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1. 发明授权

US11225329B2 Dampening risers for parachutes 有权
公开(公告)号：US11225329B2
公开(公告)日：2022-01-18
申请号：US16279579
申请日：2019-02-19
申请人： GOODRICH CORPORATION
发明人： Jaro S. Volny , Timothy C. Haynes
IPC分类号： B64D17/22
摘要： A suspension line assembly for a parachute may comprise a plurality of suspension lines bound together at a confluence, and a dampening riser coupled to the confluence, wherein the dampening riser comprises a first length in the stowed position and the dampening riser is configured to extend to a second length in a deployed position in response to a tensile force applied to the dampening riser.

2. 发明授权

US10532818B2 Water landing parachute trap and method 有权
公开(公告)号：US10532818B2
公开(公告)日：2020-01-14
申请号：US15220335
申请日：2016-07-26
申请人： The Boeing Company
发明人： Jamie Childress
IPC分类号： B64D17/22 , B64D1/14 , B64D17/38 , B64D25/20 , B63B22/00 , B64D1/02
摘要： Systems and methods for aerially delivering cargo into a body of water while avoiding parachute entrapment and entanglement are described. The system includes a parachute having a canopy and suspension lines. The system further includes a weight coupled to a first end of the suspension lines and a ring that is configured to float in the body of water. The weight is coupled to the cargo, and the ring is disposed between the weight and the canopy with the suspension lines passing through the center of the ring.

3. 发明申请

US20170158330A1 IMU POD AND METHOD OF RETRIEVAL OF THE SAME 审中-公开
公开(公告)号：US20170158330A1
公开(公告)日：2017-06-08
申请号：US14957172
申请日：2015-12-02
申请人： THE BOEING COMPANY
发明人： Joseph E. Justin
IPC分类号： B64D1/02 , B64D17/22 , G01C21/16
CPC分类号： B64D1/02 , F42B10/48 , F42B10/56 , G01C25/005
摘要： A pod assembly which includes a pod and an inertial measurement unit positioned within the pod. The pod assembly further includes deceleration hardware associated with the pod. A method for using a pod assembly, includes a step of securing the pod assembly, which includes a pod and an inertial measurement unit contained within the pod, to an aircraft and a step of operating the aircraft with the inertial measurement unit operating sensing movement and alignment of the pod and storing data corresponding to the sensed movement and alignment of the pod on a data collection assembly connected to the inertial measurement unit. The method further includes a step of releasing the pod assembly from the aircraft and a step of utilizing deceleration hardware associated with the pod to reduce rate of descent of the pod assembly released from the aircraft.

4. 发明授权

US09630727B1 System, method, and apparatus for marking a drop zone area 有权
公开(公告)号：US09630727B1
公开(公告)日：2017-04-25
申请号：US14934183
申请日：2015-11-06
申请人： ARCACHON HOLDINGS LLC
发明人： Gary Leegate , Marcia Baldwin
IPC分类号： B64F1/20 , F21V23/00 , F21V23/04 , F21L4/00 , B64D17/76 , B64D17/22 , G08B5/38 , B64D47/02 , B64D17/00 , F21W111/06
CPC分类号： B64F1/20 , B64D17/00 , B64D17/22 , B64D17/40 , B64D17/76 , B64D47/02 , F21L4/00 , F21V23/003 , F21V23/0407 , F21V23/0414 , F21W2111/06 , F21Y2101/00 , G08B5/38
摘要： A drop zone marker includes a parachute, a first light module connected to the parachute by a first length of cord and a second light module connected to the first light module by a second length of the cord. A ballast is connected to the second light module by a third length of the cord is provided for pulling downwardly the drop zone marker. The parachute is configured to include an integral packing/deployment bag within which all components of the drop zone marker are contained up until deployment.

5. 发明授权

US09573692B1 In canopy bleed air actuator with mesh vent 有权
标题翻译：在具有网孔的顶盖排气致动器中
公开(公告)号：US09573692B1
公开(公告)日：2017-02-21
申请号：US14709606
申请日：2015-05-12
申请人： Earthly Dynamics, LLC
发明人： Mark F Costello , Michael Brian Ward , Edward James Scheuermann , Keith Bergeron , Michael Wayne Shurtliff , Gregory Michael Noetscher
IPC分类号： B64D17/34 , B64D17/22 , B64D17/18 , B64D17/02
CPC分类号： B64D17/34 , B64D17/025 , B64D17/18 , B64D17/20 , B64D17/22
摘要： A system is described to control the flight path of a parafoil. The physical control mechanism is a series of actuators embedded within the parafoil canopy that open a series of meshed venting systems in the upper surface of the parafoil canopy. Opening and closing the meshed venting system changes the forces and moments acting on the parafoil canopy in a consistent manner such that it can be used for flight control. The meshed venting system includes an internal sealing flap and a mesh member.
摘要翻译：描述一个系统来控制parafoil的飞行路径。物理控制机制是一系列执行器嵌入在parafoil冠层，打开一系列网孔通风系统在上面的parafoil冠层。打开和关闭网状排气系统以一致的方式改变作用在石蜡冠上的力和力矩，使其可用于飞行控制。网状排气系统包括内部密封盖和网状构件。

6. 发明申请

US20160075437A1 AERIAL DELIVERY PLATFORMS 审中-公开
标题翻译：航空运输平台
公开(公告)号：US20160075437A1
公开(公告)日：2016-03-17
申请号：US14850159
申请日：2015-09-10
申请人： Airborne Systems Limited
发明人： Martyn Philip JONES
IPC分类号： B64D17/22 , B64D9/00
CPC分类号： B64D17/22 , B64D1/14 , B64D9/00
摘要： An aerial delivery platform comprises first and second modules (10a, 10b) each having a respective load-bearing surface (14). The modules (10a, 10b) are hinged together for relative flexing movement about an axis (24) between the modules (10a, 10b). A superstructure of interconnected struts (25, 26, 27, 28, 29) is connected to, and is upstanding from, the modules (10a, 10b) to hold the modules (10a, 10b) with the load bearing surfaces (14) co-planar when loaded and during descent but being elastically deformable to permit limited relative flexing movement between the modules (10a, 10b) under the loads applied by parachute opening and on landing to assist in the absorption the energy transferred to the platform.
摘要翻译：空中交付平台包括第一和第二模块（10a，10b），每个模块具有相应的承载表面（14）。模块（10a，10b）铰接在一起，用于围绕模块（10a，10b）之间的轴线（24）的相对弯曲运动。互连支柱（25,26,27,28,29）的上部结构连接到模块（10a，10b）并且从模块（10a，10b）直立，以将模块（10a，10b）与承载表面（14）共同在加载和下降期间但是可弹性变形以允许在由降落伞开口施加的负载和着陆下的模块（10a，10b）之间的有限的相对弯曲运动的平面以帮助吸收传递到平台的能量。

7. 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。

8. 发明授权

US08894015B2 Apparatus and method for paragliders 有权
标题翻译：滑翔伞的装置和方法
公开(公告)号：US08894015B2
公开(公告)日：2014-11-25
申请号：US13719108
申请日：2012-12-18
申请人： Dreamscience Propulsion Limited
发明人： Adam Edward Alexander Contoret
IPC分类号： B64D17/22 , B64D17/30 , B64D17/36 , B64C39/02 , B64C31/028 , B64C31/036
CPC分类号： B64C39/026 , B64C31/028 , B64C31/036 , B64D17/30 , Y02T50/62
摘要： Apparatus and method for propelling a user wearing paragliding equipment are disclosed The apparatus includes at least one thruster for providing thrust in a predetermined direction; and an attachment element for attaching the at least one thruster to a user's body such that the thruster is secured against the front portion of the user's body.
摘要翻译：公开了用于推进使用者滑翔设备的装置和方法。该装置包括至少一个用于在预定方向上提供推力的推进器; 以及附接元件，用于将至少一个推进器附接到使用者的身体，使得推进器固定抵靠使用者身体的前部。

9. 发明授权

US4424945A Parafoil 失效
公开(公告)号：US4424945A
公开(公告)日：1984-01-10
申请号：US377239
申请日：1982-05-12
申请人： Simon C. Dell
发明人： Simon C. Dell
IPC分类号： B64C31/036 , F02B1/04 , B64C3/30 , B64C31/02 , B64D17/22
CPC分类号： B64C31/036 , F02B1/04 , Y10S244/902
摘要： A parafoil for supporting a flying machine, which parafoil has a forwardly extending central section open at the front to scoop in air during flight, and wings attached to the rear of the central section and which receive air into the interior thereof either directly or from the central section, said wings being divided into compartments of equalized pressure, and restraining elements attached to the parafoil central section in front of the parafoil wings and to the outer ends of the parafoil wings, thereby in flight to hold down the front of the parafoil central section and hold down the parafoil wings in an inverted U-shape.
摘要翻译：用于支撑飞行器的翼型飞机，其翼型具有向前延伸的中心部分，其在前部开放，在飞行期间在空气中舀出，以及附接到中央部分后部并且将空气直接或从中央部分，所述翼分为均压的隔室，以及限制元件，其附着在翼蓬翼前面的parafoil中心部分和parafoil翼的外端，从而在飞行中压住parafoil中心的前部并将倒钩的翅膀按倒置的U形按住。

10. 发明授权

US3692262A Parachute harness and single point release 失效
标题翻译： PARACHUTE HARNESS和单点释放
公开(公告)号：US3692262A
公开(公告)日：1972-09-19
申请号：US3692262D
申请日：1970-12-11
申请人： KOCH & SONS INC H
发明人： GAYLORD JOHN A
IPC分类号： B64D17/22 , B64D17/32
CPC分类号： B64D17/30 , Y10S24/36 , Y10T24/4501
摘要： A parachute harness in which all the straps and belts are connected to a single release, and the leg straps are so connected to the lap belts as to provide a single releasable connection for each leg strap and lap belt releasably connected to one another; the single release is detachably connected to one of the straps.

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