专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2015199567A1 METHOD AND APPARATUS FOR DEPLOYING A PARACHUTE FROM FALLING HELICOPTERS, AIRCRAFT AND LAND VEHICLES AND FOR AERIAL BRAKING 审中-公开
标题翻译：从落地直升机，飞机和陆地车辆以及空中制动器中分配的方法和装置
公开(公告)号：WO2015199567A1
公开(公告)日：2015-12-30
申请号：PCT/RO2015/000015
申请日：2015-06-15
申请人： RÎNEA, Tiberiu Emil Ilie
发明人： RÎNEA, Tiberiu Emil Ilie
IPC分类号： B64D17/80 , B64D17/72 , B64D25/00
CPC分类号： B64D17/80 , B64D17/725 , B64D25/00
摘要： Method and apparatus for bailing with logic ballistic parachute for special, short, complex falls in helicopters, aircrafts and land vehicles and aerial braking The invention comprises a group of principles and methods associated so that it forms a new, innovative principle, which, together bails, from falling caused by damage, helicopters, planes, objects, regardless of the external weather conditions. Uses a microcomputer (1) which actively drives the parachute deployment through logical and anticipatively commands, correlated with the status measurements from the damaged aircraft together with spatial measurements for the landing spot. The launching of the parachute is done ballisticaly with a mini-cannon (10) and then with a carrier rocket (12) for the synchronized passing between the helicopter rotor's blades. The launching is reversed, upwards, on a short half-circle route, arriving forcefully open besides the aircraft. Both planes and helicopters can be bailed. A simple non-destructive test stand can be built for invention homologation and unitary series production.
摘要翻译：直升机，飞机和陆地车辆的特殊，短路，复杂下降的逻辑弹道降落伞和空中制动的方法和装置本发明包括一组相关的原理和方法，从而形成一种新的创新原则，，由于受到损坏，直升机，飞机，物体的损失，无论外部天气情况如何。使用微型计算机（1），其通过逻辑和预期命令主动地驱动降落伞部署，与受损飞机的状态测量相关联，以及着陆点的空间测量。降落伞的发射是用小型炮（10）进行弹道导弹，然后用载体火箭（12）进行，直升机转子叶片之间的同步通过。发射反转，向上，在短的半圈路线上，除了飞机外还强力打开。飞机和直升机都可以保释。可以建立一个简单的无损检测台，用于发明同源化和单一系列生产。

2. 发明申请

WO2014080409A1 SAFETY APPARATUS FOR A MULTI-BLADE AIRCRAFT 审中-公开
标题翻译：多叶飞机的安全装置
公开(公告)号：WO2014080409A1
公开(公告)日：2014-05-30
申请号：PCT/IL2013/050971
申请日：2013-11-25
申请人： WISEC LTD.
发明人： TSALIAH, Amir , KRAUSS, Ran
IPC分类号： B64D17/72 , B64C27/08
CPC分类号： B64D17/80 , B64C39/028 , B64C2201/027 , B64C2201/185 , B64D17/72 , B64D17/725
摘要： The present invention provides safety apparatus for a multi-blade aircraft, comprising an expandable and collapsible parachute assembly having a plurality of inflatable tubes, a plurality of electrically triggered gas generators connected to a support surface of a multi-blade aircraft, and an on-board control unit for initiating triggering of said plurality of gas generators, wherein an outlet end of each of said plurality of gas generators is connected to, and in fluid communication with, a bottom end of one of said plurality of tubes, allowing said parachute assembly to be fully expanded upon generation of inflating gas by each of said plurality of gas generators.
摘要翻译：本发明提供了一种用于多叶片飞行器的安全装置，其包括具有多个可充气管的可膨胀和可折叠降落伞组件，连接到多叶片飞行器的支撑表面的多个电触发气体发生器，用于启动所述多个气体发生器的触发的板控制单元，其中所述多个气体发生器中的每一个的出口端连接到所述多个管之一的底端并与其流体连通，允许所述降落伞组件在由所述多个气体发生器中的每一个产生膨胀气体时完全膨胀。

3. 发明申请

WO2017139803A1 AIRCRAFT PARACHUTE SYSTEM 审中-公开
标题翻译：飞机松动系统
公开(公告)号：WO2017139803A1
公开(公告)日：2017-08-17
申请号：PCT/US2017/017737
申请日：2017-02-13
申请人： CIRRUS DESIGN CORPORATION
发明人： HOMAN, Garrett John , RATHBUN, David A. , WELSH, Kevin P. , ENGEL, Jeremy Travis , KASHER, Anthony Dale
IPC分类号： B64D17/80 , B64D17/72 , B64D17/52
CPC分类号： B64D17/72 , B64C13/18 , B64C39/024 , B64D17/26 , B64D17/62 , B64D17/725 , B64D17/80
摘要： An aircraft includes an airframe parachute system. The parachute system includes an ejector assembly, a switch assembly, a projectile object and a mechanical connector. The ejector assembly includes an inflatable cushion. The switch assembly includes a switch component shiftable from an inactive position to an active position. The switch assembly is configured to initiate inflation of the inflatable cushion when the switch component is shifted from the inactive position to the active position. The projectile object is configured to travel from a stowed position to an activation position. The mechanical connector extends between and interconnects the projectile object and the switch assembly such that travel of the projectile object from the stowed position to the activation position shifts the switch component from the inactive position to the active position.
摘要翻译：
一架飞机包括一个机身降落伞系统。降落伞系统包括喷射器组件，开关组件，抛射物体和机械连接器。喷射器组件包括充气垫。开关组件包括可从不活动位置移动到活动位置的开关组件。开关组件构造成当开关部件从不活动位置移动到活动位置时开始充气垫的充气。射弹对象构造成从收起位置行进到激活位置。机械连接器在射弹对象和开关组件之间延伸并互连，使得射弹对象从收起位置到激活位置的行进将开关组件从不活动位置移动到激活位置。

4. 发明申请

WO2015059703A1 APPARATUS AND METHOD FOR RAPID DEPLOYMENT OF A PARACHUTE 审中-公开
标题翻译：装置和方法快速部署的PARACHUTE
公开(公告)号：WO2015059703A1
公开(公告)日：2015-04-30
申请号：PCT/IL2014/050920
申请日：2014-10-22
申请人： WISEC LTD.
发明人： TSALIAH, Amir , KRAUSS, Ran
IPC分类号： B64D17/72 , A62B1/00
CPC分类号： B64D17/725 , A62B1/22 , B64D17/76
摘要： The present invention relates to a parachute deploying apparatus, comprising: a )a manifold with which is releasably coupled a single vessel within which pressurized gas is generated; b) a gas generator which cooperates with said vessel; c) a plurality of hollow tubes which extend obliquely and upwardly from, and are in communication with, said manifold; and d) a plurality of projectiles, each of which formed with a rod that is receivable in a corresponding tube and to each of which is connected a cord that is also connected to a corresponding portion of an undeployed parachute, wherein the pressurized gas which is generated upon triggering of said gas generator is flowable through each of said tubes to propel said plurality of projectiles in different directions and to cause said parachute to become deployed.
摘要翻译：降落伞展开装置本发明涉及一种降落伞展开装置，包括：a）歧管，其可释放地联接在其中产生加压气体的单个容器内; b）与所述容器配合的气体发生器; c）多个中空管，其从所述歧管倾斜和向上延伸并与所述歧管连通; 以及d）多个弹丸，每个弹片形成有可接收在相应的管中的杆，并且每个都连接有一根绳索，该绳索也连接到未部署的降落伞的相应部分，其中加压气体是在所述气体发生器的触发时产生的气体可流过每个所述管，以沿着不同的方向推进所述多个射弹并使所述降落伞展开。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式