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1. 发明申请

US20130216384A1 Compact Rotorcraft Dual-Element Spherical Elastomeric Centrifugal-Force Bearing Assembly 有权
标题翻译：紧凑型Rotorcraft双元件球形弹性离心力轴承组件
公开(公告)号：US20130216384A1
公开(公告)日：2013-08-22
申请号：US13401203
申请日：2012-02-21
申请人： Frank B. Stamps , Bryan W. Marshall , Terry K. Thompson , Orion Braziel , David Popelka , Patrick Tisdale
发明人： Frank B. Stamps , Bryan W. Marshall , Terry K. Thompson , Orion Braziel , David Popelka , Patrick Tisdale
IPC分类号： B64C27/00
CPC分类号： B64C27/35
摘要： A rotary system includes a retention member and a flexible yoke having an opening forming a bridge. The rotary system is further provided with two bearing assemblies, a first bearing assembly extending through the opening of the yoke and configured to secure a rotor blade to the retention member and a second bearing assembly extending through the opening of the flexible yoke and configured to secure the rotor blade to the bridge. The second bearing element includes a bearing element having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring.
摘要翻译：旋转系统包括保持构件和具有形成桥的开口的柔性轭。旋转系统还设置有两个轴承组件，第一轴承组件延伸穿过轭的开口并且构造成将转子叶片固定到保持构件，以及延伸穿过柔性轭的开口的第二轴承组件，转子叶片到桥。第二轴承元件包括具有形成球形轮廓的第一表面和形成锥形轮廓的相对的整体第二表面的轴承元件。

2. 发明授权

US5647726A Rotor system vibration absorber 失效
标题翻译：转子系统减震器
公开(公告)号：US5647726A
公开(公告)日：1997-07-15
申请号：US599562
申请日：1996-02-15
申请人： Ajay Sehgal , Cecil E. Covington , Mithat Yuce , Bryan W. Marshall
发明人： Ajay Sehgal , Cecil E. Covington , Mithat Yuce , Bryan W. Marshall
IPC分类号： B64C27/51 , B64C27/00 , F16F15/12 , F16F15/133 , B64C27/06
CPC分类号： B64C27/001 , B64C2027/003 , Y10S416/50
摘要： A vibration absorber having a mass member which when static is supported by in-plane springs spaced apart from a base plate, top plate and spring retaining structures. The mass member has a bumper surface for contacting a motion limiter in the base plate. The mass member, base plate and top plate can have a passageway through the axis. The vibration absorber can be tuned by proper selection of the springs, degree of precompression and the variation of the amount of mass by the addition or removal of mass tuning weights.
摘要翻译：一种振动吸收器，具有质量部件，当静止由与基板，顶板和弹簧保持结构间隔开的平面内弹簧支撑时。质量构件具有用于接触基板中的运动限制器的保险杠表面。质量构件，基板和顶板可以具有穿过轴线的通道。振动吸收器可以通过弹簧的适当选择，预压缩程度和质量调整量的变化来调节。

3. 发明授权

US09702402B2 Increased capacity spherical lined bearings 有权
公开(公告)号：US09702402B2
公开(公告)日：2017-07-11
申请号：US13283973
申请日：2011-10-28
申请人： Frank B. Stamps , Bryan W. Marshall
发明人： Frank B. Stamps , Bryan W. Marshall
IPC分类号： F01D25/16 , F16C23/04 , B64C27/48 , B64C27/82
CPC分类号： F16C23/043 , B64C27/48 , B64C27/82 , F16C2326/43 , Y10T29/49332
摘要： A rotary system and method to control feathering movement of a rotor blade. The system having a yoke arm configured to rotate a rotor blade. A first bearing and a second bearing are utilized to secure the rotor blade to the yoke arm and are configured to restrict longitudinal and transverse movement, while allowing feathering movement of the rotor blade relative to yoke arm.

4. 发明授权

US5211538A Method for folding helicopter main rotor blades 失效
标题翻译：折弯直升机主转子叶片的方法
公开(公告)号：US5211538A
公开(公告)日：1993-05-18
申请号：US800578
申请日：1991-11-27
申请人： Ajay Seghal , Bryan W. Marshall
发明人： Ajay Seghal , Bryan W. Marshall
IPC分类号： B64C27/50
CPC分类号： B64C27/50
摘要： A method of folding the main rotor blades of a helicopter for storage in which blade supports are removably attached to the nose and tail of the fuselage of the helicopter. A first and second main rotor blades then are aligned with the longitudinal axis running from the forward blade support to the aft blade support. The first and second blades are placed upon, and restrained from rotation in, the blade supports. Then the first and second blades are permitted to fold about the rotor assembly of the helicopter by releasing a locking member of each blade. The first and second blades are folded by rotating the main rotor assembly while restraining from rotation the first and second blades in the forward and aft blades supports, respectively. After the rotor assembly is rotated through approximately 90 degrees, a third and fourth of the rotor blades are aligned with the longitudinal axis running through the forward and aft blade supports and the first and second blades are fully folded. Finally, the third and fourth main rotor blades are placed upon the forward and aft blade supports.
摘要翻译：折叠直升机的主转子叶片的方法可拆卸地附接到直升机的机身的鼻部和尾部，用于存储刀片支撑的主转子叶片。然后，第一和第二主转子叶片与从前叶片支撑件延伸到后叶片支撑件的纵向轴线对准。第一和第二叶片被放置在叶片支撑件上并被限制于其中。然后，允许第一和第二叶片通过释放每个叶片的锁定构件折叠在直升机的转子组件周围。第一和第二叶片通过分别旋转主转子组件而分别折叠，同时限制前后叶片支撑件中的第一和第二叶片旋转。在转子组件旋转大约90度之后，第三和第四转子叶片与延伸穿过前叶片和后叶片支撑件的纵向轴线对齐，并且第一和第二叶片被完全折叠。最后，第三和第四主转子叶片被放置在前叶片和后叶片支撑件上。

5. 发明申请

US20130108447A1 Increased Capacity Spherical Lined Bearings 有权
标题翻译：增加容量球面轴承
公开(公告)号：US20130108447A1
公开(公告)日：2013-05-02
申请号：US13283973
申请日：2011-10-28
申请人： Frank B. Stamps , Bryan W. Marshall
发明人： Frank B. Stamps , Bryan W. Marshall
IPC分类号： B64C27/32 , B23P15/00 , B64C27/45
CPC分类号： F16C23/043 , B64C27/48 , B64C27/82 , F16C2326/43 , Y10T29/49332
摘要： A rotary system and method to control feathering movement of a rotor blade. The system having a yoke arm configured to rotate a rotor blade. A first bearing and a second bearing are utilized to secure the rotor blade to the yoke arm and are configured to restrict longitudinal and transverse movement, while allowing feathering movement of the rotor blade relative to yoke arm.
摘要翻译：一种用于控制转子叶片的羽化运动的旋转系统和方法。该系统具有构造成使转子叶片旋转的轭臂。第一轴承和第二轴承用于将转子叶片固定到轭臂上，并且构造成限制纵向和横向运动，同时允许转子叶片相对于轭臂的羽化运动。

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