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1. 发明授权

US11639226B2 Device for unlocking a system for closing a container by means of a tie and container provided with such an unlocking device 有权
公开(公告)号：US11639226B2
公开(公告)日：2023-05-02
申请号：US16971843
申请日：2019-02-26
申请人： SAFRAN AEROSYSTEMS
发明人： Gaël Suze
IPC分类号： B64D17/52 , B64D17/46 , B64D17/38 , B64D17/64
摘要： A device for unlocking a system for closing a container by means of a tie, such as a rope or strap, in particular a tie tensioned between closing eyelets, includes a cutting tool (O) capable of cutting the tie in order to unlock the closing system. It also includes an actuation member linked to the cutting tool, the actuation member being capable of being manipulated manually by a user in order to cause the cutting tool (O) to move into a position for severing the tie.

2. 发明授权

US09611044B2 Method and an apparatus to shoot an object from a flying apparatus 有权
公开(公告)号：US09611044B2
公开(公告)日：2017-04-04
申请号：US15111147
申请日：2015-10-12
申请人： Skycat Oy
发明人： Henri Hiisilä
IPC分类号： B64D17/00 , B64D19/00 , B64D17/70 , B64D1/12 , B64D25/00 , B64C39/02 , B64D17/64
CPC分类号： B64D17/70 , B64C39/024 , B64C2201/128 , B64C2201/146 , B64C2201/185 , B64D1/04 , B64D1/12 , B64D7/08 , B64D17/64 , B64D25/00 , F41A19/58 , F41B7/00 , F41F1/00
摘要： The object of this invention is a method to shoot an object from a flying apparatus. Into an flying apparatus, into certain part of it, like a container that consists at least of a bottom and a shell a spring will be placed, like a push spring that has been loaded in a tense state and that is locked in this position using a fixing organ and further there will be put as an extension of the spring an object to be shot out from the flying apparatus. The fixing organ is thread, metal cord, bar, strip, rope, line, or some combination of these and tension strength (T) is greater than the tension load of the push force (F) to the mentioned fixing organ. the tension strength (T) of the fixing organ is weakened to be less than the mentioned tension load by heating, burning, or melting the mentioned fixing organ by electric energy when the fixing organ breaks, the spring expands into the direction of the object and the push force (F) pushes the object out of the container and off the flying apparatus. The apparatus that is used in the present method is also an object of the invention.

3. 发明授权

US5921503A Assistant landing device of a troubled airplane 失效
标题翻译：辅助着陆装置的困扰飞机
公开(公告)号：US5921503A
公开(公告)日：1999-07-13
申请号：US18619
申请日：1998-02-04
申请人： Ing-Lang Tsay
发明人： Ing-Lang Tsay
IPC分类号： B64D17/80 , B64D25/00 , B64D17/64
CPC分类号： B64D17/80 , B64D25/00
摘要： The assistant landing device of a troubled airplane of the present invention comprises a storing chamber under the front end of the airplane, which has a freely opened door, and a strengthen network the front end of which is connected with the airplane body. When the network is expanded from the storing chamber, it will not affect the descent of the front and back landing gears. A plurality of canopy packets arranged as an array are installed on the front and back sides of the network and may be opened by controlling so that a group of canopy packets are formed on the right and left sides of the body of the airplane so that the airplane may be descended slowly. Each of the canopy packets has a large and a small canopy packets and a gas container for being quickly charged with air so that the small canopy packet may be opened. A plurality of positioning parachutes are located on the distal end of the network, which may be opened by the applied force of the wind in order that the strengthen network will be expanded uniformly below the canopy body. The present invention has further provided a network cover the end portion of which has a decoupled parachute being controlled to expand in order that the network cover can be decoupled from the network.
摘要翻译：本发明的困扰飞机的辅助着陆装置包括在飞机前端下方的存放室，其具有自由打开的门，以及加强网，其前端与飞机主体连接。当网络从存储室扩展时，它不会影响前后起落架的下降。作为阵列布置的多个冠层包被安装在网络的前侧和后侧，并且可以通过控制来打开，使得在飞机的身体的右侧和左侧形成一组遮篷包，使得飞机可能会缓慢下降。每个盖子包具有大的和小的冠层包和一个用于快速充满空气的气体容器，以便可以打开小篷布包。多个定位降落伞位于网络的远端，其可以通过施加的风力打开，以便强化网络将均匀地在冠层体下方扩张。本发明进一步提供了一种网络覆盖件，其端部具有被解耦的降落伞被控制以扩展，以便网络覆盖物可以与网络分离。

4. 发明授权

US4948071A Deployment system for parachute 失效
标题翻译：降落伞部署系统
公开(公告)号：US4948071A
公开(公告)日：1990-08-14
申请号：US337087
申请日：1989-04-12
申请人： Clyde M. Summers, III
发明人： Clyde M. Summers, III
IPC分类号： B64D17/64
CPC分类号： B64D17/64
摘要： The deployment system includes a pilot chute and a bridle wherein the bridle is secured at one end to the forward portion of a parachute canopy. The bridle extends through a rear portion of the canopy. Prior to deployment, the deployment bag is packed such that the forward and rear portions of the canopy lie closely adjacent one another to fully extend the bridle pilot chute from the main canopy. Upon deployment, relative front-to-back opening forces of the parachute displace the front and rear portions of the parachute away from one another thereby drawing the bridle within the canopy and the pilot chute into a closely snugged location to the canopy.
摘要翻译：所述展开系统包括导向滑槽和襟翼，其中所述brid绳在一端固定在降落伞顶部的前部。襟翼延伸穿过树冠的后部。在部署之前，部署袋被包装，使得顶盖的前部和后部彼此紧密相邻，从而从主盖完全延伸襟翼导向滑槽。在部署时，降落伞的相对的前后打开力将降落伞的前部和后部部分彼此远离，从而将伞篷内的马蹄和飞行员滑槽拉入到冠层的紧密位置。

5. 发明授权

US4039164A Parachute with main chute release dependant upon pilot chute deployment 失效
标题翻译：降伞具有主滑槽释放，取决于飞行员滑槽部署
公开(公告)号：US4039164A
公开(公告)日：1977-08-02
申请号：US683798
申请日：1976-05-06
申请人： William Ross Booth
发明人： William Ross Booth
IPC分类号： B64D17/64 , B64D17/40
CPC分类号： B64D17/64
摘要： This invention is an improvement in the art of parachutes. A parachute has a pilot chute and a main chute and provides that the main chute is locked in place and is not released until the pilot chute is properly deployed. This improvement may also provide for the actuating of the release of the main chute by the deployment of the pilot chute. This improvement in turns allows other improvements such as providing the individual parachutes with alternative mountings of the pilot chute for left and right handed people.
摘要翻译：本发明是降落伞技术的改进。降落伞具有飞行员滑槽和主滑槽，并且允许主滑道锁定在适当位置，并且在飞行员滑槽正确部署之前不释放。这种改进还可以通过部署导向槽来提供主滑槽的释放的致动。这种改进可以进行其他改进，例如为左转和右转人员提供飞行员滑槽的替代安装的单个降落伞。

6. 发明授权

US11260981B2 Automatic safety parachute deployment system for multi rotor drones 有权
公开(公告)号：US11260981B2
公开(公告)日：2022-03-01
申请号：US16272631
申请日：2019-02-11
申请人： Helmuth G. Bachmann
发明人： Helmuth G. Bachmann
IPC分类号： B64D17/80 , B64C39/02 , B64D17/64
摘要： This invention relates to the use of an automatic safety parachute deployment system for drones (UAVs), which utilizes an airflow trigger that deploys one or more parachutes under certain aerodynamic conditions from the upward airflow during a flight malfunction. The system is mechanically activated without the use of electronics, batteries or an ejection spring which reduces the complexity and weight.

7. 发明申请

US20160311530A1 Aircraft With A Plurality Of Engines Driving A Common Driveshaft 审中-公开
标题翻译：具有多个发动机的飞机驱动常见的驱动轴
公开(公告)号：US20160311530A1
公开(公告)日：2016-10-27
申请号：US15204547
申请日：2016-07-07
申请人： Frick A. Smith
发明人： Frick A. Smith
IPC分类号： B64C29/00 , B64C27/28 , B64D31/00 , B64C39/02 , B64C27/82 , B64D17/64 , B64D17/80 , B64D27/02 , B64C1/14 , B64C27/52 , B64C27/26 , B64D17/24
CPC分类号： B64C29/0033 , B64C1/1415 , B64C1/1476 , B64C27/22 , B64C27/26 , B64C27/28 , B64C27/52 , B64C27/82 , B64C29/00 , B64C29/0016 , B64C39/02 , B64C39/024 , B64C2201/04 , B64C2201/088 , B64C2201/10 , B64C2201/104 , B64C2201/108 , B64C2201/162 , B64D17/24 , B64D17/34 , B64D17/62 , B64D17/64 , B64D17/80 , B64D27/02 , B64D31/00 , B64D35/04
摘要： An aircraft may have a fuselage, a left wing extending from the fuselage, a right wing extending from the fuselage, a tail section extending from a rear portion of the fuselage, and a first engine and a second engine operably connected by a common driveshaft, wherein the first and second engines are configured for freewheeling such that if one of the first and second engines loses power the other of the first and second engines continues to power the aircraft.
摘要翻译：飞机可以具有机身，从机身延伸的左翼，从机身延伸的右翼，从机身的后部延伸的尾部，以及通过共同的驱动轴可操作地连接的第一发动机和第二发动机，其中所述第一和第二发动机被配置为自由转动，使得如果所述第一和第二发动机中的一个发动机失去动力，则所述第一和第二发动机中的另一个继续为所述飞行器供电。

8. 发明申请

US20150284065A1 Near-space operation systems 有权
标题翻译：近空操作系统
公开(公告)号：US20150284065A1
公开(公告)日：2015-10-08
申请号：US14188581
申请日：2014-02-24
申请人： WORLD VIEW ENTERPRISES, INC.
发明人： Taber K. MacCallum , Jacob H. Dang , Robert Alan Eustace , John Zaniel Maccagnano , Julian R. Nott , Sebastian A. Padilla , Sreenivasan Shankarnarayan , John Straus
IPC分类号： B64B1/02 , B64D17/64 , B64D17/62 , B64D17/00 , B64D17/22
CPC分类号： B64D17/64 , B64B1/02 , B64B1/40 , B64D10/00 , B64D17/00 , B64D17/22 , B64D17/62 , B64D2010/005 , B64D2010/007
摘要： A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
摘要翻译：一个能够在极高海拔地区（高于70,000英尺）进行安全人员和无人操作的系统。该系统利用气球发射系统和降落伞和/或parafoil恢复。

9. 发明授权

US09010691B1 Parachute deployment system 有权
标题翻译：降落伞部署系统
公开(公告)号：US09010691B1
公开(公告)日：2015-04-21
申请号：US14071713
申请日：2013-11-05
申请人： Google Inc.
发明人： Daniel Ratner , Phillip Clarin
IPC分类号： B64D17/52 , B64D17/64 , B64B1/40 , B64D17/70 , B64D17/72
CPC分类号： B64D17/64 , B64B1/40 , B64D1/12 , B64D17/70
摘要： The present disclosure provides a parachute deployment system. The system may include a deployment spring arranged on a launch platform with a parachute that is foldable and positionable on an opposite side of the deployment spring from the launch platform. The system may also include a bridle line attached to the parachute, and a lanyard line having a first end and a second end. The first end of the lanyard line may be attached to the deployment spring, and the second end of the lanyard line may be attached to the launch platform. The system may also include a trigger system configured to initiate deployment of the parachute. Upon deployment, the deployment spring may be configured to launch the parachute and the bridle line substantially perpendicular to the launch platform. After deployment, the deployment spring and the lanyard line may be configured to hang from the launch platform.
摘要翻译：本公开提供了一种降落伞部署系统。该系统可以包括布置在发射平台上的展开弹簧，其具有可降落伞，该降落伞可在展开弹簧的与发射平台相对的一侧上可折叠和定位。该系统还可以包括连接到降落伞上的连线，以及具有第一端和第二端的挂绳。绳索的第一端可以附接到展开弹簧，并且挂绳的第二端可以附接到发射平台。该系统还可以包括被配置为启动降落伞部署的触发系统。在部署时，部署弹簧可以被配置成发射基本上垂直于发射平台的降落伞和蹬绳。部署后，部署弹簧和挂绳可能被配置为从发射平台挂起。

10. 发明申请

US20120025028A1 PARACHUTE SAFETY DEVICE 有权
标题翻译： PARACHUTE安全装置
公开(公告)号：US20120025028A1
公开(公告)日：2012-02-02
申请号：US13173291
申请日：2011-06-30
申请人： M. Gael Suze
发明人： M. Gael Suze
IPC分类号： B64D17/52 , B64D17/64
CPC分类号： B64D17/38 , B64D17/60 , B64D17/64 , B64D17/74
摘要： The safety device comprises a first bridle connecting a pilot chute of the reserve parachute to a deployment bag, a second bridle connecting the main parachute to the first bridle, a pin fastened to this first bridle and passed in a releasable manner in a loop formed on a locking bridle fastened to the locking pin and passed through a loop fastened to the second bridle and two eyelets formed through the first bridle.
摘要翻译：安全装置包括将预备降落伞的先导滑槽连接到展开袋的第一桥梁，将主降落伞连接到第一桥架的第二桥梁，固定到该第一桥架上的销，并以可释放的方式通过在环形成的环中紧固在锁定销上并通过固定在第二匝上的环的锁定掣子和通过第一襟翼形成的两个孔眼。

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