旁路流动附着到VABI阀和芯流道壁因为它被注入到核心气流中。

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