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公开(公告)号:US20160039520A1
公开(公告)日:2016-02-11
申请号:US14454377
申请日:2014-08-07
申请人: Goodrich Corporation
发明人: DAVID DRENNEN , KEVIN REHFUS , ROBERT FRENCH , ALBERT KEITH PANT , JOSEPH E. BEASON , HARALD KLODE
CPC分类号: B64C25/44 , B60T13/741 , F16D59/02 , F16D63/002 , F16D65/12 , F16D65/183 , F16D65/186 , F16D2121/18 , F16D2121/20 , F16D2121/22 , F16D2127/06
摘要: An electro-mechanical actuator including an aircraft parking brake may include a motor shaft, a park brake disk, and a voice coil assembly. The voice coil assembly may include a bobbin configured to translate between an engaged position and a disengaged position. An engagement feature may be coupled to the bobbin. The engagement feature may contact the park brake disk in the engaged position. The engagement feature may be magnetically coupled to a voice coil magnet and washer in the disengaged position.
摘要翻译: 包括飞行器驻车制动器的机电致动器可以包括马达轴,驻车制动盘和音圈组件。 音圈组件可以包括构造成在接合位置和分离位置之间平移的线轴。 接合特征可以联接到线轴。 接合功能可以在接合位置接触驻车制动盘。 接合特征可以磁耦合到处于脱离位置的音圈磁体和垫圈。
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公开(公告)号:US20160146273A1
公开(公告)日:2016-05-26
申请号:US15012412
申请日:2016-02-01
申请人: GOODRICH CORPORATION
发明人: DAVID DRENNEN , HARALD KLODE , KEVIN REHFUS
CPC分类号: F16D49/02 , B60T1/062 , F16D65/14 , F16D2121/20 , F16D2125/18
摘要: A park brake system for an electric motor actuator is provided. The system may comprise a wrap spring that may rotatably engage the shaft. In this regard, the system may be configured to exert a radial force on a shaft of the electric motor actuator to lock the actuator. Moreover, in various embodiments, the system may be bi-stable.
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公开(公告)号:US20160123445A1
公开(公告)日:2016-05-05
申请号:US14528816
申请日:2014-10-30
申请人: GOODRICH CORPORATION
发明人: DAVID DRENNEN , KEVIN REHFUS , SATINDER MANN , ROBERT FRENCH , HARALD KLODE
CPC分类号: F16H25/2204 , B60T13/741 , B64C25/44 , F16D65/18 , F16D2121/24 , F16D2125/40 , F16D2125/50 , F16H2025/2075
摘要: A mechanical linear actuator in an aircraft brake may include a ball nut, a ball screw, and an actuator drive unit housing. The ball screw may rotate to drive the ball nut axially. The ball screw and the actuator drive unit housing may form a series of annular raceways. The ball screw may have a first window corresponding to a first raceway and a second window corresponding to a second raceway. Balls may be inserted into the first raceway through the first window and into the second raceway through the second window.
摘要翻译: 飞行器制动器中的机械线性致动器可以包括滚珠螺母,滚珠丝杠和致动器驱动单元壳体。 滚珠丝杠可以旋转以轴向驱动滚珠螺母。 滚珠丝杠和致动器驱动单元壳体可以形成一系列环形滚道。 滚珠丝杠可以具有对应于第一滚道的第一窗口和对应于第二滚道的第二窗口。 球可以通过第一窗口插入第一滚道并通过第二窗口进入第二滚道。
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公开(公告)号:US20150115778A1
公开(公告)日:2015-04-30
申请号:US14067003
申请日:2013-10-30
申请人: GOODRICH CORPORATION
发明人: DAVID DRENNEN , HARALD KLODE , KEVIN REHFUS
CPC分类号: H02K11/0094 , B60T8/1703 , B60T13/741 , B64C25/44 , F16D65/18 , F16D2121/24 , F16D2125/36 , H02K7/06 , H02K7/08 , H02K7/088 , H02K11/20 , H02K11/24 , H02K2205/03
摘要: An integrated actuator drive unit (ADU) assembly for an electric motor actuator is disclosed. The integrated ADU assembly may comprise at least one of an integrally formed ring gear, an integrally formed thrust bearing and integrally formed load cell. The integrated ADU assembly may comprise a portion of an electromechanical actuator. The electromechanical actuator may be utilized for aircraft braking systems.
摘要翻译: 公开了一种用于电动机致动器的集成致动器驱动单元(ADU)组件。 集成的ADU组件可以包括整体形成的环形齿轮,整体形成的推力轴承和整体形成的测力传感器中的至少一个。 集成ADU组件可以包括机电致动器的一部分。 机电致动器可用于飞机制动系统。
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