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公开(公告)号：US08500067B2
公开(公告)日：2013-08-06
申请号：US13567015
申请日：2012-08-04
IPC分类号： B64C1/32
CPC分类号： B64C1/30 , A63H27/001 , A63H27/02 , B64C15/00 , B64C19/00 , B64C39/028 , B64C2201/028 , B64C2201/042 , B64C2201/104 , B64C2201/127 , B64C2201/165 , B64C2201/18 , B64C2201/187 , B64C2201/201 , B64D1/14 , B64D9/00 , B64D27/26
摘要： An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust-vectoring (“T/V”) module and a second T/V module, and an electronics module. The electronics module provides commands to the two T/V modules. The two T/V modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as T/V modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.
摘要翻译： 描述了一种无人驾驶飞机。 飞行器包括机身，连接到机身的后部的一对翼片，连接到机身的底部的一对二面支架，第一推力矢量（“T / V”）模块和第二T / V模块，以及电子模块。 电子模块向两个T / V模块提供命令。 两个T / V模块被配置为通过直接控制飞行器的俯仰，滚动和偏航中的每一个的推力矢量来向飞行器提供侧向和纵向控制。 使用直接连接的电动机作为T / V模块，使飞机能够在大范围的空速下执行紧半径的转弯。
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公开(公告)号：US20080142635A1
公开(公告)日：2008-06-19
申请号：US11825758
申请日：2007-07-09
摘要： A system for enabling the safe landing of an aircraft during an in-flight emergency is provided. The system includes a plurality of onboard devices for releasably securing a plurality of wings to a fuselage, and a non-electric module for activating said onboard devices. Said onboard devices are released to separate said wings from the fuselage.
摘要翻译： 提供了一种用于在飞行中紧急情况下使飞机安全着陆的系统。 该系统包括多个用于将多个翼片可释放地固定到机身的车载装置，以及用于启动所述车载装置的非电动模块。 所述车载装置被释放以将机翼与机身分开。
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公开(公告)号：US5954296A
公开(公告)日：1999-09-21
申请号：US25479
申请日：1998-02-18
CPC分类号： B64C1/32
摘要： An aircraft canopy fracturing system includes a canopy having fore and aft portions and a region that is severable from the canopy to provide an opening therethrough for the egress of aircraft occupants. The severable region has a shape that inhibits passage of the severable region through the opening created in the canopy once the severable region is freed from the canopy and is displaced aftward relative to the canopy. The canopy fracturing system also may include one or more mechanisms that will impart an aftward impulse to the severable region of the canopy once it has been severed and freed from the remainder of the canopy.
摘要翻译： 飞机冠层压裂系统包括具有前部和后部的顶盖以及可与篷盖分离的区域，以为飞机乘员的出口提供穿过其的开口。 可分割区域具有禁止可分割区域穿过冠层中产生的开口的形状，一旦可分割区域离开树冠并相对于顶盖向后移动。 冠层压裂系统还可以包括一个或多个机构，其将一旦被切断并且从冠层的其余部分中释放就会向顶篷的可分割区域赋予后向冲击。
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44.发明授权
公开(公告)号：US4892271A
公开(公告)日：1990-01-09
申请号：US255398
申请日：1988-10-11
申请人： Andrew M. Elford
发明人： Andrew M. Elford
CPC分类号： B64C1/06 , B29C59/103 , B29C59/106 , B64C1/32 , B64D25/10 , H01T19/00
摘要： Apparatus for and a method of rendering selected areas 17, 18 of an aircraft canopy 2 receptive to an adhesive by means of which a detonating cord 7 is attached in loop form to the canopy, to facilitate fracture of the canopy for pilot ejection in an emergency, comprises pretreating those areas 17, 18 by corona discharge. The canopy 2 is mounted in a jig 10 shaped to conform with the canopy and having rebates 11 for accommodating discharge electrodes 12 located at a distance from the canopy 2. A pump 16 is provided to remove ozone formed due to the discharge and trapped between the canopy 2 and the jig 10.
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公开(公告)号：US4580746A
公开(公告)日：1986-04-08
申请号：US499494
申请日：1983-05-31
申请人： Walter R. Peck
发明人： Walter R. Peck
CPC分类号： B64D25/12
摘要： A capsule and rocket extraction system for providing an inflight escape system for the pilot of a damaged aircraft. The system comprises a capsule that is separable from the main fuselage of the aircraft and a rocket for extracting the pilot from the capsule. A control system is carried by the capsule for sensing the capsule's speed, altitude and attitude, and for actuating only the rocket to extract the pilot directly from the capsule when the speed, altitude and attitude are at predetermined conditions, and for sequentially actuating a capsule separation device to separate the capsule from the main fuselage and then actuating the rocket to extract the pilot from the separated capsule when the speed, altitude and attitude are at different predetermined conditions.
摘要翻译： 一种胶囊和火箭提取系统，用于为受损飞机的飞行员提供飞行逃生系统。 该系统包括可与飞行器的主机身分离的胶囊和用于从胶囊提取飞行员的火箭。 控制系统由胶囊承载，用于感测胶囊的速度，高度和姿态，并且当速度，高度和姿态处于预定条件下时，仅驱动火箭从胶囊中直接提取飞行员，并且用于依次致动胶囊 分离装置，以使胶囊与主机身分离，然后当速度，高度和姿态处于不同的预定条件时，致动火箭从分离的胶囊中提取飞行员。
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46.发明授权Device for maintaining a detonating cord against a transparent aircraft canopy member 失效用于将引爆线保持在透明飞机机盖部件上的装置
公开(公告)号：US4512538A
公开(公告)日：1985-04-23
申请号：US470944
申请日：1983-03-01
申请人： Jules H. P. Devienne
发明人： Jules H. P. Devienne
CPC分类号： B64C1/32
摘要： Device for maintaining a detonating cord against a transparent aircraft canopy member which is of the type comprising a closed sheath within which is placed the cord. The device also has an outer envelope, whereof a first part, surrounded by the closed sheath, is maintained against the transparent member and whereof a second part is fixed to a structural component of the aircraft cockpit.
摘要翻译： 用于将引爆线保持在透明飞机顶盖部件上，该透明机顶盖部件的类型包括封闭的鞘，其中放置有绳索。 该装置还具有外封套，其中由封闭护套围绕的第一部分保持在透明构件上，并且其中第二部分固定到飞行器驾驶舱的结构部件。
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公开(公告)号：US4275858A
公开(公告)日：1981-06-30
申请号：US945106
申请日：1978-09-25
摘要： A Panel Breaking Apparatus comprising at least one fusible conductor having at least one region of increased fusibility and embedded in intimate contact with the panel material and connected to a source of electrical power operable to produce a high-energy pulse of current sufficient to fuse the conductor and thus to break the panel.
摘要翻译： 一种面板破裂装置，包括至少一个易熔体导体，其具有至少一个具有增加的可熔性的区域，并且嵌入与面板材料的紧密接触并且连接到电源，可操作地产生足以熔化导体的高能量脉冲 从而打破了面板。
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公开(公告)号：US4102011A
公开(公告)日：1978-07-25
申请号：US809837
申请日：1977-06-24
CPC分类号： B64C1/1407 , E05D7/12 , E05D2007/128 , E05Y2900/502 , E05Y2900/531 , Y10T16/53605
摘要： An aircraft door adapted to pivot about a pair of vertical hinges is detachably fixed to the door frame by a secondary joint at each hinge. Retraction of a short horizontal pin at each secondary joint releases the door for jettison.
摘要翻译： 适于围绕一对垂直铰链枢转的飞机门通过每个铰链处的次级接头可拆卸地固定到门框。 在每个次级接头处缩短一个短的水平销释放门以进行抛弃。
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公开(公告)号：US3919939A
公开(公告)日：1975-11-18
申请号：US51996074
申请日：1974-11-01
申请人： US NAVY
发明人： MURRAY JAMES L , SIRES LAWRENCE M
摘要： A method and apparatus is provided for suppressing light flashes from a linear-shaped charge, for example, on a cargo dispenser. Undesirable light flashes may be suppressed by either manufacturing the linear shaped charge container from silver or placing a container of chemical suppressant along the external skin of the cargo section at the cutting line of the linear shaped charge or both.
摘要翻译： 提供了一种方法和装置，用于例如在货物分配器上抑制线形电荷的闪光。 可以通过从银制造线性形状的充电容器或者沿着线性成形电荷的切割线沿着货物部分的外部皮肤放置化学抑制剂的容器或两者来抑制不期望的闪光。
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