公开(公告)号：EP3224143A1

公开(公告)日：2017-10-04

申请号：EP15778154.3

申请日：2015-09-25

申请人： Raytheon Company

发明人： KESHTKAR, Reza ,  BREDEHOFT, Kevin T.

IPC分类号： B64G1/64

CPC分类号： B64G1/645 ,  B64G1/641 ,  F16B7/0426 ,  F16F7/12 ,  F42B15/36

摘要： An energy absorbing restraint device for a clamp system (100) is disclosed. The clamp system can include a releasable clamp (102) having first and second ends, a securing mechanism (108) connecting the ends and facilitating clamping and release of the clamp, and a restraint device (110) for containing the clamp after release. An energy absorbing member (112) supported about the restraint device can be configured to interface with the releasable clamp to dissipate the impact energy of the releasable clamp and decrease the magnitude of impact shock about the restraint device as created by the release of the clamp.

摘要翻译： 公开了一种用于夹紧系统的能量吸收限制装置。 该夹紧系统可以包括具有第一端和第二端的可释放夹具，连接端部并便于夹紧和释放夹具的固定机构以及用于在释放后容纳夹具的约束装置。 围绕约束装置支撑的能量吸收构件可以构造成与可释放夹具接合以消散可释放夹具的冲击能量并且减小由夹具释放产生的约束装置周围的冲击震动的量值。

公开(公告)号：EP3027512B1

公开(公告)日：2017-05-03

申请号：EP14747613

申请日：2014-07-31

申请人： AIRBUS SAFRAN LAUNCHERS SAS

发明人： MEDINA FELIPE ,  PREAUD LUC

IPC分类号： F42B15/36 ,  B64G1/64 ,  F42B15/38

CPC分类号： F42B15/38 ,  B64G1/645 ,  F42B15/36

公开(公告)号：EP3145812A1

公开(公告)日：2017-03-29

申请号：EP15796897.5

申请日：2015-05-19

申请人： MacDonald, Dettwiler and Associates Inc.

发明人： SACHDEV, Tej Singh ,  LYMER, John Douglas ,  BRYAN, Richard Andrew ,  FRANCETIC, Branko ,  PEACOCK, Paul Robert ,  KRIMBALIS, Peter Panagiotis

IPC分类号： B64G1/64

CPC分类号： B64G1/641 ,  B64G1/645

摘要： There is disclosed a Payload Ejection System (PES) able to store any set of payloads for launch and eject that set of payloads at a controlled speed with a low tumble rate while accommodating any offset centre of mass within a restricted volume. The need for ballasting or balancing is eliminated thus freeing up the design space for these payloads. Insensitivity to centre of mass location is enabled by the use of a deployment hinge assembly arrangement which uses two or more non-parallel folding hinge arrangements that allow for linear motion of the output link in one direction while restricting the motion all other directions. One embodiment of the current PES concept uses four (4) hinge panel assemblies, selected to provide optimal stiffness around the entire mechanism. The stiffness of the PES is integral to managing offset centre-of-mass locations by allowing the mechanism to translate the effective force vector to the center of mass location.

摘要翻译： 公开了一种有效载荷喷射系统（PES），其能够存储用于发射的任何一组有效载荷，并以低转速的受控速度弹出该组有效载荷，同时在受限制的体积内容纳任何偏移质心。 消除了压载或平衡的需要，从而释放了这些有效载荷的设计空间。 通过使用展开铰链组合装置可实现对质心定位中心的不敏感，所述部署铰链组件装置使用两个或更多个不平行的折叠铰链装置，其允许输出连杆在一个方向上的线性运动，同时限制所有其它方向的运动。 当前PES概念的一个实施例使用四（4）个铰链板组件，其被选择以在整个机构周围提供最佳刚度。 通过允许机构将有效力向量转换到质心位置，PES的刚度对于管理偏移质心位置是一体的。

公开(公告)号：EP3027512A1

公开(公告)日：2016-06-08

申请号：EP14747613.9

申请日：2014-07-31

申请人： Airbus Defence and Space SAS

发明人： MEDINA, Felipe ,  PREAUD, Luc

IPC分类号： B64G1/64 ,  F42B15/38

CPC分类号： F42B15/38 ,  B64G1/645 ,  F42B15/36

摘要： The method and the device according to the invention allow two elements (1, 2) that are fixed to one another by two respective connecting plates (10, 20) belonging to the first element (1) and to the second element (2) to be separated linearly. The connecting and separating means are combined and consist of a layer (30). The connecting means consist of brazing, adhesive or resin, while the separating means consist of thermite. All of these elements can also be laid in layers. Electrically triggering this assembly (30) causes it to heat up quickly and locally and therefore allows the two elements (1, 2) to be separated. Application to the separation of two stages of an aeronautical launcher.

公开(公告)号：EP3027511A1

公开(公告)日：2016-06-08

申请号：EP14744870.8

申请日：2014-07-31

申请人： Airbus Defence and Space SAS

发明人： MEDINA, Felipe ,  PREAUD, Luc

IPC分类号： B64G1/64 ,  F42B15/38

CPC分类号： F42B15/38 ,  B64G1/641 ,  B64G1/645

摘要： The method and the device according to the invention allow two elements (1, 2) that are fixed to one another by two respective connecting surfaces (10, 20) belonging to the two elements (1, 2) to be separated linearly. The connecting layer (30) is placed between the two connecting pieces (10, 20). Thermite (15) is used to make this layer of connecting means (30) melt. This thermite may be positioned on the other side of the first connecting piece (10) towards the first element (1), a heat shield plate (17) completing this setup. The thermite may also be placed in groves made on the connecting surface (22) of the second connecting plate (20) so as to be in direct contact with the layer of connecting means (30). Application to the separation of two stages of an aeronautical launcher.

公开(公告)号：EP2319764B1

公开(公告)日：2013-07-03

申请号：EP10185980.9

申请日：2010-10-01

申请人： Thales

发明人： Legrand, Silvain ,  Baudasse, Yannick

IPC分类号： B64G1/22 ,  B64G1/64

CPC分类号： B64G1/222 ,  B64G1/443 ,  B64G1/645

公开(公告)号：EP2570349A2

公开(公告)日：2013-03-20

申请号：EP12006275.7

申请日：2012-09-06

申请人： Astrium GmbH

发明人： Wagner, Adalbert ,  Nussbaumer, Tobias

IPC分类号： B64G1/64

CPC分类号： B64G1/645

摘要： Die Erfindung beschreibt eine Vorrichtung zum nicht-explosiven Aktuieren einer Komponente, insbesondere einer Raumfahrtkomponente. Diese umfasst ein Gehäuse (10) sowie einen zentral in dem Gehäuse (10) angeordneten Bolzen (20). Der Bolzen (20) ist zwischen einer ersten Position, in der ein äußerer Abschnitt (23) des Bolzens (20) in Bezug auf das Gehäuse (10) außerhalb des Gehäuses (10) angeordnet ist, und einer zweiten Position, in der der äußere Abschnitt (23) des Bolzens (20) innerhalb des Gehäuses (10) angeordnet ist, bewegbar. Die Komponente umfasst weiterhin eine Feder (30), die zwischen dem Gehäuse (10) und dem Bolzen (20) angeordnet ist. Eine, zwischen einer ersten und einer zweiten Stellung, drehbar in dem Gehäuse (10) angeordnete Aktuatorhülse (40) umfasst einen als Bahnkurve (BK) ausgebildeten Führungsabschnitt (41), entlang dem der Bolzen (20) während einer Drehung der Aktuatorhülse (40) geführt wird.

摘要翻译： 装置（1）具有壳体（10）和布置在壳体中的螺栓（20）。 螺栓在螺栓的外部部分布置在壳体的外侧的位置和外部部分布置在壳体的内侧中的另一位置之间移动。 弹簧（30）即螺旋弹簧布置在壳体和螺栓之间。 致动器壳体（40）以可旋转的方式布置在壳体中，并且具有被设计为轨迹的引导部分（41），其中螺栓在壳体旋转期间沿着轨迹被引导。

公开(公告)号：EP2537759A1

公开(公告)日：2012-12-26

申请号：EP11744734.2

申请日：2011-02-18

申请人： Mitsubishi Heavy Industries, Ltd.

发明人： KOBAYASHI, Mitsuru ,  SUZUKI, Keiji

IPC分类号： B64G1/64 ,  F16B2/08

CPC分类号： F16B1/0014 ,  B64G1/645

摘要： A coupling and separating device is provided which can reduce a separation impact when separating a launch vehicle and a structure. The coupling and separating device is provided with a clamp band 6 which has blocks 3 and a strap 2, and a coupling section 4. The block 3 engages an installation member 20 of the launch vehicle and the structure 20 installed on the installation member 20. The strap 2 maintains the block 3 from outside. The coupling section 4 couples or separates the end sections 2a of the strap 2. The strap 2 is formed of shape memory alloy and is provided with a stretching section 11 which stretches through heating.

摘要翻译： 的联接和分离装置提供一种能够减少分离冲击时分离运载火箭和的结构。 联接和分离装置被提供有一夹紧条6其嵌段3和表带2和耦合部分4。块3接合在运载火箭的安装构件20和结构20安装在安装构件20 表带2从外侧保持块3。 连结部4耦合或分离所述带2带2的端部2a形成的形状记忆合金制成，并设置有通过加热拉伸的拉伸部11。

公开(公告)号：EP2468632A3

公开(公告)日：2012-09-12

申请号：EP12160728.7

申请日：2009-09-22

申请人： Eads Casa Espacio S.L.

发明人： Plaza Baonza, Miguel Ángel

IPC分类号： B64G1/22 ,  B64G1/64 ,  F16B21/12

CPC分类号： B64G1/222 ,  B64G1/645 ,  F16B21/12 ,  Y10T24/45225 ,  Y10T24/45466 ,  Y10T403/593

摘要： Device (1) for the restraint and release of a deployable body mounted on a support structure, the device (1) being operable between a stowed condition and a released condition, and comprising:
- a pair of subassemblies (2, 3), each for being attached to either the deployable body or the support structure, these subassemblies (2, 3) comprising mating surfaces which interlock with one another in the stowed condition to substantially prevent lateral movement of the deployable body relative to the support structure;
- a releasable tensioned element (5) which is connected to both of the subassemblies (2, 3), exerting a compressive pre-load action on the said subassemblies (2, 3) that keep them together;
- a force measurement system (6) that allows monitoring the cited compressive pre-load action applied;
- a releasing device (7) for releasing the cited pre-load, allowing the free separation of the subassemblies (2, 3);
- further comprising a tensioning mechanism embedded in the device (1) such that it applies a substantially pure-tension pre-load to the releasable tensioned element (5),
- and further comprising substantial mechanical spherical articulation capability, guaranteeing tilt misalignment adjustment of the stowed body relative to the support structure and the reduced hyperstaticity of body to support structure restriction, by substantially cancelling the moments exchange among them.

公开(公告)号：EP2451711A2

公开(公告)日：2012-05-16

申请号：EP10729891.1

申请日：2010-07-08

申请人： Astrium SAS

发明人： BEHAR, Jacques

IPC分类号： B64G1/64 ,  F42B15/36

CPC分类号： F42B15/38 ,  B64G1/645 ,  Y10T29/49826 ,  Y10T29/53096

摘要： The invention relates to a device (12) for linear separation of a first part (2) and a second part (4). The first part is linearly connected to the second part (4). The device comprises a heat source (12) applied to the first part (2), which applies a heat stimulus to the first part (2) such as to separate the first part (2) from the second part (4) by thermal deformation of the first part (2).