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公开(公告)号：US20110165828A1
公开(公告)日：2011-07-07
申请号：US12651823
申请日：2010-01-04
申请人： Darrell Horner , Ross F. Meyer , Albert Kang , Kevin Prodromides , Barrett Fuhrmann , Karl Schroeder , Beth Miller , David P. Gentile , Govind Yadav
发明人： Darrell Horner , Ross F. Meyer , Albert Kang , Kevin Prodromides , Barrett Fuhrmann , Karl Schroeder , Beth Miller , David P. Gentile , Govind Yadav
IPC分类号： B64D13/02
CPC分类号： F24F13/1426 , B64D13/02 , B64D13/04 , F16K1/221 , F16K1/222 , F16K1/223 , F24F13/1486 , Y02T50/44
摘要： An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
摘要翻译： 飞机舱压力控制系统流出推力回收阀包括框架，阀元件和致动硬件。 框架，阀元件和致动硬件的至少一部分由复合材料制成。 致动硬件设置在框架的外部。
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公开(公告)号：US08632381B2
公开(公告)日：2014-01-21
申请号：US12651823
申请日：2010-01-04
申请人： Darrell Horner , Ross F. Meyer , Albert Kang , Kevin Prodromides , Barry Fuhrmann , Karl Schroeder , Beth Miller , David P. Gentile , Govind Yadav
发明人： Darrell Horner , Ross F. Meyer , Albert Kang , Kevin Prodromides , Barry Fuhrmann , Karl Schroeder , Beth Miller , David P. Gentile , Govind Yadav
IPC分类号： B64D13/02
CPC分类号： F24F13/1426 , B64D13/02 , B64D13/04 , F16K1/221 , F16K1/222 , F16K1/223 , F24F13/1486 , Y02T50/44
摘要： An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
摘要翻译： 飞机舱压力控制系统流出推力回收阀包括框架，阀元件和致动硬件。 框架，阀元件和致动硬件的至少一部分由复合材料制成。 致动硬件设置在框架的外部。
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公开(公告)号：US20100240291A1
公开(公告)日：2010-09-23
申请号：US12409286
申请日：2009-03-23
CPC分类号： B64D13/02 , Y10T137/6906
摘要： An aircraft cabin pressure control system outflow valve includes a frame, a valve element, and a position sensor. The frame is configured to be mounted on an aircraft exterior skin. The valve element is rotationally coupled to the frame, and is coupled to receive an actuation drive force. The valve element is responsive to the actuation drive force to rotate to a position between a closed position and a plurality of open positions. The position sensor is coupled to the frame and is configured to directly sense rotation of the valve element and supply a position signal representative of valve element position.
摘要翻译： 飞机舱压力控制系统流出阀包括框架，阀元件和位置传感器。 框架被配置为安装在飞机外部皮肤上。 阀元件旋转地联接到框架，并且被联接以接收致动驱动力。 阀元件响应致动驱动力以旋转到关闭位置和多个打开位置之间的位置。 位置传感器联接到框架并且被配置为直接感测阀元件的旋转并且提供表示阀元件位置的位置信号。
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公开(公告)号：US08864559B2
公开(公告)日：2014-10-21
申请号：US12350712
申请日：2009-01-08
申请人： Darrell Horner , Bob Olson , Gerard McCoy
发明人： Darrell Horner , Bob Olson , Gerard McCoy
摘要： A multiple outflow valve control system for an aircraft is provided having a plurality of outflow valves that may be controlled independently via an all electrical control system. The outflow valves may be located in various locations in an aircraft. The control system may have a control loop controlling the outflow valve motors via open-loop PWM commands and may not have a motor speed feedback in the control loop. The cabin pressure control system may have manual and auto controls controlling separate motors on each outflow valve. Auto motor control may be performed via software biasing command logic included in the control laws in the control system. Air flow may be biased through selected outflow valves and the degree of biasing may be automatically or manually set.
摘要翻译： 提供了一种用于飞行器的多重流出阀控制系统，其具有可经由全部电气控制系统独立控制的多个流出阀。 流出阀可以位于飞行器的各个位置。 控制系统可以具有通过开环PWM命令控制流出阀马达的控制回路，并且可能在控制回路中不具有马达速度反馈。 机舱压力控制系统可以具有手动和自动控制，每个流出阀上控制单独的电动机。 自动电机控制可以通过控制系统中控制规律中包含的软件偏置指令逻辑执行。 空气流可以通过选定的流出阀偏置，并且偏置度可以自动或手动设定。
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公开(公告)号：US20120064813A1
公开(公告)日：2012-03-15
申请号：US12878776
申请日：2010-09-09
申请人： Darrell Horner , Justin A. Tanner
发明人： Darrell Horner , Justin A. Tanner
IPC分类号： B64D13/02
摘要： A single valve door thrust recovery outflow valve is provided that does not rely on a relatively large and expensive actuator to move it, and does not create unwanted drag during aircraft cruise operations. The valve includes a valve frame, a valve door, and an aerodynamic flap. The valve door is rotationally coupled to the valve frame, is adapted to receive a drive torque, and is configured, upon receipt of the drive torque, to rotate between a closed position, a full-open position, and a plurality of partial-open positions between the closed position and the full-open position. The aerodynamic flap is coupled to the valve door. When the valve door is in the closed position and in numerous partial-open positions, the aerodynamic flap makes the thrust recovery outflow valve aerodynamically clean.
摘要翻译： 提供单个阀门推力回收流出阀，其不依赖于相对较大和昂贵的致动器来移动它，并且在飞行器巡航操作期间不产生不期望的阻力。 该阀包括阀架，阀门和空气动力学翼片。 阀门旋转地联接到阀框架，适于接收驱动扭矩，并且在接收到驱动扭矩时被配置为在关闭位置，全开位置和多个部分打开之间旋转 关闭位置和全开位置之间的位置。 气动翼片联接到阀门。 当阀门处于关闭位置并且处于多个部分打开位置时，空气动力翼片使推力回收流出阀在空气动力学上清洁。
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6.发明授权Cabin pressure control system thrust recovery outflow valve and method that enable ram air recovery 有权车厢压力控制系统推力回收流出阀和使压头空气回收的方法公开(公告)号：US09475584B2
公开(公告)日：2016-10-25
申请号：US13224890
申请日：2011-09-02
申请人： Darrell Horner , Eric Thomas Jeffers , Robert Ryan Lunderville , Mark William Mundell , John Nathan Bowler , Derek Schell
发明人： Darrell Horner , Eric Thomas Jeffers , Robert Ryan Lunderville , Mark William Mundell , John Nathan Bowler , Derek Schell
IPC分类号： B64D13/02
CPC分类号： B64D13/02
摘要： A thrust recovery outflow valve and method for controlling the transfer of air between a cabin in an aircraft and atmosphere outside of the aircraft are provided. An outflow valve is mounted on the aircraft that includes a valve frame, a first valve door, and a second valve door. The first valve door is rotated to a first predetermined open position while the second valve door is in the second door closed position to thereby open first and second flow passages that place the aircraft cabin in fluid communication with the atmosphere. When the first valve door is at a first predetermined open position, a flap is rotated, relative to the first valve door, to at least partially cover the second flow passage and thereby at least inhibit flow through the second flow passage.
摘要翻译： 提供了一种用于控制飞行器舱室与飞机外部气氛之间的空气传送的推力回收流出阀和方法。 一个流出阀安装在飞机上，其中包括一个阀架，一个第一阀门和一个第二阀门。 第一阀门旋转到第一预定打开位置，而第二阀门处于第二门关闭位置，从而打开使飞机机舱与大气流体连通的第一和第二流动通道。 当第一阀门处于第一预定打开位置时，翼片相对于第一阀门门旋转，以至少部分地覆盖第二流动通道，从而至少阻止流过第二流动通道。
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公开(公告)号：US20100173575A1
公开(公告)日：2010-07-08
申请号：US12350712
申请日：2009-01-08
申请人： Darrell Horner , Bob Olson , Gerard McCoy
发明人： Darrell Horner , Bob Olson , Gerard McCoy
IPC分类号： B64D13/02
摘要： A multiple outflow valve control system for an aircraft is provided having a plurality of outflow valves that may be controlled independently via an all electrical control system. The outflow valves may be located in various locations in an aircraft. The control system may have a control loop controlling the outflow valve motors via open-loop PWM commands and may not have a motor speed feedback in the control loop. The cabin pressure control system may have manual and auto controls controlling separate motors on each outflow valve. Auto motor control may be performed via software biasing command logic included in the control laws in the control system. Air flow may be biased through selected outflow valves and the degree of biasing may be automatically or manually set.
摘要翻译： 提供了一种用于飞行器的多重流出阀控制系统，其具有可经由全部电气控制系统独立控制的多个流出阀。 流出阀可以位于飞行器的各个位置。 控制系统可以具有通过开环PWM命令控制流出阀马达的控制回路，并且可能在控制回路中不具有马达速度反馈。 机舱压力控制系统可以具有手动和自动控制，每个流出阀上控制单独的电动机。 自动电机控制可以通过控制系统中控制规律中包含的软件偏置指令逻辑执行。 空气流可以通过选定的流出阀偏置，并且偏置度可以自动或手动设定。
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公开(公告)号：US20060019594A1
公开(公告)日：2006-01-26
申请号：US11048010
申请日：2005-01-31
申请人： Darrell Horner , Thomas Whitney , Tim Arthurs
发明人： Darrell Horner , Thomas Whitney , Tim Arthurs
IPC分类号： B64D13/02
摘要： A cabin pressure control system and method includes one or more dual-channel controllers. One of the channels is a primary channel and the other channel is a secondary channel. The primary channel includes two dissimilar cabin pressure sensors and a controller that is used to modulate the position of an outflow valve, to thereby control cabin pressure, in response to the sensed cabin pressures. The secondary channel includes a cabin pressure sensor and a differential pressure sensor that is configured to sense cabin-to-atmosphere differential pressure. The secondary channel, based the sensed differential pressure, will implement differential pressure limiting in the event the primary channel does not. The primary and secondary channels both implement a cabin altitude limit function. The primary channel uses its two cabin pressure sensors, and a signal derived from the cabin pressure sensor in the secondary channel, to implement this function, and the secondary channel uses its cabin pressure sensor, and signals derived from the cabin pressure sensors in the primary channel, to implement this function.
摘要翻译： 机舱压力控制系统和方法包括一个或多个双通道控制器。 其中一个频道是主频道，另一频道是次频道。 主通道包括两个不同的舱室压力传感器和用于响应于感测的舱室压力来调节流出阀的位置从而控制舱室压力的控制器。 辅助通道包括舱室压力传感器和差压传感器，其构造成感测舱室至大气压差。 基于感测压差的次通道将在主通道不发生的情况下实施压差限制。 主要和次要通道都实现了机舱高度限制功能。 主通道使用其两个舱室压力传感器，以及从次要通道中的舱室压力传感器得到的信号，以实现该功能，次通道使用其舱室压力传感器，以及从主舱内的舱室压力传感器得到的信号 通道，实现这个功能。
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公开(公告)号：US20050263733A1
公开(公告)日：2005-12-01
申请号：US10854100
申请日：2004-05-26
CPC分类号： F16K1/221 , F16K27/0218
摘要： Methods and apparatus for retaining a butterfly plate within a valve housing after complete drive shaft failure. More particularly, the present invention is directed to the use of a pin extending between the butterfly plate and the valve housing where an end of the pin extends into a semi-circular channel centered on the center axis of the drive shaft. In preferred embodiments, the pin is immovably fixed to the valve housing, and extends into a channel on the butterfly plate assembly where the channel is sized, dimensioned, and positioned such that it corresponds to the path of an end of the pin as the plate rotates on the drive shaft.
摘要翻译： 在完全驱动轴故障之后，将蝶板保持在阀壳体内的方法和装置。 更具体地说，本发明涉及在蝴蝶板和阀壳体之间延伸的销的使用，其中销的端部延伸成以驱动轴的中心轴线为中心的半圆形通道。 在优选实施例中，销不可移动地固定到阀壳体，并且延伸到蝶板组件上的通道中，其中通道的尺寸，尺寸和位置使得其对应于作为板的销的端部的路径 在驱动轴上旋转。
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公开(公告)号：US08382035B2
公开(公告)日：2013-02-26
申请号：US12556345
申请日：2009-09-09
IPC分类号： B64D11/00
CPC分类号： B64D13/02
摘要： A valve for use in a cabin pressure control system includes a valve body and a poppet. The valve body includes an inlet, an outlet, and a fluid flow passage therebetween. The poppet is disposed in the valve body. The poppet is moveable between at least a closed position, in which the poppet at least substantially restricts fluid from flowing through the fluid flow passage, and an open position, in which fluid is allowed to flow through the fluid flow passage. The valve body, the poppet, or both, have a fluorocarbon coating.
摘要翻译： 用于机舱压力控制系统的阀包括阀体和提升阀。 阀体包括入口，出口和其间的流体流动通道。 提升阀配置在阀体内。 提升阀可以在至少一个关闭位置之间移动，在该关闭位置，提升阀至少基本上限制流体流过流体流动通道，而打开位置允许流体流过流体流动通道。 阀体，提升阀或两者都具有氟碳涂层。
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