公开(公告)号：US4637292A

公开(公告)日：1987-01-20

申请号：US812565

申请日：1985-12-23

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： B64D7/08 ,  F41F3/06

CPC分类号： B64D7/08

摘要： The invention is a rotary launcher system for an aircraft having a weapon bay with an opening in communication with the exterior of the aircraft. In detail, the system comprises a plurality of first doors mounted on the aircraft which are movable from an open position to a closed position thereby sealing off a portion of the opening and forming a portion of the external contour of the aircraft over the opening. A frame member having at least one weapon mounting assembly mounted thereto is rotatively mounted within the weapon bay. The weapon mounting assembly is rotatably alignable with the opening upon rotation thereof. A second weapon mounting assembly is mounted to the frame member and is alignable with the opening upon rotation of the frame member. The second weapon mounting assembly comprises a pair of second doors rotatively mounted to the frame member. The pair of second doors is movable from an open position to a closed position so that the remaining portion of the opening is sealed off and forms the remaining portion of the external contour of the aircraft. A missile ejector assembly is mounted to at least one of the second door system for moving the missile from a retracted position to an extended position so that the missile can be launched when the second door system is in the open position.

摘要翻译： 本发明是一种用于飞行器的旋转发射器系统，其具有具有与飞机外部连通的开口的武器舱。 详细地，系统包括安装在飞机上的多个第一门，其可以从打开位置移动到关闭位置，从而密封开口的一部分并且在开口上形成飞行器的外部轮廓的一部分。 具有安装在其上的至少一个武器安装组件的框架构件可旋转地安装在武器舱内。 武器安装组件在其旋转时可旋转地与开口对准。 第二武器安装组件安装到框架构件并且在框架构件旋转时可与开口对准。 第二武器安装组件包括可旋转地安装到框架构件的一对第二门。 一对第二门可以从打开位置移动到关闭位置，使得开口的剩余部分被密封并形成飞行器的外部轮廓的剩余部分。 导弹喷射器组件安装到第二门系统中的至少一个，用于将导弹从缩回位置移动到延伸位置，使得当第二门系统处于打开位置时可以启动导弹。

公开(公告)号：US4050656A

公开(公告)日：1977-09-27

申请号：US687283

申请日：1976-05-17

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： B64D1/06 ,  B64D1/02

CPC分类号： B64D1/06

摘要： An ejector rack that is attachable to an aircraft and is for supporting and selectively releasing and/or ejecting a store that is carried internal of the aircraft, i.e., in a bomb bay. The store can be released from the ejector rack, and from the aircraft, in either of two ways, namely: by pushing on a manually operated release handle; or, by forced ejection, the only way used during flight of the aircraft. Forced ejection is achieved by sending an electrical impulse to either or both of two cartridges in the breech of the ejector rack, igniting the cartridge(s). Gas is generated thereby; and, the resultant pressure that is built up in a gas system in the rack provides force that acts upon an unlocking piston, causing the piston to move out of its "locked" position. In turn, the moving piston provides a force on a slide, rotating a latch that allows the main linkage bellcrank to rotate and thus to open two hooks which are holding the store, thereby releasing the suspended store. Concurrently, gas pressure is manifolded to two sway brace ejection piston cylinders, and the ejection pistons therein are forcefully extended, causing positive and forcible ejection of the store by the ejection pistons. Unlike prior art devices, this ejector rack incorporates: a fully automatic sway brace system; a counterbalance assembly with a counterweight that prevents vibration loads from causing the inadvertent release of the store from the rack; and, a safety lock that automatically closes and also latches the hook linkage when the lock is moved to the locked position.

摘要翻译： 一种可附接到飞行器并且用于支撑和选择性地释放和/或喷射在飞行器内部携带的商店（即在炸弹舱中）的喷射器架。 商店可以从喷射器架和从飞行器以两种方式中的一种释放，即：通过推动手动操作的释放手柄; 或者通过强制弹射，在飞机飞行中使用的唯一方式。 通过向喷射器架的后膛中的两个盒中的任一个或两个发送电脉冲来点燃盒，来实现强制喷射。 从而产生气体; 并且在机架中的气体系统中建立的合成压力提供作用在解锁活塞上的力，导致活塞移出其“锁定”位置。 反过来，移动的活塞在滑动件上提供力，旋转一个闩锁，允许主联动曲拐转动，从而打开两个保持储存器的钩，从而释放悬挂的储存器。 同时，两个摆动支架弹出活塞气缸的气体压力分歧，其中的喷射活塞被强力地延伸，从而引起喷射活塞的存储器的正向和强制的喷射。 与现有技术的设备不同，该喷射器机架包括：全自动摇摆支架系统; 具有配重的平衡组件，其防止振动负载导致商店从机架的意外释放; 以及当锁移动到锁定位置时，自动关闭的安全锁还锁定钩连杆。

公开(公告)号：US4753151A

公开(公告)日：1988-06-28

申请号：US879705

申请日：1986-06-27

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： B64D1/02 ,  F41F5/02

CPC分类号： B64D1/02

摘要： The actuator system comprises an actuator which includes a cylinder having a first end adapted to receive one or more gas generators and a second end having an opening therethrough. A piston having first and second ends defining the length thereof is movably mounted in the cylinder, dividing the cylinder into first and second variable volume chambers. The piston includes a piston rod attached thereto which extends out through the opening of the second end of the cylinder. An accumulator is coupled by a first passage system to the second variable volume chamber at substantially the second end of the cylinder. A first sequencing system provides for the charging of the accumulator and second chamber after a portion of the stroke. As the piston continues, the gas in the second chamber compresses, building up pressure and slowing the piston down. Near the end of the stroke, a second sequencing system vents the first chamber overboard and when the piston reaches the second end of the cylinder the gas in the accumlator is used to drive the piston back to the retracted position.

摘要翻译： 致动器系统包括致动器，该致动器包括具有适于容纳一个或多个气体发生器的第一端和具有穿过其中的开口的第二端的气缸。 具有限定其长度的第一端和第二端的活塞可移动地安装在气缸中，将气缸分成第一和第二可变容积室。 活塞包括附接到其上的活塞杆，其延伸穿过气缸的第二端的开口。 蓄液器通过第一通道系统在基本上在气缸的第二端处连接到第二可变容积室。 第一排序系统提供在一部分行程之后蓄能器和第二室的充电。 随着活塞的继续，第二腔室中的气体压缩，增加压力并使活塞减速。 靠近行程结束时，第二排序系统将第一室排空，当活塞到达气缸的第二端时，蓄能器中的气体被用于将活塞驱动回缩回位置。

公开(公告)号：US4075929A

公开(公告)日：1978-02-28

申请号：US653055

申请日：1976-01-28

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： F15B15/16 ,  F01B15/00 ,  F15B11/18 ,  F15B15/22

CPC分类号： F15B15/16

摘要： A telescopic fluid ram or thruster utilizing pressurized gas and having an inner and outer piston that slides within a cylindrical bore including a central probe which is tapered and extends into the bore of the inner piston where it will cause the inner piston to move under high pressure while the gas escaping from around the tapered area produces a holding force to hold the outer piston in place until the inner piston is fully extended, at which time the outer piston will extend under a reduced pressure.

摘要翻译： 一种利用加压气体并具有内部和外部活塞的伸缩液体冲击器或推进器，所述内部和外部活塞在圆柱形孔内滑动，所述圆柱形孔包括中心探针，所述中心探针是锥形的并且延伸到内部活塞的孔中，在该孔中将使内部活塞在高压下移动 而从锥形区域周围逸出的气体产生保持力，以将外部活塞保持就位直到内部活塞完全伸出，此时外部活塞将在减压下延伸。

公开(公告)号：US4679751A

公开(公告)日：1987-07-14

申请号：US857004

申请日：1986-04-29

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： B64D7/08 ,  B64D1/06

CPC分类号： B64D7/08

摘要： The invention is a weapon dispensing system for an aircraft. The system includes a weapon positioning assembly for positioning the weapon in a stored position and a release position. The weapon positioning assembly comprises a weapon support rack and a pair of fore and aft links having first and second ends. The first ends of the links are pivotally coupled to the aircraft and the second ends are pivotally coupled to the rack. An actuator assembly is coupled by its first end to the aircraft and by its second end to the weapon positioning assembly. It is adapted to move the positioning assembly from the stored position to the release position. Fore and aft weapon attaching devices for releasably locking the weapon to the rack is attached to the weapon positioning assembly. The weapon releasing devices are adapted to lock the weapon to the rack when the weapon position assembly is in the stored position and to only unlock the weapon from the positioning assembly when it is in the release position. Thus, upon actuation, the rack with the weapon locked thereto is rotated in a downward and forward direction and automatically released when the release position is reached.

摘要翻译： 本发明是用于飞行器的武器分配系统。 该系统包括用于将武器定位在存储位置和释放位置的武器定位组件。 武器定位组件包括武器支撑架和具有第一和第二端的一对前后链节。 链节的第一端枢转地联接到飞行器，并且第二端枢转地联接到齿条。 致动器组件通过其第一端连接到飞机并且其第二端连接到武器定位组件。 它适于将定位组件从存储位置移动到释放位置。 用于将武器可释放地锁定到机架的前后武器附接装置附接到武器定位组件。 武器释放装置适于当武器位置组件处于存储位置时将武器锁定到机架上，并且当武器处于释放位置时仅从定位组件解锁武器。 因此，一旦致动，装有武器的机架锁定在其上，向下和向前方向旋转，并且在达到释放位置时自动释放。

公开(公告)号：US4049222A

公开(公告)日：1977-09-20

申请号：US707139

申请日：1976-07-20

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： B64D1/04

CPC分类号： B64D1/04

摘要： A 30 inch ejector rack, for use with an aircraft, to support and release and/or forcibly eject a nuclear store (or a large conventional store) from the aircraft, with both the ejector rack and the store carried internal of the aircraft. Unlike the prior art, this ejector rack structurally incorporates, among other novel fundamental features and/or improvements: mechanical "spools", rather than valves or orifices, to obtain pitch or tilt of the store during forced ejection; bypass grooves near the end (i.e., the bottom) of the piston stroke to provide snubber action, thus preventing damage to the store due to impact of the piston and the store during ejection; cartridge debris screens in the gas system of the ejection rack and, structural configuration which permits quick removal of piston components for rapid and easy cleaning, without necessitating the complete disassembly of the ejector rack, or even the removal of the rack from the aircraft to which it is attached.

摘要翻译： 与飞机一起使用的30英寸喷射器架，用于从飞机支撑和/或强制弹出核存储（或大型常规商店），两个喷射器架和在飞机内部运送的商店。 不同于现有技术，除了其他新颖的基本特征和/或改进之外，该喷射器架结构上包括机械“线轴”而不是阀或孔，以在强制喷射期间获得商店的俯仰或倾斜; 在活塞行程的端部（即底部）附近的旁路槽以提供缓冲作用，从而防止由于活塞和存储在喷射期间的冲击而对存储器造成的损坏; 喷射架的气体系统中的墨盒碎片屏幕，以及允许快速清除活塞部件以快速且容易地清洁的结构配置，而不需要完全拆卸喷射器架，或甚至从机架上移除机架 它是附加的。