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1. 发明申请

US20110239439A1 ECCENTRIC FITTING ASSEMBLY 有权
标题翻译：偏心配件
公开(公告)号：US20110239439A1
公开(公告)日：2011-10-06
申请号：US13132922
申请日：2009-10-26
申请人： Rpbert W. Maxwell , Scott A. Chasen , Barton J. Hainsworth
发明人： Rpbert W. Maxwell , Scott A. Chasen , Barton J. Hainsworth
IPC分类号： F16B21/12 , F16B17/00 , B23P11/00
CPC分类号： B64C1/20 , F16B21/16
摘要： An eccentric fitting assembly includes an outer eccentric fitting which defines an outer axis, the outer eccentric fitting defines an opening offset from the outer axis and an inner eccentric fitting which defines an inner axis, the inner eccentric fitting defines a stud opening offset from the inner axis, the inner eccentric fitting receivable within the opening.
摘要翻译：偏心配件组件包括限定外轴线的外偏心配件，外偏心配件限定从外轴偏移的开口和限定内轴线的内偏心配件，内偏心配件限定了从内侧偏移的螺柱孔口轴心，内偏心配件可接收在开口内。

2. 发明授权

US5850991A Mechanical emergency dual-release mechanism for an external cargo hook system 失效
标题翻译：用于外部货物挂钩系统的机械紧急双重释放机构
公开(公告)号：US5850991A
公开(公告)日：1998-12-22
申请号：US942764
申请日：1997-10-02
申请人： Barton J. Hainsworth , Marc R. Poland
发明人： Barton J. Hainsworth , Marc R. Poland
IPC分类号： B64D1/12 , B64D1/22 , B64D25/00 , B64D1/08 , B64D9/00
CPC分类号： B64D1/22
摘要： One embodiment of a mechanical emergency dual-release mechanism for use in combination with a helicopter external cargo hook system that includes a cargo hook assembly that is operative to jettison an externally-attached cargo includes an interface member for mounting the dual-release mechanism in rigid combination with the cargo hook assembly, a pulley axle mounted in rigid combination with the interface member, a cockpit pulley assembly mounted in rotatable combination with the pulley axle, a cabin pulley assembly mounted in rotatable combination with the pulley axle, and a displacement transfer member that operatively interconnects the cockpit pulley assembly and the cabin pulley assembly. The cabin pulley assembly is functionally interconnected to the cargo hook assembly and operative in response to a mechanical stimulus generated by means of the cockpit pulley assembly or the cabin pulley assembly to activate the cargo hook assembly to jettison the externally-attached cargo.
摘要翻译：用于与直升机外部货物挂钩系统组合使用的机械紧急双重释放机构的一个实施例包括可卸下外部附着货物的货物钩组件，其包括用于将双重释放机构安装在刚性中的接口部件与货钩组件组合，与接口构件刚性组合安装的滑轮轴;与滑轮轴可旋转组合地安装的驾驶舱滑轮组件;与滑轮轴可旋转组合安装的客舱滑轮组件，以及位移传递构件其可操作地将驾驶舱滑轮组件和客舱滑轮组件相互连接。机舱滑轮组件在功能上互连到货钩组件并且响应于通过驾驶舱滑轮组件或客舱滑轮组件产生的机械刺激而起作用，以激活货钩组件以排出外部附着的货物。

3. 发明授权

US5291820A Inertial restraint mechanism for rail-mounted missiles 失效
标题翻译：轨道导弹惯性约束机制
公开(公告)号：US5291820A
公开(公告)日：1994-03-08
申请号：US988612
申请日：1992-12-10
申请人： Barton J. Hainsworth , Anton J. Kompare
发明人： Barton J. Hainsworth , Anton J. Kompare
IPC分类号： F41F3/052 , F41F3/06
CPC分类号： F41F3/052
摘要： An inertial restraint mechanism restrains a rail mounted missile against forward movement along a missile launch rail in response to a deceleration force. The restraint mechanism comprises a mass the movement of which is opposed by a spring force. When the mass overcomes the spring force due to a deceleration force in excess of a threshold magnitude, a locking mechanism is activated to a missile restraining position, thereby restraining the missile against forward movement. The restraint mechanism is locked in the missile restraining position to prevent release of a missile in response to multiple deceleration forces experienced by the missile and launch rail. Additionally, a detent may be provided which prevents actuation of the restraint mechanism to the missile restraining position unless the missile is stored in a storage compartment.
摘要翻译：惯性约束机制限制轨道安装的导弹，以响应于减速力沿着导弹发射轨向前运动。约束机构包括其运动由弹簧力相反的质量。当质量克服由于超过阈值大小的减速力引起的弹簧力时，锁定机构被激活到导弹限制位置，从而限制导弹向前移动。限制机制锁定在导弹限制位置，以防止导弹和导弹经受的多重减速力的弹力释放。此外，可以设置制动器，其防止约束机构致动到导弹限制位置，除非导弹被存储在储藏室中。

4. 发明授权

US08667663B2 Eccentric fitting assembly 有权
标题翻译：偏心配件组件
公开(公告)号：US08667663B2
公开(公告)日：2014-03-11
申请号：US13132922
申请日：2009-10-26
申请人： Robert W. Maxwell , Scott A. Chasen , Barton J. Hainsworth
发明人： Robert W. Maxwell , Scott A. Chasen , Barton J. Hainsworth
IPC分类号： F16B21/12
CPC分类号： B64C1/20 , F16B21/16
摘要： An eccentric fitting assembly includes an outer eccentric fitting which defines an outer axis, the outer eccentric fitting defines an opening offset from the outer axis and an inner eccentric fitting which defines an inner axis, the inner eccentric fitting defines a stud opening offset from the inner axis, the inner eccentric fitting receivable within the opening.
摘要翻译：偏心配件组件包括限定外轴线的外偏心配件，外偏心配件限定从外轴偏移的开口和限定内轴线的内偏心配件，内偏心配件限定了从内侧偏移的螺柱孔口轴心，内偏心配件可接收在开口内。

5. 发明授权

US06199793B1 System for deployment and retrieval of airborne towed vehicles 有权
标题翻译：机载拖车的部署和检索系统
公开(公告)号：US06199793B1
公开(公告)日：2001-03-13
申请号：US09330655
申请日：1999-06-11
申请人： Barton J. Hainsworth , William F. Beaver, Jr.
发明人： Barton J. Hainsworth , William F. Beaver, Jr.
IPC分类号： B64D302
CPC分类号： B64D3/02 , B63B21/66 , B64D1/02
摘要： A towed vehicle deployment and retrieval system for attachment to an aircraft. The system includes a pylon support that is designed to mount to an aircraft and project outward therefrom. A stores pylon is mounted to the pylon support. The stores pylon has at least one swaybrace reciprocally attached to it for removably engaging with a towed vehicle. The system also includes a winch that is configured for mounting within the aircraft. The winch controls the feeding and retrieval of a winch cable that is attached to the towed vehicle. A tow cable is removably attached to the aircraft and is engaged with the winch cable using a tow pole such that the tow cable fully supports the towed vehicle when the towed vehicle is in the towing position. A method is also disclosed for attaching a winch cable and towed vehicle to a tow cable.
摘要翻译：用于附接到飞机的牵引车辆部署和检索系统。该系统包括一个支架，其设计用于安装在飞机上并向外突出。一个商店的塔架安装在塔架支架上。商店吊架具有至少一个相互连接的摇摆架，用于可拆卸地与被牵引的车辆接合。该系统还包括配置为安装在飞行器内的绞盘。绞车控制连接在牵引车上的绞车电缆的进给和取出。拖曳电缆可拆卸地连接到飞机上，并且使用拖曳杆与绞盘缆线接合，使得当牵引车辆处于拖曳位置时，拖曳缆索完全支撑拖曳车辆。还公开了一种用于将绞车缆绳和牵引车辆附接到牵引绳索的方法。

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