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1. 发明授权

US11840333B2 Package delivery mechanism 有权
公开(公告)号：US11840333B2
公开(公告)日：2023-12-12
申请号：US16687427
申请日：2019-11-18
申请人： Flirtey Holdings, Inc.
发明人： Matthew Sweeny , Jess Hayden , Joseph Rinaldi
IPC分类号： B64C39/02 , B64D1/10 , B64D1/12 , B26D5/00 , B64D1/02 , B64D17/38 , B26F3/12 , F16B21/02 , B64U10/13 , B64U101/60
CPC分类号： B64C39/024 , B26D5/00 , B64D1/02 , B64D1/10 , B64D1/12 , B26F3/12 , B64D17/38 , B64U10/13 , B64U2101/60 , B64U2201/10 , F16B21/02
摘要： Disclosed is a package delivery mechanism for use by an unmanned aerial vehicle (UAV). The package delivery mechanism includes a gravity activated locking mechanism to lock and unlock a package attached to the UAV based on the weight of the package. When the package is attached to suspension means of the UAV that lowers the package to the ground from the UAV, the locking mechanism automatically engages with the package and keeps the package locked to the suspension means, due to the weight of the package. When the package is lowered and reaches on the ground, the weight of the package is offloaded from the suspension means, which enables the locking mechanism to be disengaged, thereby releasing the package. The package delivery mechanism includes a severing module to sever the suspension means from the UAV.

2. 发明授权

US09718546B2 System and method for deploying loads out of an aircraft 有权
公开(公告)号：US09718546B2
公开(公告)日：2017-08-01
申请号：US13891290
申请日：2013-05-10
申请人： Airbus Operations GmbH , Airbus SAS
发明人： Carsten Bohlen , Holger Bohlen
IPC分类号： B64D1/12 , B64D1/10 , B64D17/38 , B64D17/62 , B64D17/68 , B64D17/74 , B64D45/00
CPC分类号： B64D1/12 , B64D1/10 , B64D17/38 , B64D17/62 , B64D17/68 , B64D17/74 , B64D2045/0085
摘要： A system for deploying loads out of an aircraft comprises an aerial delivery parachute with an aerial-delivery parachute line and an activation means for placing the aerial delivery parachute in an enveloping flow past the aircraft. Within the aircraft a receiving device can be positioned that receives a tractive force acting on the aerial-delivery parachute line, which tractive force has been determined by a force measuring device and has been transmitted by way of a transmitting device. With the knowledge of the tractive force it is possible both to implement emergency release and to assess whether an aerial delivery parachute has correctly deployed in the flow enveloping the aircraft.

3. 发明申请

US20160340036A1 SYSTEM AND METHOD FOR DETACHING AN EXTRACTION UNIT FROM AN EXTRACTABLE UNIT 审中-公开
标题翻译：从提取单元中分离提取单元的系统和方法
公开(公告)号：US20160340036A1
公开(公告)日：2016-11-24
申请号：US15159016
申请日：2016-05-19
申请人： Airbus Operations GmbH
发明人： Roland Gad
IPC分类号： B64D1/12 , B64D17/62
CPC分类号： B64D1/12 , B64D17/38 , B64D17/62
摘要： A system and method for detaching an extractable unit from an extraction unit pulling the extractable unit in an extraction direction out of a cargo bay of an aerospace vehicle for aerial delivery. The system includes a detachment unit which is connectable to an extractable unit and which is operable for controllably detaching an extraction unit from the extractable unit, a guiding system and a release unit. The release unit is movably attached to the guiding system and physically connected to the detachment unit such that the release unit is movable with an extractable unit to which the detachment unit has been connected in the extraction direction along the guiding system. The release unit is controllable to operate the detachment unit to which the release unit is connected for detaching an extraction unit from the extractable unit.
摘要翻译：一种用于从提取单元中分离可提取单元的系统和方法，所述提取单元将提取单元沿提取方向拉出航天飞行器的货舱以进行空中传送。该系统包括可拆卸单元，其可连接到可抽出单元，并且其可操作用于可控地从提取单元分离提取单元，引导系统和释放单元。释放单元可移动地附接到引导系统并且物理地连接到分离单元，使得释放单元可以沿着引导系统沿着提取方向连接有拆卸单元的可抽出单元移动。释放单元是可控制的，以操作连接有释放单元的分离单元，用于将提取单元与可抽出单元分离。

4. 发明申请

US20130112813A1 MULTIPLE BUNDLE SLING LOAD SYSTEM 有权
标题翻译：多功能吊装系统
公开(公告)号：US20130112813A1
公开(公告)日：2013-05-09
申请号：US13288411
申请日：2011-11-03
申请人： Marc Tardiff , George N. Moorachian, JR. , Todd Grenga , William S. Ricci , Richard John Benney
发明人： Marc Tardiff , George N. Moorachian, JR. , Todd Grenga , William S. Ricci , Richard John Benney
IPC分类号： B64D1/12 , B64D17/38
CPC分类号： B64D1/12 , B64D17/38
摘要： A multiple bundle sling load system including a sling for attachment to an aircraft, a support system suspended from the sling for carrying a plurality of bundles, a load release mechanism interconnecting each bundle with the support structure, a parachute associated with at least one of the bundles, a parachute release mechanism interconnecting each parachute with the support structure. And an actuator for remotely operating each release mechanism for selectively releasing each load release mechanism and not releasing the associated parachute release mechanism for an air drop operation and selectively releasing each load release mechanism and each associated parachute release mechanism for a land drop operation.
摘要翻译：一种多捆吊带装载系统，包括用于附接到飞行器的吊索，悬挂在吊索上的用于承载多个束的支撑系统，将每个束与支撑结构相互连接的卸载机构，与至少一个束，降落伞释放机构将每个降落伞与支撑结构互连。以及用于远程操作每个释放机构的致动器，用于选择性地释放每个卸载机构，而不释放用于空气降落操作的相关联的降落伞释放机构，并且选择性地释放每个负载释放机构和每个相关联的降落伞释放机构以进行落地操作。

5. 发明授权

US08324903B2 Fluid conductivity sensor for actuating and testing an electroexploding device 有权
标题翻译：用于启动和测试电气爆炸装置的流体电导率传感器
公开(公告)号：US08324903B2
公开(公告)日：2012-12-04
申请号：US12646137
申请日：2009-12-23
申请人： Andre Cournand
发明人： Andre Cournand
IPC分类号： G01N27/02 , G01R27/22
CPC分类号： F42C11/005 , B64D17/38 , G01N27/10
摘要： Disclosed is an apparatus for sensing the electrical conductivity of fluid wherein when electrodes of the apparatus are exposed to fluid. When the electrodes are exposed to a fluid with a predetermined salinity, a voltage is developed on a capacitor which in turn fires a load, such as a resistive bridge wire. Also disclosed is a testing circuit, whereby the integrity of the circuit can be ascertained without the necessity of actually firing the circuit.
摘要翻译：公开了一种用于感测流体的电导率的装置，其中当设备的电极暴露于流体时。当电极暴露于具有预定盐度的流体时，在电容器上产生电压，该电容器又引起负载，例如电阻桥式电线。还公开了一种测试电路，由此可以确定电路的完整性，而不需要实际烧制电路。

6. 发明申请

US20120291234A1 RELEASABLE PACK FOR PARACHUTING WHEN CARRYING EQUIPMENT 有权
标题翻译：用于装载设备时的可释放的包装
公开(公告)号：US20120291234A1
公开(公告)日：2012-11-22
申请号：US13476907
申请日：2012-05-21
申请人： Michael Scott Berge
发明人： Michael Scott Berge
IPC分类号： A44B11/26
CPC分类号： B64D17/46 , B64D17/38 , B64D17/52 , Y10T24/3423
摘要： A separating mechanism for releasing an equipment bag. The mechanism includes a base assembly, a removable soft loop assembly, an attachment ring, and a retention member. The base assembly includes a base member, an aperture, and one or more base assembly rings. The soft loop assembly includes a soft loop base and a soft loop. The soft loop is inserted through the aperture and a first of the base assembly rings. The soft loop base is configured to not be pulled through the aperture. A last of the base assembly rings is inserted through the attachment ring. The retention member is inserted through the soft loop to restrain the first base assembly ring. The base assembly rings are sequentially engaged to couple the attachment ring with the base member. The retention member is pulled out of the soft loop to release the base assembly rings thereby releasing the attachment ring.
摘要翻译：一种用于释放设备袋的分离机构。该机构包括基座组件，可拆卸软环组件，附接环和保持构件。基座组件包括基座构件，孔，以及一个或多个基座组件环。软环组件包括软环基座和软环。软环通过孔插入并且第一个基座组件环插入。软环底座被配置为不被拉过孔。最后一个基座组件环通过连接环插入。保持构件通过软环插入以限制第一基座组件环。基部组件环顺序地接合以将附接环与基部构件联接。保持构件被拉出软环以释放基座组件环，从而释放附接环。

7. 发明授权

US08256717B2 Ground impact cargo parachute release mechanism 有权
标题翻译：地面撞击式降落伞释放机构
公开(公告)号：US08256717B2
公开(公告)日：2012-09-04
申请号：US12794931
申请日：2010-06-07
申请人： James E. Sadeck
发明人： James E. Sadeck
IPC分类号： B64D17/38
CPC分类号： B64D17/38
摘要： A ground impact cargo parachute release mechanism includes a pair of interlocking release elements, one for connection to the parachute the other the cargo; each release element has a pawl and a notch for engaging the pawl of the other release element; a shear pin mounted in both the release elements shears upon parachute opening and enables the pawls and notches to engage; a bias device urges the elements apart upon impact of the load with the ground releasing the pawls from engagement with the notches.
摘要翻译：地面撞击货物降落伞释放机构包括一对互锁释放元件，一个用于连接降落伞的另一个货物; 每个释放元件具有棘爪和用于接合另一个释放元件的棘爪的凹口; 安装在两个释放元件上的剪切销在降落伞开口处剪切并使得棘爪和凹口啮合; 偏置装置在与地面的载荷冲击时促使元件分开，从而释放爪与凹口接合。

8. 发明授权

US08146215B2 Flexible connection and release device and method 有权
标题翻译：灵活的连接和释放装置和方法
公开(公告)号：US08146215B2
公开(公告)日：2012-04-03
申请号：US13053365
申请日：2011-03-22
申请人： James E. Sadeck
发明人： James E. Sadeck
IPC分类号： A44B18/00
CPC分类号： B64D17/38 , B66C1/12 , B66C1/18 , Y10T24/4501 , Y10T24/47 , Y10T29/49947
摘要： A flexible connection and release device which allows quick release while under load. The device includes a first link; a second link; a first sling having one end attached to the first link; a second sling having one end attached to the second link; a tab attached to the first sling; a grommet contained in the tab; a curved length of a first flexible cable connected between two fixed points in the first sling on either side of the tab; a second flexible cable; and a pin or a third flexible cable. The links are connected together with multiple turns of the second flexible cable which forms a loop at its center. The curved length of the first flexible cable is passed through the loop in the second flexible cable and through the grommet so that a part of the first flexible cable protrudes from the grommet. The pin or third cable is passed through the protruding part of the first flexible cable to lock the first flexible cable in place.
摘要翻译：灵活的连接和释放装置，允许在负载下快速释放。该设备包括第一链路; 第二个环节第一吊带，其一端连接到第一连杆; 第二吊带，其一端连接到第二连杆; 连接到第一吊带的翼片; 标签中包含的索环; 第一柔性电缆的弯曲长度连接在所述突片的任一侧上的所述第一吊索中的两个固定点之间; 第二根柔性电缆; 和一根或第三条柔性电缆。链路连接在一起，第二根柔性电缆的匝数在其中心形成一个环。第一柔性电缆的弯曲长度通过第二柔性电缆中的环并穿过索环，使得第一柔性电缆的一部分从索环突出。销或第三电缆穿过第一柔性电缆的突出部分，以将第一柔性电缆锁定到位。

9. 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。

10. 发明申请

US20110297791A1 Ground Impact Cargo Parachute Release Mechanism 有权
标题翻译：地面降落伞降落伞释放机制
公开(公告)号：US20110297791A1
公开(公告)日：2011-12-08
申请号：US12794931
申请日：2010-06-07
申请人： James E. Sadeck
发明人： James E. Sadeck
IPC分类号： B64D17/38
CPC分类号： B64D17/38
摘要： A ground impact cargo parachute release mechanism includes a pair of interlocking release elements, one for connection to the parachute the other the cargo; each release element has a pawl and a notch for engaging the pawl of the other release element; a shear pin mounted in both the release elements shears upon parachute opening and enables the pawls and notches to engage; a bias device urges the elements apart upon impact of the load with the ground releasing the pawls from engagement with the notches.
摘要翻译：地面撞击货物降落伞释放机构包括一对互锁释放元件，一个用于连接降落伞另一个货物; 每个释放元件具有棘爪和用于接合另一个释放元件的棘爪的凹口; 安装在两个释放元件上的剪切销在降落伞开口处剪切并使得棘爪和凹口啮合; 偏置装置在与地面的载荷冲击时促使元件分开，从而释放爪与凹口接合。

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