公开(公告)号：US11970274B2

公开(公告)日：2024-04-30

申请号：US17510118

申请日：2021-10-25

Applicant: AMI Industries, Inc.

Inventor： Bradley Mastrolia ,  Ian Walter Haas

IPC: B64D17/24 ,  B64D17/34 ,  B64D17/78 ,  B64D17/30

CPC classification number: B64D17/24 ,  B64D17/34 ,  B64D17/78 ,  B64D17/30

Abstract: A suspension line assembly for a parachute assembly, comprising a plurality of suspension lines bound together at a confluence, a first riser extending between the confluence and a first attachment location disposed on a first strap, a second riser extending between the confluence and a second attachment location disposed on a second strap and a cradle disposed between the first riser and the second riser.

公开(公告)号：US11958619B2

公开(公告)日：2024-04-16

申请号：US16485846

申请日：2018-02-27

Applicant: RPS AEROSPACE s.r.l.

Inventor： Giacomo Lunerti ,  Nausicaa Asia Vezzoli ,  Andrea Berna

IPC: B64D17/72 ,  B64C39/02 ,  B64D17/02 ,  B64D17/26 ,  B64D17/34 ,  B64D25/00 ,  B64D27/24 ,  B64U10/13 ,  B64U70/83 ,  B64D35/02 ,  B64D35/04 ,  B64U50/19

CPC classification number: B64D17/72 ,  B64C39/024 ,  B64D17/02 ,  B64D17/26 ,  B64D17/34 ,  B64D25/00 ,  B64D27/24 ,  B64D35/02 ,  B64D35/04 ,  B64D2201/00 ,  B64U10/13 ,  B64U50/19 ,  B64U70/83

Abstract: A remote piloted aircraft comprising a secondary flight assembly adapted to intervene in case of failure or an emergency of the aircraft, said secondary flight assembly being provided with an additional control unit configured to process flight relevant data and which includes an additional receiver configured to receive commands from the remote pilot by means of a remote control unit, in case of failure or emergency said additional control unit being configured to generate, as a response, an activation command adapted to activate a first device to expel an upper wing placed in a first compartment of the aircraft and to inflate a lower wing housed in a second compartment of the aircraft, and also to generate an interdiction command of the primary propulsion unit, said upper wing being maneuverable by means of a further remote control unit.

公开(公告)号：US20160176531A1

公开(公告)日：2016-06-23

申请号：US14966997

申请日：2015-12-11

Applicant: Airbus Defence and Space GmbH

Inventor： Juka Biehl

IPC: B64D17/22

CPC classification number: B64D17/22 ,  B64D17/025 ,  B64D17/34

Abstract: A carrier system for carrying out interception maneuvers of a loadbearing paraglider which has a glider having a trailing edge for carrying out the maneuver with at least one interception line is fixed to said edge includes at least one carried load unit, which is connected to the carrier system via a first, short load carrier belt and a second, longer load carrier belt. A carried load connected to the carried load unit is carried by way of the first, short load carrier belt. The trailing edge is adjusted to carry out the maneuver by the gravitational force of the carried load, in that the first, short load carrier belt is separated and the carried load is carried by way of the longer, second load carrier belt.

Abstract translation: 一种用于执行承载滑翔伞的拦截机动的载体系统，其具有具有用于执行具有至少一个拦截线的操纵的后缘的滑翔机被固定到所述边缘，所述至少一个承载的负载单元连接到所述载体 系统经由第一短负载传送带和第二较长负载传送带。 连接到承载的负载单元的承载负载通过第一短负载传送带承载。 后缘被调节以通过承载负载的重力来执行机动，因为第一短负载传送带被分离，承载负载通过较长的第二负载传送带承载。

公开(公告)号：US20130048787A1

公开(公告)日：2013-02-28

申请号：US13222223

申请日：2011-08-31

Applicant: David Ray Riley ,  Zachary Anton Nielsen

Inventor： David Ray Riley ,  Zachary Anton Nielsen

IPC: B64D1/08

CPC classification number: B64D1/08 ,  B64D1/14 ,  B64D17/34

Abstract: A steerable container delivery system (“CDS”) includes a pallet configured with inflatable fins for steering a CDS cargo bundle during free fall when airdropped. The inflatable fins are inflated shortly after deployment using compressed air carried by a tank in the pallet. A flight management computer (“FMS”) continuously monitors the location of the CDS bundle using GPS technology and determines a vector to a drop location based on stored GPS measurements. The FMC continuously monitors and positions the CDS bundle over the drop location, and is able to independently rotate the fins to control the position of the CDS bundle, either by rotating the CDS bundle or laterally moving it. At the appropriate altitude, the FMC causes the main parachute to open to slow the descent of the CDS bundle for impact.

Abstract translation: 可转向的集装箱运输系统（CDS）包括一个托盘，该货盘配置有可充气的散热片，用于在空运时自由落体时转向CDS货物捆。 展开后不久充气的翅片在托盘中由坦克携带的压缩空气充气。 飞行管理计算机（FMS）使用GPS技术连续监视CDS束的位置，并根据存储的GPS测量结果确定向下降位置的向量。 FMC连续监测和定位CDS束在放置位置，并且能够独立地旋转散热片以通过旋转CDS束或横向移动来控制CDS束的位置。 在适当的高度，FMC会使主降落伞打开，以减缓CDS束的下降以产生冲击。

公开(公告)号：US20120305713A1

公开(公告)日：2012-12-06

申请号：US13429939

申请日：2012-05-17

Applicant: Frank Deazley ,  Scott Hilton

Inventor： Frank Deazley ,  Scott Hilton

IPC: B64D17/34

CPC classification number: B64D17/34 ,  B64D17/025

Abstract: A method of controlling a ram air parachute using a variable trim platform is disclosed. In a particular embodiment, the method includes securing a front trim control line between a front portion of the variable trim platform and a guidance control unit and securing a rear trim control line between a rear portion of the variable trim platform and the guidance control unit. The method also includes securing ram air parachute suspension lines between the variable trim platform and the parachute and securing guidance unit risers between the variable trim platform and the guidance unit. An attachment point of the guidance unit risers to the variable trim platform is separate from an attachment point of the suspension lines to the platform to create a pivot point for the variable trim platform to rotate about.

Abstract translation: 公开了一种使用可变修剪平台来控制冲压空气降落伞的方法。 在一个具体实施例中，该方法包括将可调整平台的前部与引导控制单元之间的前装饰控制线固定，并将后装饰控制线固定在可调整平台的后部与引导控制单元之间。 该方法还包括在可调整平台和降落伞之间固定冲压空气降落伞悬挂线，并将引导单元立管固定在可变调节平台和引导单元之间。 引导单元的连接点上升到可变修剪平台，与悬挂线的连接点分离到平台，以创建用于可变修剪平台围绕的旋转点。

公开(公告)号：US06889942B2

公开(公告)日：2005-05-10

申请号：US10315466

申请日：2002-12-09

Applicant: Daniel Preston

Inventor： Daniel Preston

IPC: B64D1/14 ,  B64D17/02 ,  B64D17/04 ,  B64D17/08 ,  B64D17/34 ,  B64D17/38 ,  B64D17/54 ,  B64D17/00

CPC classification number: F42B10/56 ,  B64D1/08 ,  B64D1/14 ,  B64D17/025 ,  B64D17/04 ,  B64D17/08 ,  B64D17/34 ,  B64D17/38 ,  B64D17/54 ,  B64D17/74 ,  F42B4/28 ,  F42B10/58 ,  G05D1/105

Abstract: An autonomous guided parachute system for cargo drops that divides the requirements of guidance and soft landing into separate parachutes. Said invention includes a high wing-loaded ram air parachute for guidance, a larger round parachute for soft landing, a harness/container system, flight computer, position sensors and actuation system. The system is dropped from an airplane. A predetermined period of drogue fall ensures a stable position prior to deploying the guidance parachute. The flight controller determines a heading to intersect with an area substantially above the desired target and controls the guidance parachute via pneumatic actuators connected to the parachutes steering lines to fly on that heading. At a minimum altitude prior to the system's impact with the ground the flight computer transitions the system from the fast high performance guidance parachute to a larger landing parachute by releasing the guidance parachute to static line extract and deploy the landing parachute. If the system reaches a position substantially above target area prior to the parachute transition altitude the flight computer controls the system into a spiral dive or other rapid altitude dropping maneuver until the transition altitude is reached. Once transitioned to the landing parachute the system descends for a brief period unguided under the landing parachute until touchdown.

Abstract translation: 货舱的自主引导降落伞系统，将引导和软着陆的要求分为单独的降落伞。 所述发明包括用于引导的高机翼加载式冲压空气降落伞，用于软着陆的较大圆形降落伞，线束/容器系统，飞行计算机，位置传感器和致动系统。 系统从飞机上掉下来。 在部署导向降落伞之前，预定的锥套落下时间确保了稳定的位置。 飞行控制器确定与基本上高于期望目标的区域相交的航向，并通过连接到降落伞转向线的气动执行器在该航向上飞行来控制引导降落伞。 在系统与地面撞击之前的最低高度，飞行计算机将系统从快速高性能指导降落伞转换到更大的降落伞，通过将引导降落伞释放到静态线路提取并部署着陆降落伞。 如果系统在降落伞转换高度之前达到大致高于目标区域的位置，飞行计算机将系统控制成螺旋式潜水或其他快速高度降落机动，直到达到过渡高度。 一旦过渡到着陆降落伞，该系统在登陆降落伞之前的短暂时间内下降直到达阵。

公开(公告)号：US20020166925A1

公开(公告)日：2002-11-14

申请号：US09853973

申请日：2001-05-11

Inventor： Richard J. Benney ,  Glen J. Brown

IPC: B64D017/00 ,  B64D019/00 ,  B64D021/00 ,  B64D023/00

CPC classification number: B64D17/78 ,  B64D17/00 ,  B64D17/34 ,  B64D23/00

Abstract: A soft landing assembly for a parachute includes an altitude sensor mounted on the parachute and a control assembly mounted on the parachute for activating parachute landing velocity affectors at preselected altitudes detected by the altitude sensor. A first of the parachute landing velocity affectors is an automatic riser slip actuator for providing a riser slip, and thereby horizontal velocity reduction at an optimum time and in an optimum direction. A second of the parachute landing velocity affectors is an automatic pneumatic muscle retraction actuator for providing vertical retraction of a parachutist, and thereby vertical velocity reduction of the parachutist, at an optimum time prior to impact with ground.

Abstract translation: 用于降落伞的软着陆组件包括安装在降落伞上的高度传感器和安装在降落伞上的控制组件，用于在由高度传感器检测的预选高度处激活降落伞着陆速度感应器。 降落伞着陆速度探测器中的第一个是用于提供立管滑动的自动提升滑块致动器，从而在最佳时间和最佳方向上水平减速。 降落伞着陆速度感应器中的第二个是自动气动肌肉收缩致动器，用于在撞击地面之前的最佳时间提供飞镖的垂直回缩，从而使飞镖的垂直速度降低。

公开(公告)号：US06364251B1

公开(公告)日：2002-04-02

申请号：US09574281

申请日：2000-05-19

Applicant: James H. Yim

Inventor： James H. Yim

IPC: B64D1702

CPC classification number: B64D17/025 ,  B64C3/30 ,  B64C31/036 ,  B64D17/34 ,  Y10S244/90

Abstract: The airwing structure according to the present invention comprises of an airfoil structure, a main frame, and a means for providing a downward and a forward tension on the airfoil structure. The airfoil structure further comprises of a leading edge, a trailing edge, a left edge, a right edge, a central wing root, and a plurality of chord lines. Moreover, the airfoil structure comprises of a substantially flexible surface skin and the airfoil structure also has a downward arc for producing lift by aerodynamic forces exerted thereon. The main frame attached to the airfoil structure comprises of a leading bar and a supporting bar. The leading bar is fixedly attached to the leading edge supporting and maintaining the leading edge from collapsing. The supporting bar is attached to the leading bar and attached to the trailing edge supporting and maintaining the airfoil structure from collapsing.

Abstract translation: 根据本发明的抽风结构包括翼型结构，主框架和用于在翼型结构上提供向下和向前张力的装置。 翼型结构还包括前缘，后缘，左边缘，右边缘，中央翼根和多条弦线。 此外，翼型结构包括基本上柔性的表面皮肤，翼型结构还具有向下的弧形，用于通过施加在其上的空气动力来产生升力。 连接到翼型结构的主框架包括导杆和支撑杆。 引导杆固定地连接到前缘，支撑并保持前缘不起皱。 支撑杆连接到引导杆并且附接到后缘，支撑并保持翼型结构不会塌陷。

公开(公告)号：US3989207A

公开(公告)日：1976-11-02

申请号：US533532

申请日：1974-12-17

Applicant: Heinz B. Mader

Inventor： Heinz B. Mader

IPC: B64D17/34 ,  B64D17/76

CPC classification number: B64D17/34 ,  B64D17/76

Abstract: The invention relates to a parachute having a circular canopy and rigging lines secured to the base of said canopy. A continuous strip of material is attached to said rigging lines below the canopy base whereby, during folding up of the canopy during packing of the parachute, a section of the strip between each pair of adjacent rigging lines can be folded in between each respective section of the canopy.

Abstract translation: 本发明涉及一种降落伞，其具有固定到所述舱盖底部的圆形顶盖和索具线。 连续的材料条带连接到伞篷底部下面的所述索具线，由此在降落伞的堆叠期间在折叠顶篷期间，每对相邻索具之间的条带的一部分可以折叠在每个相应的部分 冠层。

公开(公告)号：US3724277A

公开(公告)日：1973-04-03

申请号：US3724277D

申请日：1971-03-22

Applicant: PARMENTIER J

Inventor： PARMENTIER J

IPC: B64D17/34 ,  G01D11/10 ,  G01D11/24

CPC classification number: B64D17/34

Abstract: A case or enclosure enclosing at least one instrument which is protected against shocks by a body of neoprene or the like elastomer. The elastomer body is provided with a recess the shape and size of which match those of the instrument embedded within said recess, preferably open at both ends. Such cases are intended for use by parachutists or else for laboratory purposes or again on vehicle instrument boards.

Abstract translation: 封闭至少一个仪器的外壳或外壳，防止氯丁橡胶或类似弹性体的冲击。 弹性体设置有凹部，其形状和尺寸与嵌入所述凹部内的仪器的形状和尺寸相匹配，优选在两端敞开。 这种情况是由飞行员使用，或者用于实验室目的或再次用于车辆仪表板上。