公开(公告)号：US4737075A

公开(公告)日：1988-04-12

申请号：US885996

申请日：1986-07-16

申请人： Jean-Luc Leman ,  Bruno Guimbal

发明人： Jean-Luc Leman ,  Bruno Guimbal

IPC分类号： B64C27/48 ,  B64C27/32 ,  B64C27/35 ,  B64C27/38

CPC分类号： B64C27/322

摘要： The flapping stop device of the invention is intended for a gyroplane rotor comprising a hub (3) to which each blade (22) is connected by retaining and pivoting members (16) having two frames, one (17) of which is fixed to the hub (3) and the other (19) of which, in an internal radial position with respect to the first one, is locked for movement with the root (23) of the blade (22). The internal frame (19) has, projecting radially inwardly, at least one nose piece (29) having a stop surface and defining a convex cylindrical sliding surface (28) on the internal radial face of the frame (19). The nose piece or pieces (29) and the convex surface (28) cooperate respectively with one or more bearing surfaces (34) and a complementary concave surface (33) of a central stop (30) integral with the hub (3) or with the rotor mast (2).

摘要翻译： 本发明的颤动停止装置用于包括轮毂（3）的陀螺仪转子，所述轮毂（3）通过具有两个框架的保持和枢转构件（16）连接每个叶片（22），其中一个（17）固定到 轮毂（3）和另一个（19）在相对于第一个的内部径向位置被锁定以与叶片（22）的根部（23）一起运动。 内部框架（19）具有径向向内突出的至少一个具有止动表面并且在框架（19）的内部径向表面上限定凸形圆柱形滑动表面（28）的鼻部件（29）。 鼻部件（29）和凸形表面（28）分别与一个或多个轴承表面（34）和与毂（3）成一体的中心止动件（30）的互补凹面（33）配合，或与 转子桅杆（2）。

公开(公告)号：US4630998A

公开(公告)日：1986-12-23

申请号：US732767

申请日：1985-05-10

申请人： Jean-Luc Leman ,  Michel V. Russier ,  Robert J. Suzzi

发明人： Jean-Luc Leman ,  Michel V. Russier ,  Robert J. Suzzi

IPC分类号： B64C27/605 ,  B64C27/35

CPC分类号： B64C27/605

摘要： Apparatus for controlling both collective and cyclic pitch of blades of a helicopter rotor comprises a non-rotating plate which is connected via a fixed caliper and servo controls to a fixed housing and to which is attached the internal ring of a ball race bearing. The external ring of the bearing carries a rotating plate, which is connected by means of rotating caliper or links to each of the rotors and by means of pitch rods to control levers for adjusting the pitch of the blades. The non-rotating plate is fixed to external armatures of laminated joint pieces which are mounted slidingly up and down a guide base. The collective pitch is controlled by sliding the assembly of non-rotating plate and joint pieces up or down the guide base while the cyclic pitch is controlled by inclining the assembly relative to the main rotor shaft. This inclination involves deformations in the laminated joints.

摘要翻译： 用于控制直升机转子的叶片的集合和循环节距的装置包括非旋转板，其经由固定卡钳连接并且伺服控制器连接到固定壳体，并且安装有滚珠轴承的内圈。 轴承的外圈带有旋转板，旋转板通过旋转卡钳或连杆连接到每个转子上，并通过俯仰杆连接，以控制杠杆以调节叶片的桨距。 非旋转板被固定在层叠接头片的外部电枢上，该电枢被滑动地上下安装在导向基座上。 通过将非旋转板和接头件的组件向上或向下滑动在引导基座上，同时通过使组件相对于主转子轴倾斜来控制循环间距来控制集合间距。 该倾斜涉及层压接头中的变形。

公开(公告)号：US4749339A

公开(公告)日：1988-06-07

申请号：US885997

申请日：1986-07-16

申请人： Rene L. Mouille ,  Jean-Luc Leman

发明人： Rene L. Mouille ,  Jean-Luc Leman

IPC分类号： B64C27/35 ,  B64C27/32 ,  B64C27/38

CPC分类号： B64C27/32

摘要： The invention provides an integrated hub-mast with a single piece tubular body which supports, by its hub body part (3), a reinforcing girdle (6) on each side of which openings (10, 11) are formed. For each blade of the rotor a retaining and pivoting member (13), formed preferably by a spherical stratified stop, is fixed to the girdle (6) and is retained in the hub body (3), and this member (13) is also fixed between the ends inside the hub body (3), of the lower (20) and upper (21) branches of a forked fastening part (19) connecting the blade to this member (13), these branches passing through the openings (10, 11) of a corresponding pair of openings. A heel (23) fixed under the lower branch (20) bears against a reciprocal ring (24) mounted on a support (29) in the hub-mast (1), which has external fastenings for coupling to resilient return and drag damping members of the blades.

摘要翻译： 本发明提供了一种具有单件式管状主体的集成式轮毂，其通过其轮毂主体部分（3）支撑在其每一侧上形成有开口（10,11）的加强带（6）。 对于转子的每个叶片，优选地由球形分层止动件形成的保持和枢转构件（13）被固定到腰带（6）并且保持在轮毂体（3）中，并且该构件（13）也是 固定在轮毂体（3）内的端部之间，将叶片连接到该构件（13）的叉形紧固部分（19）的下部（20）和上部（21）分支之间，这些分支穿过开口 ，11）相应的一对开口。 固定在下分支（20）下方的脚跟（23）抵靠安装在轮毂 - 桅杆（1）中的支撑件（29）上的往复环（24）上，所述倒钩环具有外部紧固件，用于联接到弹性回复和阻力阻尼构件 的刀片。

公开(公告)号：US07631737B2

公开(公告)日：2009-12-15

申请号：US11502542

申请日：2006-08-11

申请人： Charles Louis ,  Jean-Luc Leman ,  Patrick Quesne

发明人： Charles Louis ,  Jean-Luc Leman ,  Patrick Quesne

IPC分类号： F16D23/02 ,  B64C27/12

CPC分类号： B64C27/14 ,  F16D11/10

摘要： To achieve automatic setting into coincidence, the following are provided: a mechanical tension elements arranged to act on an upstream member (9) substantially along the axis (X) along which approach elements (13) act, but in the opposite direction; elements (37) for constraining the member (9) in rotation with a mechanical angular guide element; and phase-shifter elements (47) for shifting the phase of the upstream member (9) relative to the downstream member (10) by sliding against a reference that is stationary in rotation relative to the downstream member (10).

摘要翻译： 为了实现自动设置成一致，提供以下：机械张力元件，其布置成基本上沿着所述轴线（X）作用在上游构件（9）上，接近元件（13）沿着所述轴线（X）起作用但沿相反方向; 用于通过机械角度引导元件约束所述构件（9）旋转的元件（37）; 以及用于通过相对于下游构件（10）旋转静止的基准滑动而相对于下游构件（10）移动上游构件（9）的相位的移相器元件（47）。

公开(公告)号：US5388961A

公开(公告)日：1995-02-14

申请号：US56545

申请日：1993-05-05

申请人： Jean-Luc Leman ,  Philippe Legendre ,  Etienne Rampal

发明人： Jean-Luc Leman ,  Philippe Legendre ,  Etienne Rampal

IPC分类号： B64C27/00 ,  B64C27/54 ,  G01L5/04

CPC分类号： G01L5/047 ,  B64C27/008 ,  B64C27/54

摘要： Mechanical assembly for transmitting forces along an axis driven by a substantially axial movement in translation under the effect of a thrust load. This mechanical assembly comprises a transmitting part of the thrust load input movement and a receiving part of the thrust load output movement, said mechanical assembly comprising a detector for detecting the passing of a force threshold represented by a predetermined value of the thrust load, and including an elastic element and an indicator part arranged in such a way that when the thrust load exceeds the threshold value, the thrust load acts on the elastic element and modifies its axial dimension allowing the indicator part to move to the warning position.

摘要翻译： 用于沿轴向传递力的机械组件，其在推力负载的作用下由平移的基本上轴向运动驱动。 该机械组件包括推力载荷输入运动的传递部分和推力载荷输出运动的接收部分，所述机械组件包括检测器，用于检测由推力载荷的预定值表示的力阈值的通过，并且包括 弹性元件和指示器部件，其布置成使得当推力载荷超过阈值时，推力载荷作用在弹性元件上并修改其轴向尺寸，使得指示器部件移动到警告位置。

公开(公告)号：US20070036649A1

公开(公告)日：2007-02-15

申请号：US11502542

申请日：2006-08-11

申请人： Charles Louis ,  Jean-Luc Leman ,  Patrick Quesne

发明人： Charles Louis ,  Jean-Luc Leman ,  Patrick Quesne

IPC分类号： B64C27/00

CPC分类号： B64C27/14 ,  F16D11/10

摘要： To achieve automatic setting into coincidence, the following are provided: a mechanical tension elements arranged to act on an upstream member (9) substantially along the axis (X) along which approach elements (13) act, but in the opposite direction; elements (37) for constraining the member (9) in rotation with a mechanical angular guide element; and phase-shifter elements (47) for shifting the phase of the upstream member (9) relative to the downstream member (10) by sliding against a reference that is stationary in rotation relative to the downstream member (10).

摘要翻译： 为了实现自动设置成一致，提供以下：机械张力元件，其布置成基本上沿着轴线（X）作用在上游构件（9）上，接近元件（13）沿着轴线（X）起作用，但是在相反方向上; 用于通过机械角度引导元件约束所述构件（9）旋转的元件（37）; 以及用于通过相对于下游构件（10）旋转静止的基准滑动而相对于下游构件（10）移动上游构件（9）的相位的移相器元件（47）。

公开(公告)号：US5199849A

公开(公告)日：1993-04-06

申请号：US697383

申请日：1991-05-09

申请人： Jean-Luc Leman

发明人： Jean-Luc Leman

IPC分类号： B64C27/605

CPC分类号： B64C27/605

摘要： The control device is of the type including two annular disks (3,6), a rotating and non-rotating disk, assembled by at least one ball bearing (20) and mounted concentrically about the rotor shaft (1). The non-rotating disk (3) is mounted so as to oscillate with respect to the shaft (1) via a mechanism consisting of swivel/laminated articulations (2, 10). The mechanism for tilting, for axial displacement and for retention in rotation of the non-rotating disk includes two swivel joints (2) which are diametrically opposite on either side of the axis of rotation of the shaft (1) and are centered on the longitudinal tilting axis (A--A) of the non-rotating disk (3). Each swivel joint is retained between a disk support (5), which is mounted so as to slide parallel to the axis of the shaft (1) along a disk guide (4) which is itself coaxial with the shaft (1) and fixed about the latter, and an element (9) for fixing to the non-rotating disk (3). Tilting of this disk ( 3) about the lateral tilting axis (B--B) is permitted by two deformable linking assemblies with laminated blocks (10). Each linking assembly is arranged between the disk support (5) and a swivel joint (2).

摘要翻译： 控制装置是包括两个环形盘（3,6），旋转和非旋转盘，由至少一个滚珠轴承（20）组装并且围绕转子轴（1）同心安装。 非旋转盘（3）通过由旋转/层压关节（2,10）组成的机构安装成相对于轴（1）摆动。 用于轴向位移和用于在非旋转盘的旋转中保持的倾斜机构包括两个旋转接头（2），其在轴（1）的旋转轴线的任一侧上沿径向相对并且在纵向 非旋转盘（3）的倾斜轴（AA）。 每个旋转接头保持在盘支撑件（5）之间，该盘支架（5）安装成沿着本体与轴（1）同轴的盘导向器（4）平行于轴（1）的轴线平行并且围绕 后者，以及用于固定到非旋转盘（3）的元件（9）。 通过具有层压块（10）的两个可变形连接组件允许该盘（3）围绕横向倾斜轴线（B-B）倾斜。 每个连接组件布置在盘支撑件（5）和旋转接头（2）之间。

公开(公告)号：US4652210A

公开(公告)日：1987-03-24

申请号：US648213

申请日：1984-09-07

申请人： Jean-Luc Leman ,  Robert J. Suzzi

发明人： Jean-Luc Leman ,  Robert J. Suzzi

IPC分类号： B64C27/51 ,  B64C27/32 ,  B64C27/48 ,  B64C27/38

CPC分类号： B64C27/322

摘要： The invention relates to a device incorporating retractable stops for limiting the flappings of the blades of the main rotor of a rotorcraft. Each lower stop comprises a convex roller presenting a convex stop surface and bearing a weight at the end of an arm. By its convex roller, the lower stop is mounted to pivot about the pin for retaining the blade on the hub. On the ground, the bearing member is in contact with a lower bearing surface fast with the blade at the level of the pitch control lever, in order to limit the downward flappings of the blade. The lower stop pivots about the pin above the lower plate. The upward flappings of the blade may be limited by upper stops disposed substantially symmetrically below the upper plate. A second lower weight, returned by a spring, and engaging by a nose-shaped element in a notch in the rear of the bearing surface, acts as upper stop. The invention is more particularly applicable to equipping helicopters.

摘要翻译： 本发明涉及一种装置，该装置包括用于限制旋翼航空器的主转子的叶片的翻盖的可缩回止动件。 每个下停止件包括一个凸起的辊子，其具有凸起的止动表面并且在臂的端部处承受重量。 通过其凸轮，下止动件安装成围绕销枢转以将刀片保持在毂上。 在地面上，轴承构件与叶片在俯仰控制杆的水平面处快速地与下轴承表面接触，以便限制叶片的向下的襟翼。 下止动器围绕下板上方的销枢转。 叶片的向上的襟翼可能受到大致对称地设置在上板下方的上止动器的限制。 由弹簧返回的第二个较小的重量，并且通过一个鼻形元件与支承表面后部的凹口啮合起到上限的作用。 本发明更适用于装备直升机。