公开(公告)号：US20160169104A1

公开(公告)日：2016-06-16

申请号：US14569349

申请日：2014-12-12

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Steven Brian Rowe ,  Dan Birchak ,  Bill Ryan

IPC: F02C7/06 ,  F16B37/00 ,  F02C9/18 ,  F16K31/04

CPC classification number: F02C9/18 ,  F01D17/105 ,  F01D25/18 ,  F04D27/0215 ,  F04D27/023 ,  F16B37/00 ,  F16H57/045 ,  F16H57/0464 ,  F16H57/0497 ,  F16K31/047

Abstract: Variable bleed valve systems thereof including a stop mechanism with a self-lubricating follower nut assembly are provided. Self-lubricating follower nut assembly includes a follower nut and a pair of grease reservoirs. Follower nut has a recess at each of a first end and a second end and a groove extending between the first and second ends. A grease reservoir is disposed within each recess. Each grease reservoir has an outlet opening substantially aligned with a corresponding end of the groove. Each grease reservoir is compressible to expel lubricating grease into the groove upon compression. The self-lubricating follower nut assembly is configured to translate along a hollow screw between opposed end stops disposed within a housing of the stop mechanism. Each grease reservoir is compressed each time the self-lubricating follower nut assembly impacts an end stop of the opposed end stops.

Abstract translation: 提供了可变放气阀系统，其包括具有自润滑从动螺母组件的止动机构。 自润滑跟随螺母组件包括从动螺母和一对油脂储存器。 从动螺母在第一端和第二端各自具有凹部，在第一和第二端之间延伸有凹槽。 在每个凹槽内设置油脂储存器。 每个油脂储存器具有基本上与槽的对应端对齐的出口开口。 每个油脂储存器可压缩，以便在压缩时将润滑油脂排出到凹槽中。 自润滑从动螺母组件构造成沿着设置在止动机构的壳体内的相对的端部止动块之间的中空螺钉平移。 每次自润滑跟随螺母组件撞击相对的端部挡块的端部挡块时，每个油脂储存器都会被压缩。

公开(公告)号：US09873513B2

公开(公告)日：2018-01-23

申请号：US14602667

申请日：2015-01-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Steven Brian Rowe ,  William F. Ryan ,  Dan Birchak ,  Christopher Thomas ,  Albert Kang

IPC: B64D13/02 ,  B64D13/04 ,  F16K1/22 ,  F16K1/226

CPC classification number: B64D13/04 ,  F16K1/221 ,  F16K1/223 ,  F16K1/2261

Abstract: Embodiments of a cabin outflow valve having one or more laterally-tapered sealing surfaces are provided, as are cabin pressure controls system including cabin outflow valves. In one embodiment, the cabin outflow valve includes a frame and a first door, which is pivotally coupled to the frame and which is rotated by an actuator between open and closed positions. The first door includes, in turn, a torque input point at which the actuator applies a closing force when rotating the first door into a closed position. A laterally-tapered sealing surface extends along a lateral axis of the cabin outflow valve and has a profile height decreasing with increasing proximity to the torque input point. The laterally-tapered sealing surface helps to ensure the formation of a complete lateral seal when in the first door is rotated into the closed position to significantly reduce or eliminate leakage through the cabin outflow valve.

公开(公告)号：US20160214721A1

公开(公告)日：2016-07-28

申请号：US14602667

申请日：2015-01-22

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Steven Brian Rowe ,  William F. Ryan ,  Dan Birchak ,  Christopher Thomas ,  Albert Kang

IPC: B64D13/04 ,  F16K1/226 ,  F16K1/22

CPC classification number: B64D13/04 ,  F16K1/221 ,  F16K1/223 ,  F16K1/2261

Abstract: Embodiments of a cabin outflow valve having one or more laterally-tapered sealing surfaces are provided, as are cabin pressure controls system including cabin outflow valves. In one embodiment, the cabin outflow valve includes a frame and a first door, which is pivotally coupled to the frame and which is rotated by an actuator between open and closed positions. The first door includes, in turn, a torque input point at which the actuator applies a closing force when rotating the first door into a closed position. A laterally-tapered sealing surface extends along a lateral axis of the cabin outflow valve and has a profile height decreasing with increasing proximity to the torque input point. The laterally-tapered sealing surface helps to ensure the formation of a complete lateral seal when in the first door is rotated into the closed position to significantly reduce or eliminate leakage through the cabin outflow valve.

Abstract translation: 提供具有一个或多个侧向锥形密封表面的客舱流出阀的实施例，包括舱室流出阀的舱室压力控制系统也是如此。 在一个实施例中，机舱流出阀包括框架和第一门，其可枢转地联接到框架并且由致动器在打开位置和关闭位置之间旋转。 第一门又包括转矩输入点，当转动第一门进入关闭位置时，致动器施加闭合力。 横向锥形的密封表面沿着客舱流出阀的横向轴线延伸，并且具有随扭矩输入点越来越近的轮廓高度而减小。 横向锥形密封表面有助于确保在第一门旋转到关闭位置时形成完整的横向密封，以显着减少或消除通过客舱流出阀的泄漏。