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1. 发明授权

CN105307934B 空投系统失效
公开(公告)号：CN105307934B
公开(公告)日：2018-07-13
申请号：CN201480030502.7
申请日：2014-05-29
申请人：库克基金会
发明人：乔治·库克 , 乔纳森·库克 , 迈克尔·库克
IPC分类号： B64D1/14 , B64D1/10
CPC分类号： B64D1/14 , B64D1/10 , B64D1/12 , B64D17/02 , B64D17/26
摘要：用于从飞机释放的空投箱(30)包括用于装载物的保持部(31)和用于保护保持部的装载物的撞击吸收区(32)。保持部和撞击吸收区由生物可降解材料形成。撞击吸收区(32)包括具有蜂窝结构的至少一个层，该蜂窝结构界定沿层的平面延伸的小室网络。还公开了空投组件，包括空投箱(30)、降落伞(20)和将降落伞(20)连接到空投箱(30)的多个伞索(21)。还公开了通过空投来投递货物的方法，包括将空投组件从飞机释放。空投组件可从飞机的货舱释放，特别地，货舱包括附接到飞机的第一壳体和在第一壳体后面附接到第一壳体的第二壳体。第一壳体和第二壳体界定用于接收组件的开口。第二壳体适于从第一壳体释放以暴露降落伞并由此允许降落伞充气并从第一壳体提取空投箱。

2. 发明公开

CN105307934A 空投系统失效
公开(公告)号：CN105307934A
公开(公告)日：2016-02-03
申请号：CN201480030502.7
申请日：2014-05-29
申请人：库克基金会
发明人：乔治·库克 , 乔纳森·库克 , 迈克尔·库克
IPC分类号： B64D1/14 , B64D1/10
CPC分类号： B64D1/14 , B64D1/10 , B64D1/12 , B64D17/02 , B64D17/26
摘要：用于从飞机释放的空投箱(30)包括用于装载物的保持部(31)和用于保护保持部的装载物的撞击吸收区(32)。保持部和撞击吸收区由生物可降解材料形成。撞击吸收区(32)包括具有蜂窝结构的至少一个层，该蜂窝结构界定沿层的平面延伸的小室网络。还公开了空投组件，包括空投箱(30)、降落伞(20)和将降落伞(20)连接到空投箱(30)的多个伞索(21)。还公开了通过空投来投递货物的方法，包括将空投组件从飞机释放。空投组件可从飞机的货舱释放，特别地，货舱包括附接到飞机的第一壳体和在第一壳体后面附接到第一壳体的第二壳体。第一壳体和第二壳体界定用于接收组件的开口。第二壳体适于从第一壳体释放以暴露降落伞并由此允许降落伞充气并从第一壳体提取空投箱。

3. 发明授权

US09145211B1 Method of improved load distribution over the surface of a parachute canopy 有权
标题翻译：改善降落伞冠层表面负荷分布的方法
公开(公告)号：US09145211B1
公开(公告)日：2015-09-29
申请号：US14623862
申请日：2015-02-17
申请人： The United States of America as Represented by the Secretary of the Army
发明人： James E. Sadeck
IPC分类号： B64D17/02 , B64D17/24 , B64D17/14
CPC分类号： B64D17/24 , B64D17/02 , B64D17/14 , B64D17/22 , B64D17/26 , B64D17/28
摘要： A parachute canopy system includes a canopy having a skirt and a suspension line system, where each suspension line of the suspension line system is attached to the skirt. A pair of first line members is attached to the canopy, the pair of first line members extending in a substantially radial direction away from the skirt towards a center of the canopy. A first end of each line member in the pair of first line members is connected together to the suspension line at the skirt. A first end of the second line member is connected to adjacent second ends of adjacent pairs of first line members that extend towards the center of the canopy.
摘要翻译：降落伞冠层系统包括具有裙部和悬挂线系统的罩，其中悬挂系统系统的每个悬挂线连接到裙部。一对第一线构件附接到顶盖，一对第一线构件沿着远离裙部的大致径向方向朝向顶盖的中心延伸。一对第一线构件中的每个线构件的第一端部连接在裙部的悬挂线上。第二线构件的第一端连接到相对于顶盖的中心延伸的相邻的第一线构件对的相邻的第二端。

4. 发明公开

EP3003857A1 AERIAL DELIVERY SYSTEM 审中-公开
标题翻译： AIR货运系统
公开(公告)号：EP3003857A1
公开(公告)日：2016-04-13
申请号：EP14728253.7
申请日：2014-05-29
申请人： The Cook Foundation
发明人： COOK, George , COOK, Jonathan , COOK, Michael
IPC分类号： B64D1/14 , B64D1/10
CPC分类号： B64D1/14 , B64D1/10 , B64D1/12 , B64D17/02 , B64D17/26
摘要： An aerial delivery box (30) for release from an aircraft comprises a hold (31) for a payload; and an impact absorbing zone (32) for protecting the payload of the hold. The hold and the impact absorbing zone are formed of biodegradable materials. The impact absorbing zone (32) comprises at least one layer having a honeycomb structure, the honeycomb structure defining a cellular network extending in the plane of the layer. Also disclosed is an aerial delivery assembly comprising: the aerial delivery box (30); a parachute (20); and a plurality of shroud lines (21) connecting the parachute (20) to the aerial delivery box (30). Also disclosed is a method of delivering goods by aerial delivery, comprising releasing the aerial delivery assembly from an aircraft. The aerial delivery assembly may be released from a cargo pod of an aircraft, in particular a cargo pod comprising: a first casing attached to the aircraft; and a second casing attached to the first casing rearwardly of the first casing. The first and second casings define an opening to receive the assembly. The second casing is adapted to be releasable from the first casing so as to expose the parachute and thereby allow the parachute to inflate and extract the aerial delivery box from the first casing.

5. 发明公开

EP3268279A1 RIGIDIZED ASSISTED OPENING SYSTEM FOR HIGH ALTITUDE PARAFOILS 审中-公开
标题翻译：用于高海拔翼伞的刚性辅助开启系统
公开(公告)号：EP3268279A1
公开(公告)日：2018-01-17
申请号：EP16762468.3
申请日：2016-03-09
申请人： World View Enterprises Inc.
发明人： LEIDICH, Jared , MACCALLUM, Taber, Kyle , BOWEN, Ty
IPC分类号： B64D17/02 , B64D17/22 , B64D17/40 , B64D17/62
CPC分类号： B64D17/76 , B64B1/40 , B64D1/12 , B64D17/025 , B64D17/24 , B64D17/26 , B64D17/40 , B64D17/62 , B64D17/70 , B64D17/72
摘要： A parafoil for operation at high altitudes, in low density air, or at low airspeeds, and methods for opening same. Some versions of the parafoil comprise flexible members connected to the parafoil canopy. When the parafoil canopy is in a stowed configuration, the members are deformed, storing elastic energy. When the canopy is released from its stowed configuration, the members spring back to their undeformed shapes, thereby opening or assisting with opening the canopy. The flexible member may also be attached to a base structure, which is attached to the payload. The members may comprise rods or hollow tubes that can be flexed using a fulcrum near the base structure, or a spacer plate, so that the ends connected to the canopy are restrained by a parachute bag containing the stowed or packed canopy. The parachute bag can be opened prior to or during detachment of the parafoil from the flight vehicle.

6. 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。

7. 发明申请

WO2009129642A1 RESCUE DEVICE 审中-公开
标题翻译：救援设备
公开(公告)号：WO2009129642A1
公开(公告)日：2009-10-29
申请号：PCT/CH2009/000133
申请日：2009-04-23
申请人： LIECHTI, Heinz , RYSER, Werner
发明人： LIECHTI, Heinz , RYSER, Werner
IPC分类号： A62B1/22 , B64D17/26
CPC分类号： A62B1/22 , B64D17/06 , B64D17/26 , B64D17/34 , B64D17/70
摘要： A parachute rescue device (3) has parachutes (13) whose lines are formed by parachute rods (37) or arrangements of rods and cords (92). These spring-elastic rods (37) serve for deploying the parachutes (13) at standstill already. The canopy (25) may also be deployed by such rods (29). The rescue device (3) may furthermore comprise two such parachutes that are attached to a carrier system (7, 11) and inclined away from each other. The parachutes (13) are attached to the carrier system (1, 11) rotatably about their longitudinal axes and their canopies (25) are e.g. composed of segments (53) one edge (56) of each of which is only loosely connected to the rod structure (29). The air escaping through the thus created openings (57) may apply an autorotating motion to the parachutes (13) while tilting the parachutes allows steering the fall.
摘要翻译：降落伞救援装置（3）具有降落伞（13），其线由降落伞杆（37）或杆和绳索（92）的布置形成。这些弹簧弹簧杆（37）用于将降落伞（13）部署在停止状态。顶篷（25）也可以由这种杆（29）展开。救援装置（3）还可以包括两个这样的降落伞，其连接到承载系统（7,11）并且彼此远离。降落伞（13）围绕其纵向轴线可旋转地附接到载体系统（1,11），并且它们的檐篷（25）是例如。由段（53）组成，每个边缘（56）仅松散地连接到杆结构（29）。通过这样产生的开口（57）逸出的空气可以对降落伞（13）施加自动运动，同时倾斜降落伞允许转向下降。

8. 发明公开

US20230166850A1 PARACHUTE WITH CANOPY SLITS OR OPENINGS FOR PREVENTING CANOPY INVERSION 审中-公开
公开(公告)号：US20230166850A1
公开(公告)日：2023-06-01
申请号：US17992342
申请日：2022-11-22
申请人： AIRBORNE SYSTEMS NA INC.
发明人： William Louis Bruce GARGANO
IPC分类号： B64D17/14 , B64D17/26
CPC分类号： B64D17/14 , B64D17/26
摘要： Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.

9. 发明申请

US20160297537A1 RIGIDIZED ASSISTED OPENING SYSTEM FOR HIGH ALTITUDE PARAFOILS 有权
标题翻译：用于高海拔参数的刚性辅助开启系统
公开(公告)号：US20160297537A1
公开(公告)日：2016-10-13
申请号：US15189850
申请日：2016-06-22
申请人： World View Enterprises Inc.
发明人： Taber Kyle MacCallum , Jared Leidich
IPC分类号： B64D17/76 , B64D17/02 , B64D17/40 , B64D1/12 , B64D17/26 , B64B1/40
CPC分类号： B64D17/76 , B64B1/40 , B64D1/12 , B64D17/025 , B64D17/24 , B64D17/26 , B64D17/40 , B64D17/62 , B64D17/70 , B64D17/72
摘要： A parafoil for operation at high altitudes, in low density air, or at low airspeeds, and methods for opening same. Some versions of the parafoil comprise flexible members connected to the parafoil canopy. When the parafoil canopy is in a stowed configuration, the members are deformed, storing elastic energy. When the canopy is released from its stowed configuration, the members spring back to their undeformed shapes, thereby opening or assisting with opening the canopy. The flexible member may also be attached to a base structure, which is attached to the payload. The members may comprise rods or hollow tubes that can be flexed using a fulcrum near the base structure, or a spacer plate, so that the ends connected to the canopy are restrained by a parachute bag containing the stowed or packed canopy. The parachute bag can be opened prior to or during detachment of the parafoil from the flight vehicle
摘要翻译：在高海拔，低密度空气或低空速下运行的石棺，以及打开相同的方法。一些版本的parafoil包括连接到parafoil冠层的柔性构件。当石棺顶盖处于收起状态时，构件变形，储存弹性能量。当树冠从收起的构造中释放时，构件弹回到未变形的形状，从而打开或辅助打开盖子。柔性构件还可以附接到附接到有效载荷的基部结构。构件可以包括杆或中空管，其可以使用基部结构附近的支点或间隔板弯曲，使得连接到顶盖的端部被包含收起或堆积的顶盖的降落伞包限制。降落伞袋可以在从飞行器车辆卸下石蜡片之前或之中打开

10. 发明授权

US08220751B1 Multi-grommet retained slider for parachutes 有权
标题翻译：多索环保留滑块用于降落伞
公开(公告)号：US08220751B1
公开(公告)日：2012-07-17
申请号：US13344138
申请日：2012-01-05
申请人： Jean C. Berland
发明人： Jean C. Berland
IPC分类号： B64D17/00
CPC分类号： B64D17/025 , B64D17/26 , B64D17/343
摘要： A reefing slider for providing improved line management and canopy deployment characteristics of a ram air inflated airfoil type canopy. During initial descent of the parachute the slider, secured by retaining elements, is held against the canopy in the upper reefing position where it mechanically restricts canopy deployment while giving the canopy time to achieve proper orientation following the drop from the launching aircraft. Upon sufficient air flow into the canopy cells, the retaining elements separate, releasing the slider and enabling full opening of the canopy.
摘要翻译：一种用于提供改进的管线管理和一个冲压空气充气翼型式的冠层部署特征的折叠滑块。在降落伞的初始下降期间，通过保持元件固定的滑块在上部折叠位置处被保持抵靠顶盖，其中机械地限制雨篷部署，同时在发射飞机下降之后提供冠层时间以实现适当的定向。当足够的气流进入顶盖单元时，保持元件分离，释放滑块并使盖子完全打开。

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