公开(公告)号：US06397948B1

公开(公告)日：2002-06-04

申请号：US09433413

申请日：1999-11-03

申请人： Michael R. Williams ,  John A. Johansen ,  Christina A. Ross ,  David E. Wendt ,  Sylvester A. Joan ,  Stanley J. Rogala

发明人： Michael R. Williams ,  John A. Johansen ,  Christina A. Ross ,  David E. Wendt ,  Sylvester A. Joan ,  Stanley J. Rogala

IPC分类号： E21B43013

CPC分类号： E21B33/038 ,  E21B29/12 ,  E21B33/0355 ,  E21B43/017 ,  Y10T83/97

摘要： A load limiting break away arrangement for a subsea umbilical includes telescoping inner and outer bodies. The inner body includes multiple cross-bored holes; the outer body has slotted openings on its top and bottom sides. A shearing blade is positioned at one end of a top slot of the outer body. Individual umbilical tubes pass through a bottom slot of the outer body, through individual holes in the inner body and out a top slot of the outer body for attachment to multiple quick connect couplers on an umbilical termination head of an Umbilical Termination Assembly (UTA) and of an Electro-Hydraulic Distribution Module (EHDM). Tension resistant actuation members run between the UTA and EHDM so that when a snag of an umbilical occurs, the inner and outer bodies are pulled apart and the tubes are severed one by one by the blade of the outer body.

摘要翻译： 用于海底脐带的负载限制脱离装置包括伸缩的内部和外部主体。 内体包括多个十字孔; 外体在其顶部和底部具有开槽开口。 剪切刀片定位在外体的顶部狭槽的一端。 单个脐带管穿过外部主体的底部狭槽，穿过内部主体中的各个孔，并穿过外部主体的顶部狭槽，以连接到脐带终止组件（UTA）的脐带头端部上的多个快速连接耦合器，以及 的电液分配模块（EHDM）。 抗张力致动构件在UTA和EHDM之间延伸，使得当发生脐带的钩子时，内部和外部主体被拉开并且管被外部主体的叶片一个接一个地切断。

公开(公告)号：US5816042A

公开(公告)日：1998-10-06

申请号：US773586

申请日：1996-12-27

申请人： Daniel P. Guinan ,  David E. Wendt

发明人： Daniel P. Guinan ,  David E. Wendt

IPC分类号： F02K1/06 ,  F02K1/82 ,  F02K3/04

CPC分类号： F02K1/82 ,  F02K1/06

摘要： A flow diverting mechanism for the twin duct offtakes or coannular offtake for a turbo fan engine powering aircraft with either thrust reversing or short takeoff and vertical landing or both capabilities includes a rotary drum mounted between the turbine and afterburner sections and includes ports complementing the inlets in the offtakes to divert the core stream through the offtakes and passages to proportion the fan discharge air utilized for cooling purposes in the engine to cool the liner and walls of the offtakes and the engine components located downstream of the rotary drum while assuring separation of the core stream flow and fan air flow.

摘要翻译： 用于具有推力反向或短起飞和垂直着陆或两者能力的涡轮风扇发动机的涡轮风扇发动机的双向管道换向或换向机构的分流机构包括安装在涡轮机和后燃器部分之间的旋转鼓，并且包括与在 将芯流转移通过出料口和通道的比例，用于在发动机中用于冷却目的的风扇排出空气，以冷却位于转鼓的下游的出料口和发动机部件的衬套和壁，同时确保芯部分离 流量和风扇空气流量。

公开(公告)号：US6102329A

公开(公告)日：2000-08-15

申请号：US087891

申请日：1998-05-30

申请人： Daniel P. Guinan ,  David E. Wendt

发明人： Daniel P. Guinan ,  David E. Wendt

IPC分类号： F02K1/06 ,  F02K1/82 ,  B64B1/24

CPC分类号： F02K1/82 ,  F02K1/06

摘要： A flow diverting mechanism for the twin duct offtakes or coannular offtake for a turbo fan engine powering aircraft with either thrust reversing or short takeoff and vertical landing or both capabilities includes a rotary drum mounted between the turbine and afterburner sections and includes ports complementing the inlets in the offtakes to divert the core stream through the offtakes and passages to proportion the fan discharge air utilized for cooling purposes in the engine to cool the liner and walls of the offtakes and the engine components located downstream of the rotary drum while assuring separation of the core stream flow and fan air flow.

摘要翻译： 用于具有推力反向或短起飞和垂直着陆或两者能力的涡轮风扇发动机的涡轮风扇发动机的双向管道换向或换向机构的分流机构包括安装在涡轮机和后燃器部分之间的旋转鼓，并且包括与在 将芯流转移通过出料口和通道的比例，用于在发动机中用于冷却目的的风扇排出空气，以冷却位于转鼓的下游的出料口和发动机部件的衬套和壁，同时确保芯部分离 流量和风扇空气流量。

公开(公告)号：US5431344A

公开(公告)日：1995-07-11

申请号：US152625

申请日：1993-11-12

申请人： Rudolph J. Novotny ,  David E. Wendt ,  Gary D. Jones ,  James S. Johnson

发明人： Rudolph J. Novotny ,  David E. Wendt ,  Gary D. Jones ,  James S. Johnson

IPC分类号： F02K1/00 ,  F02K1/12 ,  F02K1/08 ,  B64C15/00

CPC分类号： F02K1/002 ,  F02K1/1261 ,  Y02T50/671

摘要： Exit area control panels 18 are supported for movement at an angle with respect to the nozzle axis 12. A varying exit area is formed as actuator 26 axially positions the panels 18. In each exit area control panel 18, there is slidably supported a throat area control panel 28, driven by actuator 32. A sliding throat is achieved as the two panels 18,28 are moved in each quadrant. Yaw and pitch vectoring is accomplished with selective positioning of the two panels.

摘要翻译： 出口区域控制面板18被支撑成相对于喷嘴轴线12以一定角度运动。当致动器26轴向地定位面板18时，形成变化的出射区域。在每个出口区域控制面板18中，可滑动地支撑着喉部区域 控制面板28由致动器32驱动。当两个面板18,28在每个象限中移动时，实现滑动喉部。 通过两个面板的选择性定位来实现偏航和俯仰矢量。