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公开(公告)号：US4299539A
公开(公告)日：1981-11-10
申请号：US962303
申请日：1978-11-20
申请人： Alois Schwarz , Karlheinz Mautz , Michael Stephan
发明人： Alois Schwarz , Karlheinz Mautz , Michael Stephan
CPC分类号： B64C27/45
摘要： The present four-blade rotor is made up of two blade pairs, each blade pairaving two rotor blades arranged diametrically opposite one another. The blades of each blade pair are coupled to each other by means of a coupling loop for taking up centrifugal forces produced by the rotation of the blades. The present rotor system also has a centering device including a centering body and tension straps for each coupling loop. The tension straps connect the respective loop end to the centering body whereby the two coupling loops may be centered in the rotor head practically without play and without substantially limiting the free movement of the coupling loops.
摘要翻译： 本发明的四叶片转子由两个叶片对构成，每个叶片对具有彼此直径相对设置的两个转子叶片。 每个叶片对的叶片通过联接回路彼此联接，以吸收由叶片的旋转产生的离心力。 本转子系统还具有定心装置，其包括用于每个联接回路的定心体和张力带。 张力带将相应的环端连接到定心体，由此两个耦合回路可以在转子头部中实际上不起跳而不会基本上限制耦合回路的自由运动。
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公开(公告)号：US4243359A
公开(公告)日：1981-01-06
申请号：US972878
申请日：1978-12-26
申请人： Alois Schwarz , Karlheinz Mautz , Michael Stephan
发明人： Alois Schwarz , Karlheinz Mautz , Michael Stephan
CPC分类号： B64C27/45 , B64C27/327
摘要： The present hingeless rotor structure, especially for rotary wing aircraft,omprises at least one pair of rotor blades, whereby the blades of a pair are arranged diametrically opposite each other. The blades are secured to a rotor head for proper blade angle adjustment. Each blade has its root or radially inner end secured in a blade root sleeve which in turn is held in a respective blade angle bearing bushing. The blades of a pair are interconnected by a tension resistant, torsionally yielding member. One bearing which is pressure loadable in the direction of the longitudinal blade axis is provided for each blade pair between one of the respective blade root sleeves and the corresponding blade angle bearing bushing. The tension resistant, torsionally yielding member is capable of a certain stretching or elongation during operation. In order to compensate for such an elongation, the tension resistant, torsionally yielding members are installed in such a manner that in the rest or non-rotating condition of the blades, the center is radially displaced from the axis of rotation of the rotor head toward the respective pressure loadable bearing by one half of the length of said elongation.
摘要翻译： 本发明的无铰链转子结构，特别是用于旋转飞行器的铰链转子结构包括至少一对转子叶片，由此一对叶片彼此径向相对布置。 叶片被固定到转子头以进行适当的叶片角度调整。 每个叶片的根部或径向内端固定在叶片根部套筒中，叶片根部套筒又保持在相应的叶片角度轴承衬套中。 一对刀片通过抗张力扭转的构件相互连接。 在各个叶片根部套筒之一和相应的叶片角度轴承衬套之间为每个叶片对提供沿纵向叶片轴线的方向可承受压力的一个轴承。 抗张力扭转屈服构件能够在操作期间具有一定的拉伸或伸长。 为了补偿这种伸长，抗张力扭转的构件以这样一种方式安装，即在叶片的静止或不旋转状态下，中心从转子头的旋转轴向径向偏移 相应的可承受压力的轴承长度为所述伸长长度的一半。
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公开(公告)号：US4432696A
公开(公告)日：1984-02-21
申请号：US300378
申请日：1981-09-08
申请人： Michael Stephan , Karlheinz Mautz , Alois Schwarz
发明人： Michael Stephan , Karlheinz Mautz , Alois Schwarz
摘要： The blade angle of the blades of a rotary wing aircraft is adjusted by a control rod (5) inside the hollow rotor head operating a control shaft (8) extending radially out of the rotor head in axial alignment with the blade angle adjustment axis. The adjustment movement of the shaft (8) is transmitted to the respective blade (3.3) by a yoke (11, 12) and a torsion-stiff sleeve (7) which bridge the blade root (3.1) and the torsion yielding blade neck (3.2) respectively. The blade root (3.1) is connected to the rotor hub (1) by a forked member (2) through which a portion (11) of the yoke extends for connection to the control shaft.
摘要翻译： 旋转翼飞行器的叶片的叶片角度通过在中空转子头内部的控制杆（5）来调节，所述控制杆操作控制轴（8），所述控制轴（8）沿着与叶片角度调整轴线轴向对准地从转子头径向延伸。 轴（8）的调节运动通过轭（11,12）和扭转刚性套筒（7）传递到相应的叶片（3.3），扭矩刚性套筒（7）将叶片根部（3.1）和扭转屈服叶片颈部 3.2）。 叶片根部（3.1）通过叉形构件（2）连接到转子轮毂（1），轭架的一部分（11）通过该叉形件延伸用于连接到控制轴。
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公开(公告)号：US4251188A
公开(公告)日：1981-02-17
申请号：US962304
申请日：1978-11-20
申请人： Alois Schwarz , Karlheinz Mautz , Michael Stephan
发明人： Alois Schwarz , Karlheinz Mautz , Michael Stephan
CPC分类号： B64C27/45
摘要： The present four-blade rotor structure comprises two pairs of rotor blades.iametrically opposite each other located blades form a pair and the blades of a pair are connected to each other by coupling belts which are tension resistant and torsionally yielding. One coupling belt extends substantially horizontally whereas the other extends substantially vertically. The coupling belts are centered in the rotor head by respective centering bodies. The centering bodies are connected to their respective belt by bearing elements capable of taking up pressure loads while simultaneously permitting a blade angle adjustment. In a modification the bearings may be slide bearings.
摘要翻译： 现有的四叶片转子结构包括两对转子叶片。 彼此相对定位的叶片形成一对，并且一对的叶片通过具有抗张力和扭转屈服的连接带彼此连接。 一个联接带基本上水平地延伸，而另一个连接带基本上垂直地延伸。 联轴器带通过相应的定心体在转子头中心。 定心体通过能够承受压力负载的轴承元件连接到它们各自的带，同时允许叶片角度调节。 在修改中，轴承可能是滑动轴承。
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5.发明授权Apparatus for adjusting the tracking of the blades in a rotor, especially for a rotary wing aircraft 失效用于调节转子中的叶片的跟踪的装置，特别是用于旋翼机
公开(公告)号：US4585394A
公开(公告)日：1986-04-29
申请号：US705012
申请日：1985-02-25
申请人： Alois Schwarz , Karlheinz Mautz
发明人： Alois Schwarz , Karlheinz Mautz
摘要： The blade angle of the blades is adjustable in a rotor for a rotary wing craft by a lever mechanism (13, 14 or 41, 42) secured to the radially inner end of an extension bushing (7; 7.1) or shaft (43). The extension bushing (7; 7.1) or shaft (43) is connected with its radially outer lever (15 or 44) to the blade root (2) or a blade root mounting (39, 50) of a rotor blade in an angular position adjustable manner for adjusting the tracking of the blades. The bushing (7; 7.1) or shaft (43) is adjustable in its angular position relative to the blade root (2) by adjustment screws cooperating with a free end of the lever (15 or 44) which reaches into a gap between two of such adjustment screws (16 or 45) cooperating with counter nuts (17 or 46). By adjusting the angular position of the bushing or shaft with the screws it is possible to assure a uniform tracking among all the blades of a multiblade rotor. Such uniform tracking is desirable if the blades of a rotor are to rotate in the same plane.
摘要翻译： 叶片的叶片角度可以通过固定到延伸套管（7,7.1）或轴（43）的径向内端的杠杆机构（13,14或41,42）在用于旋转翼飞行器的转子中是可调节的。 延伸套管（7; 7.1）或轴（43）与其径向外部杠杆（15或44）连接到叶片根部（2）或转子叶片的叶片根部安装件（39,50）处于角位置 可调节的方式来调整叶片的跟踪。 衬套（7; 7.1）或轴（43）可以通过调节螺丝与其相对于叶片根部（2）的角度位置调节，调节螺钉与杠杆（15或44）的自由端相配合，该自由端到达两个 这种调节螺钉（16或45）与反螺母（17或46）配合。 通过利用螺钉调整衬套或轴的角度位置，可以确保在多叶片转子的所有叶片之间的均匀跟踪。 如果转子的叶片在相同的平面中旋转，则这种均匀跟踪是期望的。
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6.发明授权
公开(公告)号：US4545733A
公开(公告)日：1985-10-08
申请号：US474044
申请日：1983-03-10
申请人： Alois Schwarz , Karlheinz Mautz
发明人： Alois Schwarz , Karlheinz Mautz
摘要： The blade angle of the blades is adjustable in a rotor for a rotary wing craft by a lever mechanism (13, 14 or 41, 42) secured to the radially inner end of an extension bushing (7; 7.1) or shaft (43). The extension bushing (7; 7.1) or shaft (43) is connected with its radially outer lever (15 or 44) to the blade root (2) or a blade root mounting (39, 50) of a rotor blade in an angular position adjustable manner for adjusting the tracking of the blades. The bushing (7; 7.1) or shaft (43) is adjustable in its angular position relative to the blade root (2) by adjustment screws cooperating with a free end of the lever (15 or 44) which reaches into a gap between two of such adjustment screws (16 or 45) cooperating with counter nuts (17 or 46). By adjusting the angular position of the bushing or shaft with the screws it is possible to assure a uniform tracking among all the blades of a multiblade rotor. Such uniform tracking is desirable if the blades of a rotor are to rotate in the same plane.
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公开(公告)号：US4321013A
公开(公告)日：1982-03-23
申请号：US142848
申请日：1980-04-22
申请人： Alois Schwarz , Karlheinz Mautz
发明人： Alois Schwarz , Karlheinz Mautz
CPC分类号： B64C27/32 , Y02E10/721
摘要： In a rotor for a rotary wing aircraft, an integral central headpiece supps the rotor blades. The headpiece consists of two plates interconnected by a centrally arranged distance member. Each plate has a similar star-shape with at least four angularly spaced point-like arms. Each plate is formed of a number of superposed layers with each layer containing continuous loops extending in the direction of the point-like arms. At least one loop extends from one point-like arm into another diametrically opposite point-like arm. Others of the loops, located in the other point-like arms, extend radially outwardly from the loop extending through the two point-like arms. The headpiece consisting of the plates and distance member, is a unitary or integral structure.
摘要翻译： 在用于旋转飞行器的转子中，整体的中央头盔支撑转子叶片。 头盔由通过中心布置的距离构件互连的两个板组成。 每个板具有与至少四个角度间隔开的点状臂相似的星形。 每个板由多个重叠层形成，每个层包含在点状臂的方向上延伸的连续环。 至少一个环从一个点状臂延伸到另一个直径相对的点状臂。 位于另一个点状臂中的其他环路从延伸穿过两个点状臂的环径向向外延伸。 由板和距离构件组成的头盔是一体的或一体的结构。
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公开(公告)号：US4183718A
公开(公告)日：1980-01-15
申请号：US855668
申请日：1977-11-29
申请人： Karlheinz Mautz , Emil Weiland , Alois Schwarz
发明人： Karlheinz Mautz , Emil Weiland , Alois Schwarz
CPC分类号： B64C27/45
摘要： A rotor for a rotary wing aircraft includes a rotor head and an even number of rotor blades arranged in pairs about the rotor head. The rotor blades of each pair are located diametrically opposite each other and each blade has a root end positioned radially inwardly toward the head. Bearings carried by the rotor head pivotally support each of the rotor blades. A torsionally elastic connection member extends between and connects the roots of a pair of rotor blades, and the connection member is mounted at its longitudinal center in the rotor head for pivotal movement about its longitudinal axis.
摘要翻译： 用于旋转翼飞行器的转子包括转子头部和偶数个转子叶片成对设置的转子叶片。 每对转子叶片彼此沿径向相对，并且每个叶片具有朝向头部径向向内定位的根端。 由转子头承载的轴承枢转地支撑每个转子叶片。 扭转弹性连接构件在一对转子叶片的根部之间延伸并连接，并且连接构件在其纵向中心处安装在转子头部中，用于围绕其纵向轴线枢转运动。
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公开(公告)号：US4352632A
公开(公告)日：1982-10-05
申请号：US231042
申请日：1981-02-04
摘要： The rotor blades of a rotary wing aircraft are mounted at their blade rootspon a rotor head formed as an integral body of composite fiber material shaped to define a plurality of bifurcated rotor blade support arms between which the blade roots are mounted. Each of the blades is formed, at least in the region of the blade roots, with a laminated configuration including at least two layers formed with a fiber loop having a unidirectional fiber orientation extending longitudinally of the rotor blade and about a load-bearing connection between the blade root and the rotor head. An intermediate layer having a crosswise fiber orientation is provided between each of the at least two layers of the blade root which integrally joins the two layers and the fiber loop is enclosed by support members at its longitudinal edges at the inside and outside thereof at least in the region of the load-bearing connection.
摘要翻译： 旋转翼飞行器的转子叶片在叶片根部安装在转子头上，该转子头形成为复合纤维材料的整体，该复合纤维材料成形为限定多个分叉的转子叶片支撑臂，叶片根部之间安装有多个分叉的转子叶片支撑臂。 每个叶片至少在叶片根部的区域中形成为包括由纤维环形成的至少两层的层压构造，所述纤维环具有沿着转子叶片纵向延伸的单向纤维取向，以及围绕在转子叶片纵向延伸的承载连接 叶片根部和转子头部。 具有横向纤维取向的中间层设置在叶片根部的至少两层之间，其一体地连接两层，并且纤维环在其内部和外部的纵向边缘处由支撑构件包围，至少在 承重连接区域。
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公开(公告)号：US4257738A
公开(公告)日：1981-03-24
申请号：US886653
申请日：1978-03-15
申请人： Alois Schwarz , Karlheinz Mautz
发明人： Alois Schwarz , Karlheinz Mautz
CPC分类号： B64C27/32 , B64C27/33 , B64C27/35 , Y02E10/721
摘要： The mounting assembly of a rotary wing aircraft is formed to include a ceal headpiece which operates to support the rotor blades of the aircraft, which blades are mounted to extend radially outwardly from the central headpiece. The headpiece includes rotor mounting supports having a bifurcated configuration consisting of two arms each having a flat, generally planar shape which extend at a right angle relative to the plane of the rotor. The headpiece may be formed of a pair of generally congruent plate members with an intermediate spacer member located therebetween, with the plate members and the spacer member being integrally joined together in a unitary structure made of composite fiber material.
摘要翻译： 旋转翼飞行器的安装组件形成为包括操作以支撑飞行器的转子叶片的中心头部，该叶片安装成从中心头部径向向外延伸。 头盔包括转子安装支架，其具有由两个臂组成的分叉构造，每个臂具有平坦的大致平面形状，其相对于转子的平面成直角地延伸。 头盔可以由一对大体上一致的板构件形成，中间间隔构件位于它们之间，其中板构件和间隔构件以由复合纤维材料制成的整体结构整体连接在一起。
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