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公开(公告)号：US5398614A
公开(公告)日：1995-03-21
申请号：US265461
申请日：1994-06-10
Applicant: Walter Koenig
Inventor： Walter Koenig
IPC: F42B10/56
CPC classification number: F42B10/56
Abstract: A cover or apron interposed between a ballute and the aft cover of a submtion for delaying deployment of the ballute and preventing the ballute from contacting the aft cover during deployment.
Abstract translation: 插入在子弹药之间的气球和后盖之间的盖子或挡板，用于延迟部件的推出，并防止球团在展开期间与后盖接触。
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公开(公告)号：US5174527A
公开(公告)日：1992-12-29
申请号：US580244
申请日：1990-09-10
Applicant: Anthony D. Kasher
Inventor： Anthony D. Kasher
Abstract: An annular spinning parachute is composed of an annular canopy symmetrical about an apex, suspension lines of substantially the same length and interconnected together at the canopy apex and extending radially outwardly therefrom across the canopy and downwardly therefrom for coupling to an object supported by the parachute, and centerlines interconnected with the suspension lines at the canopy apex and extending downwardly therefrom for coupling to the object supported by the parachute. The annular canopy includes fabric panels each having a generally trapezoidal shape defined by a pair of opposing inner and outer borders with the outer border being greater length than the inner border and a pair of opposing side borders of substantially the same length. The annular canopy also includes inner and outer lateral bands respectively extending along and connected to the inner and outer borders of the fabric panels so as to dispose the panels in circumferentially spaced relation with respect to one another upon inflation of the canopy. The inner and outer bands and spaced panels define a central opening in the canopy having thhe canopy apex at the center of the opening and a plurality of exhaust vents arranged in alternating relation with the panels between the side borders of adjacent pairs of the panels.
Abstract translation: 环形旋转降落伞由围绕顶点对称的环形舱盖组成，悬挂线基本上相同的长度，并且在冠层顶端处互连在一起，并从其上径向向外延伸穿过冠层并向下延伸，用于联接到由降落伞支撑的物体， 以及与冠层顶点处的悬挂线相互连接并且向下延伸的中心线，用于联接到由降落伞支撑的物体。 环形顶盖包括各自具有由一对相对的内部和外部边界限定的大致梯形形状的织物面板，外部边界的长度大于内部边界的长度以及基本上相同长度的一对相对的侧边缘。 环形罩还包括分别沿着织物面板的内边界和外边缘延伸并连接到织物面板的内边缘和外边缘的内侧和外侧边带，以便在罩盖膨胀时将面板相对于彼此以周向间隔开的关系布置。 内部和外部带和间隔开的面板限定在顶盖中的中心开口，其具有位于开口中心处的顶盖顶点和与相邻面板对侧边缘之间的面板交替关系排列的多个排气口。
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公开(公告)号：US5169093A
公开(公告)日：1992-12-08
申请号：US604468
申请日：1990-10-29
Applicant: Rainer Schoffl
Inventor： Rainer Schoffl
Abstract: A parachute associated with an object unfolds faster in an airstream if the object is first accelerated in the direction of descent. This principle can be applied advantageously to a mine system combating military targets from the air because the time between starting from an ambush position in the terrain to the onset of searching movements in the air can be shortened.
Abstract translation: 如果物体首先沿下降方向加速，与物体相关联的降落伞在气流中展开更快。 这个原则可以有利地应用于从空中对抗军事目标的地雷系统，因为可以缩短从地形中的埋伏位置开始到空中搜索运动的开始之间的时间。
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公开(公告)号：US5054397A
公开(公告)日：1991-10-08
申请号：US517162
申请日：1990-05-01
Applicant: Paul C. Hans , Gary C. Rosenfield
Inventor： Paul C. Hans , Gary C. Rosenfield
IPC: F42B10/56
CPC classification number: F42B10/56
Abstract: Parachute ejection and recovery system for rockets which protects and permits recovery of the entire rocket after launch including means for cooling ejection gases, means for directing the cooler ejection gases for using in ejection, the nose cone and parachute therefrom during flight, and means for controlling descent of the rocket body, its nose cone and a parachute associated therewith.
Abstract translation: 用于火箭的降落伞弹射和恢复系统，其保护和允许发射后的整个火箭的恢复，包括用于冷却喷射气体的装置，用于引导冷却器喷射气体用于喷射使用的装置，飞行期间的鼻锥和降落伞，以及用于控制的装置 火箭体的下降，其鼻锥和与之相关的降落伞。
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公开(公告)号：US4889030A
公开(公告)日：1989-12-26
申请号：US254680
申请日：1988-09-22
Applicant: Werner Grosswendt , Klaus Unterstein
Inventor： Werner Grosswendt , Klaus Unterstein
Abstract: A projectile has at two parts (3, 4) axially arranged one behind the other and mutually linked, of which at least one contains a deployable parachute (6, 6'). In order to achieve a design that ensures a smooth and reliable separation of the parts (3, 4), followed by the deployment of the parachute (6, 6'), both parts (3, 4) are mutually linked by radial bolts (19) that can be radially actuated by the gas pressure generated by at least one pyrotechnic load (15) and radially moved by the gas pressure, thus separating the two parts (3, 4). The pyrotechnic load (15) can be ignited by a fuse (9).
Abstract translation: PCT No.PCT / EP87 / 00674 Sec。 371日期：1988年9月22日 102（e）1988年9月22日PCT PCT日期：1987年11月5日PCT公布。 出版物WO88 / 05523 日期：1988年7月28日。射弹具有两个部分（3,4），轴向布置在彼此之间并相互连接，其中至少一个包含可展开的降落伞（6,6'）。 为了实现确保部件（3,4）平滑可靠分离的设计，随后部署降落伞（6,6'），两个部件（3,4）都通过径向螺栓（ 19），其可以由至少一个烟火负载（15）产生的气体压力并由气体压力径向移动，从而分离两个部分（3,4）。 烟火负载（15）可以被保险丝（9）点燃。
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Patent Agency Ranking
公开(公告)号：US4753171A
公开(公告)日：1988-06-28
申请号：US16547
申请日：1987-02-19
Applicant: Lothar Stessen
Inventor： Lothar Stessen
Abstract: A carrier projectile for aerodynamically braked submunition which can be ejected rearwardly from the tail end of the carrier projectile while contacting a cup-shaped base of the projectile. The carrier projectile has the inner edge of the fabric of a braking sail retained within the cup-shaped recess of the base of the projectile, with the outer edge of the fabric of the sail being equipped with centrifugal masses or flyweights mounted in proximity to the opening of the cup-shaped recess in the base. Provision is made to arrange the fabric of a radially outwardly tensionable braking sail in the already available recess in the base of the projectile, the braking sail being extended through the pulling action exerted thereon from the centrifugal flyweights.
Abstract translation: 一种用于空气动力学制动的子弹药的载体抛射体，当与运载体的杯形基座接触时，可从载体抛射体的尾端向后喷射。 载体抛射体具有保持在射弹基部的杯形凹部内的制动帆布织物的内边缘，其中帆的织物的外边缘配备有离心质量或安装在接近 在基座中打开杯形凹槽。 布置了将径向向外张紧的制动帆布的织物布置在弹丸基座中已经可用的凹部中，制动帆通过从离心飞轮施加在其上的拉动作用而延伸。
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公开(公告)号：US4632010A
公开(公告)日：1986-12-30
申请号：US718399
申请日：1985-04-01
Applicant: Waymon Humphries , John Bryant , Richard C. Eklund , Donald C. Hayes , Peter Ferko
Inventor： Waymon Humphries , John Bryant , Richard C. Eklund , Donald C. Hayes , Peter Ferko
CPC classification number: F42B10/56 , F42B12/70 , F42C15/184 , F42C15/21
Abstract: An AIRBOC chaff deployment apparatus comprising a canister with a wind flapttached externally to the canister and connected to a drogue chute that is housed inside the canister. The drogue chute is situated atop a main chute that is atop a release mechanism, which is atop a fuze and that is atop a chaft payload, all of which is housed inside the canister. When the AIRBOC is dropped from a plane, the wind flap extends, pulling out the drogue chute. The drogue chute in turn activates the release mechanism which frees the drogue chute to pull out the main chute to which the drogue chute is connected. The deployment of the main chute causes a force greater than 40 lbs to be applied to the release mechanism, resulting in the chaff payload being released from the canister and the fuze being activated, consequently detonating the released chaff payload.
Abstract translation: 一种AIRBOC谷壳部署装置，其包括具有附接到罐的外部并连接到容纳在罐内的锥形滑槽的风瓣的罐。 锥形滑槽位于主滑槽顶部，位于引擎顶部，位于一个引信顶部，位于一个有效载荷的顶部，所有这些都位于罐内。 当空中客车从飞机上掉下来时，风翼延伸，拉出冷气滑道。 锥形滑道又激活释放机构，释放滑梯滑槽以拉出与滑道滑槽连接的主滑槽。 主滑槽的部署导致大于40磅的力施加到释放机构，导致谷壳有效载荷从罐中释放并且引信被激活，从而引爆释放的谷壳有效载荷。
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68.发明授权
公开(公告)号：US4584943A
公开(公告)日：1986-04-29
申请号：US628751
申请日：1984-07-09
Applicant: Norbert Vavra , Jens Seidensticker
Inventor： Norbert Vavra , Jens Seidensticker
CPC classification number: F42B12/10 , F42B10/56 , F42B30/006 , F42C13/006 , F42C19/06
Abstract: Missile head to be released in an airplane cargo drop or from a flying body. The missile head has a target-sensor having a transmitter, a receiver, an antenna and an explosive charge ignitable by a target location signal. In order not to interfere with the function of the explosive charge, it is best that the antenna be located in front of the target-sensor with respect to the flight direction, while the target-sensor is located behind the explosive charge with respect to the flight direction. The connection between the antenna and the target-sensor is provided by a wave carrier filled with explosives.
Abstract translation: 导弹头在飞机货物下降或从飞行的身体释放。 导弹头具有目标传感器，其具有发射器，接收器，天线和由目标位置信号可点燃的炸药。 为了不干扰爆炸物的功能，天线最好相对于飞行方向位于目标传感器的前方，而目标传感器位于爆炸物的后面。 飞行方向。 天线和目标传感器之间的连接由装有爆炸物的波浪载体提供。
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公开(公告)号：US4335826A
公开(公告)日：1982-06-22
申请号：US205961
申请日：1980-08-26
Applicant: Henry M. Prain , Andrew M. Scott
Inventor： Henry M. Prain , Andrew M. Scott
CPC classification number: F42B10/56
Abstract: A container 10 has a release device which comprises a flexible plate 14 and a line 17 attached to the contents 11 of the container; when a force is applied to line 17 it is communicated to plate 14 which flexes and is pulled clear of a retaining flange 13 to release contents 11. As shown, the force is applied to the plate 14 via washers 18,19 and 20. Plate 14 preferably has radially directed fingers. The container may constitute part of a rocket-launched projectile and may be used to release a parachute at a desired height, the other end of line 17 being fixed.
Abstract translation: PCT No.PCT / GB80 / 00005 Sec。 371日期1980年8月26日 102（e）1980年8月26日PCT PCT 1月9日，1980 PCT。 出版物WO80 / 01375 1980年7月10日。容器10具有释放装置，其包括柔性板14和连接到容器的内容物11上的管线17; 当力施加到管线17上时，它被传递到板14，板14弯曲并被拉出而脱离保持凸缘13以释放内容物11.如图所示，力通过垫圈18,19和20施加到板14上。板 14优选地具有径向指向的指状物。 容器可以构成火箭发射的射弹的一部分，并且可以用于在期望的高度释放降落伞，线17的另一端是固定的。
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公开(公告)号：US3943854A
公开(公告)日：1976-03-16
申请号：US460480
申请日：1974-04-12
Applicant: Kurt Zwicker
Inventor： Kurt Zwicker
Abstract: Ejection head for projectiles, rockets or the like having at least one ejection section including a carrier plate, a plurality of ejection tubes for containing active elements mounted annularly about the carrier plate, a descent controller connected to the carrier plate wherein the tubes are movable from a folded position to a spread-apart position for discharging the active elements contained therein. A locking device is provided for locking the tubes in the folded position and a spreading device is provided for spreading the tubes apart with a pyrotechnical element being provided for generating compressed gas for triggering the locking device to unlock the ejection tubes and causing the spreading device to spread the ejection tube apart.
Abstract translation: 具有至少一个包括承载板的喷射部分的弹丸，火箭等的喷射头，用于容纳围绕载板环形地安装的有源元件的多个喷射管，连接到载体板的下降控制器，其中管可从 折叠位置到用于排出其中包含的有源元件的扩展位置。 提供锁定装置用于将管锁定在折叠位置，并且设置扩展装置用于将管分开，提供用于产生压缩气体的烟火元件，用于触发锁定装置以解锁喷射管并使扩散装置 将喷射管分开。
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