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1. 发明授权

US07575198B2 Control handle for use with a towable airfoil 失效
标题翻译：用于牵引翼型的控制手柄
公开(公告)号：US07575198B2
公开(公告)日：2009-08-18
申请号：US11927344
申请日：2007-10-29
申请人： Corwin Hardham , Johannes Van Niekerk
发明人： Corwin Hardham , Johannes Van Niekerk
IPC分类号： B64D17/14
CPC分类号： B63B35/7979 , B63B35/817 , B63B2035/735 , Y10S244/901 , Y10S244/904
摘要： For use with towable airfoils used to supply lift to a towed rider to assist with jumping in sports and recreation, a handle system having one or more control lines for coupling to the airfoil, and a line for coupling the handle to a tow vehicle, the one or more control lines and line for coupling to the tow vehicle being coupled together by a tension translation mechanism that divides the tension from the line for the tow vehicle to the one or more control lines by a predetermined factor, which typically would be other than 1:1. The handle system may further include an engagement mechanism for engaging the one or more control lines to lock or brake a line.
摘要翻译：为了使用用于向拖曳的乘客提供电梯以协助跳跃运动和娱乐的可拖动翼型件，具有用于联接到翼型件的一个或多个控制线的手柄系统和用于将手柄连接到拖车车辆的线，一个或多个控制线和用于联接到牵引车辆的线通过张力平移机构联接在一起，所述张力平移机构将牵引车辆的线路的张力与一个或多个控制线路分开预定的因子，该预定系数通常将不同于 1：1。手柄系统还可以包括用于接合一个或多个控制线以锁定或制动线的接合机构。

2. 发明授权

US6131856A Parachute trajectory control 失效
标题翻译：降落伞轨迹控制
公开(公告)号：US6131856A
公开(公告)日：2000-10-17
申请号：US90668
申请日：1998-06-04
申请人： Glen J. Brown
发明人： Glen J. Brown
IPC分类号： B64D17/06 , B64D17/34 , B64D17/14
CPC分类号： B64D17/06 , B64D17/34 , Y10S244/902
摘要： A parachute has its suspension lines divided into groups, each group connected to the load through a linear actuator. During descent of the parachute, foreshortening of an actuator or of any group of adjacent actuators causes the parachute trajectory to move in the direction of the foreshortened actuator. Multiple parachutes connected to a single load, with each parachute being connected to the load through an actuator, can similarly have their trajectory controlled. The trajectory of the parachute can also be changed by a system of normally foreshortened actuators which lengthen by actuation. Simultaneous, rapid shortening of all actuators just before ground impact can be used to reduce the descent velocity at ground impact.
摘要翻译：降落伞将其悬挂线分成组，每组通过线性致动器连接到负载。在降落伞下降期间，致动器或任何相邻致动器组的缩短导致降落伞轨迹沿缩短的致动器的方向移动。连接到单个负载的多个降落伞，每个降落伞通过致动器连接到负载，可以类似地控制其轨迹。降落伞的轨迹也可以通过通过致动延长的正常缩短的致动器的系统来改变。在地面撞击之前，所有执行器的同时快速缩短可用于降低地面冲击下降速度。

3. 发明授权

US4191349A Parachute having an improved multi-cell canopy 失效
标题翻译：降落伞具有改进的多细胞冠层
公开(公告)号：US4191349A
公开(公告)日：1980-03-04
申请号：US926523
申请日：1978-07-19
申请人： Marcel H. Pravaz
发明人： Marcel H. Pravaz
IPC分类号： B64D17/02 , B64D17/14
CPC分类号： B64D17/025 , Y10S244/902
摘要： The multi-cell canopy of the gliding wing type comprises an upper wall and a lower wall interconnected by ribs forming partition wall defining parallel cells open on the leading edge of the wing. Parachute control lines are secured to the trailing edge for deforming a part of the latter which forms a plain flap. The canopy comprises in its upper wall at least one air outlet passage which has the shape of a rearwardly facing slot so as to direct a laminar current of air tangentially of the upper wall.
摘要翻译：滑翔翼型的多电池盖包括上壁和下壁，肋通过形成分隔壁的肋互连，限定在翼的前缘上开口的平行细胞。降落伞控制线固定到后缘以使后者的一部分变形，形成平板皮瓣。顶盖在其上壁上包括至少一个空气出口通道，该空气出口通道具有向后的槽的形状，以便引导空气的层流与上壁切向。

4. 发明授权

US4015801A Maneuverable, ram air inflated, flexible aerial wing 失效
标题翻译：机动，冲压空气膨胀，柔性空中翼
公开(公告)号：US4015801A
公开(公告)日：1977-04-05
申请号：US627118
申请日：1975-10-30
申请人： William H. Womble , John D. Campbell
发明人： William H. Womble , John D. Campbell
IPC分类号： B64D17/02 , B64D17/14
CPC分类号： B64D17/025
摘要： A maneuverable, ram air inflated, flexible aerial wing includes a plurality of adjacent, forward facing air cells having first openings along the leading edge thereof and a control surface extending between the aforesaid cells and the trailing edge. Generally rectangular in overall shape the cells are of such size and so positioned, and include rearward facing second openings, as to displace the separation point of the relative airflow across the upper surface further toward the trailing edge than with known devices, and which therefore achieves a higher lift to drag ratio. Further, the control line system and a series of rear vents combine to reduce the force required to lower the surface and help prevent erratic flight.
摘要翻译：可操纵的，冲压空气充气的柔性空中翼包括多个相邻的朝前的空气室，其具有沿其前缘的第一开口和在上述单元和后缘之间延伸的控制表面。通常矩形的整体形状，电池具有这样的尺寸和定位，并且包括面向后的第二开口，以使相对气流的分离点相对于已知的装置更靠近上表面而朝向后缘移动，从而实现更高的提升阻力比。此外，控制线系统和一系列后排气口结合起来，以减少降低表面所需的力并帮助防止不规则的飞行。

5. 发明授权

US3493199A Autorotating parachute 失效
标题翻译：自动停车
公开(公告)号：US3493199A
公开(公告)日：1970-02-03
申请号：US3493199D
申请日：1967-09-19
申请人： FLATAU ABRAHAM
发明人： FLATAU ABRAHAM
IPC分类号： B64D17/00 , B64D17/14 , B64D17/18
CPC分类号： B64D17/00

6. 发明授权

US3433441A Flexible aerodynamic body 失效
标题翻译：灵活的航空身体
公开(公告)号：US3433441A
公开(公告)日：1969-03-18
申请号：US3433441D
申请日：1966-05-16
申请人： NORTH AMERICAN ROCKWELL
发明人： CUMMINGS ALAN F
IPC分类号： B64C31/036 , B64D17/02 , B64D17/34 , B64D17/14 , B64D17/18
CPC分类号： B64D17/025 , B64C31/036 , Y10S244/903

7. 发明授权

US3420474A Method for collapsing an aerodynamic decelerating vehicle 失效
标题翻译：用于收缩气动减速机的方法
公开(公告)号：US3420474A
公开(公告)日：1969-01-07
申请号：US3420474D
申请日：1967-08-25
申请人： US NAVY
发明人： NOLES RONALD C , CRAIG JIMMIE M
IPC分类号： B64D17/38 , B64D17/78 , B64B1/58 , B64D17/14 , F41J9/00
CPC分类号： B64D17/38 , B64D17/78

8. 发明授权

US2120177A Parachute 失效
公开(公告)号：US2120177A
公开(公告)日：1938-06-07
申请号：US8920736
申请日：1936-07-06
申请人： HART RICHARD H
发明人： HART RICHARD H
IPC分类号： B64D17/14
CPC分类号： B64D17/14

9. 发明申请

US20210053690A1 VEHICLE RECOVERY SYSTEM 有权
公开(公告)号：US20210053690A1
公开(公告)日：2021-02-25
申请号：US16545457
申请日：2019-08-20
申请人： AVIATION SAFETY RESOURCES, INC.
发明人： LARRY EDWARD WILLIAMS , ROBERT LAFRANCE , GEORGE GALLOWAY
IPC分类号： B64D17/80 , B64D17/14 , B64D17/30 , B64D17/24 , B64D17/72
摘要： A vehicle recovery system includes a harness having a hub and a plurality of cords each including opposite first and second ends. The first ends are each coupled to the hub. The second ends are each configured to be connected to a fuselage of a vehicle. A tractor rocket includes a body and a bridle. The bridle includes a first end coupled to the body and an opposite second end. A parachute includes a riser, a canopy and a plurality of suspension lines. The suspension lines each include a first end coupled the canopy and an opposite second end coupled a first end of the riser. An opposite second end of the riser is coupled to the hub. The second end of the bridle is coupled to the first end of the riser.

10. 发明授权

US5174527A Annular spinning parachute 失效
标题翻译：环形降落伞
公开(公告)号：US5174527A
公开(公告)日：1992-12-29
申请号：US580244
申请日：1990-09-10
申请人： Anthony D. Kasher
发明人： Anthony D. Kasher
IPC分类号： B64D17/14 , F42B10/56
CPC分类号： B64D17/14 , F42B10/56
摘要： An annular spinning parachute is composed of an annular canopy symmetrical about an apex, suspension lines of substantially the same length and interconnected together at the canopy apex and extending radially outwardly therefrom across the canopy and downwardly therefrom for coupling to an object supported by the parachute, and centerlines interconnected with the suspension lines at the canopy apex and extending downwardly therefrom for coupling to the object supported by the parachute. The annular canopy includes fabric panels each having a generally trapezoidal shape defined by a pair of opposing inner and outer borders with the outer border being greater length than the inner border and a pair of opposing side borders of substantially the same length. The annular canopy also includes inner and outer lateral bands respectively extending along and connected to the inner and outer borders of the fabric panels so as to dispose the panels in circumferentially spaced relation with respect to one another upon inflation of the canopy. The inner and outer bands and spaced panels define a central opening in the canopy having thhe canopy apex at the center of the opening and a plurality of exhaust vents arranged in alternating relation with the panels between the side borders of adjacent pairs of the panels.
摘要翻译：环形旋转降落伞由围绕顶点对称的环形舱盖组成，悬挂线基本上相同的长度，并且在冠层顶端处互连在一起，并从其上径向向外延伸穿过冠层并向下延伸，用于联接到由降落伞支撑的物体，以及与冠层顶点处的悬挂线相互连接并且向下延伸的中心线，用于联接到由降落伞支撑的物体。环形顶盖包括各自具有由一对相对的内部和外部边界限定的大致梯形形状的织物面板，外部边界的长度大于内部边界的长度以及基本上相同长度的一对相对的侧边缘。环形罩还包括分别沿着织物面板的内边界和外边缘延伸并连接到织物面板的内边缘和外边缘的内侧和外侧边带，以便在罩盖膨胀时将面板相对于彼此以周向间隔开的关系布置。内部和外部带和间隔开的面板限定在顶盖中的中心开口，其具有位于开口中心处的顶盖顶点和与相邻面板对侧边缘之间的面板交替关系排列的多个排气口。

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