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    • 1. 发明申请
    • AERODYNAMIC LIFTING-THRUSTING PROPULSION DEVICE
    • WO03086857A8
    • 2004-06-17
    • PCT/RU0300156
    • 2003-04-14
    • OBSCHESTVO S OGRANICHENNOI OTVAKARO ANDREY IGOREVICHDENISOV ANATOLY ALEKSEEVICHZELINSKY ANATOLY MIKHAILOVICHMEDVEDEV MIKHAIL MIKHAILOVICH
    • AKARO ANDREY IGOREVICHDENISOV ANATOLY ALEKSEEVICHZELINSKY ANATOLY MIKHAILOVICHMEDVEDEV MIKHAIL MIKHAILOVICH
    • B64C39/08B64C27/08B64C27/605B64C39/00B64C11/46
    • B64C39/006B64C27/08
    • The inventive aerodynamic lifting-thrusting propulsion device comprises a frame (1) provided with an axis (2), said frame (1) being arranged with respect to the axis (2) in such a way that it is rotatable. At least two aerodynamic surfaces (3) are fixed to a fork joint in such a way that they oscillate synchronously with the rotation of the frame (1), the fork joint being fixed to a rod (5) which is arranged on said frame (1). The axis (2) is connected to each aerodynamic surface (3) by means of a mechanical transmission which enables the aerodynamic surface (3) to rotate synchronously and oppositely with respect to the rotation of the frame and the rod (5). The oscillation of the aerodynamic surfaces (3) is carried out by a mechanical copying device. Each aerodynamic surface can rotate around the axes which are parallel to the axes of the spider of the fork joint and pass through the aerodynamic surface (3). The frame (1) and the aerodynamic surfaces (3) rotate around the axis (2) with the aid of a rotary actuator. Each aerodynamic surface (3) synchronously rotates, by means of the mechanical transmission, in a direction opposite the circular motion thereof at an angle velocity which is equal to the angle velocity of said circular motion, whereby producing the progressive motion of the aerodynamic surfaces and regularly distributing aerodynamic forces therethrough. Each aerodynamic surface (3), synchronously with the rotation thereof, oscillates with the aid of the mechanical copying device, thereby producing a horizontal thrust simultaneously with a lifting force.
    • 本发明的空气动力提升推进装置包括设置有轴线(2)的框架(1),所述框架(1)相对于轴线(2)以可旋转的方式布置。 至少两个空气动力学表面(3)以与框架(1)的旋转同步地摆动的方式固定到叉形接头,叉接头被固定到布置在所述框架上的杆(5) 1)。 轴线(2)通过机械传动装置连接到每个空气动力学表面(3),这使得空气动力学表面(3)能够相对于框架和杆(5)的旋转同步且相反地旋转。 气动表面(3)的振动由机械复印装置进行。 每个空气动力学表面可以围绕平行于叉接头的蜘蛛的轴的轴线旋转并且穿过空气动力学表面(3)。 借助于旋转致动器,框架(1)和空气动力学表面(3)围绕轴线(2)旋转。 每个空气动力学表面(3)通过机械变速器以与圆周运动的角速度相等的角速度与其圆周运动相反的方向同步旋转,从而产生空气动力学表面的逐渐运动, 定期分布空气动力。 每个空气动力学表面(3)与其旋转同步,借助于机械复制装置振荡,从而与提升力同时产生水平推力。
    • 2. 发明申请
    • METHOD FOR PRODUCING A LIFT AND A HORIZONTAL THRUST
    • 用于产生升降和水平扭矩的方法
    • WO03086858A8
    • 2004-03-11
    • PCT/RU0300157
    • 2003-04-14
    • OBSCHESTVO S OGRANICHENNOI OTVAKARO ANDREY IGOREVICHDENISOV ANATOLY ALEKSEEVICHZELINSKY ANATOLY MIKHAILOVICHMEDVEDEV MIKHAIL MIKHAILOVICH
    • AKARO ANDREY IGOREVICHDENISOV ANATOLY ALEKSEEVICHZELINSKY ANATOLY MIKHAILOVICHMEDVEDEV MIKHAIL MIKHAILOVICH
    • B64C39/08B64C27/08B64C27/605B64C39/00B64C11/46
    • B64C27/605B64C27/08B64C39/006
    • The inventive method for producing a lift and a horizontal thrust by aerodynamic surfaces consists in moving the aerodynamic surfaces (1) along a circle (2) around an axis of motion (4). Each aerodynamic surface rotates synchronously with the motion along the circle (2) in a direction opposite thereto about an axis of rotation (6) which is parallel to the axis of motion (4) along the circle (2) at an angular velocity which is equal to the angular velocity of the motion along the circle (2), thereby the progressive motion of the aerodynamic surfaces (1) is produced in such a way that it makes it possible to regularly distribute aerodynamic forces along the aerodynamic surfaces (1). Each aerodynamic surface (1), synchronously with the rotation thereof, oscillates about two mutually perpendicular axes which are disposed on two mutually perpendicular planes, respectively and cut each other along the axis of rotation (6). One plane passes through the axis of motion (4) and the axis of rotation (6), and the other plane is tangent to the circle (2) and parallel to the axis of motion (4), whereby a horizontal thrust being produced.
    • 用于通过空气动力学表面产生升力和水平推力的本发明方法包括围绕运动轴线(4)沿着圆周(2)移动空气动力学表面(1)。 每个空气动力学表面沿与圆周(2)相反的方向与沿着与圆周(2)的平行于运动轴线(4)的旋转轴线(6)的方向相反的方向同步旋转,角速度为 等于沿着圆(2)的运动的角速度,由此产生空气动力学表面(1)的逐渐运动,使得其可以沿着空气动力学表面(1)规则地分布空气动力。 每个空气动力学表面(1)与其旋转同步地围绕两个相互垂直的轴线摆动,它们分别设置在两个相互垂直的平面上并沿着旋转轴线(6)彼此切割。 一个平面通过运动轴线(4)和旋转轴线(6),另一个平面与圆(2)相切并平行于运动轴线(4),从而产生水平推力。
    • 3. 发明专利
    • ДЕРЕВЯННЫЙ СТРОИТЕЛЬНЫЙ ЭЛЕМЕНТ (ВАРИАНТЫ) И ДЕРЕВЯННЫЙ СТРОИТЕЛЬНЫЙ БЛОК
    • RU2761787C1
    • 2021-12-13
    • RU2021114430
    • 2021-05-21
    • MEDVEDEV MIKHAIL VALEREVICH
    • MEDVEDEV MIKHAIL VALEREVICH
    • E04B1/10
    • Группаизобретенийотноситсяк областистроительства. Техническийрезультат: повышениетеплоизоляционныхсвойствдеревянныхстроительныхсооружений, обеспечениебезусадочностивоздвигаемыхстроительныхконструкций, снижениетрудозатратнастроительствои расширениедиапазонавозводимыхстени перегородокпотолщине. Деревянныйстроительныйэлементвыполненв видедоски, обепластовыеповерхностикоторойвыполненыпрофилированнымии содержатпрорезанныеповсейдлинепродольно-ориентированныеопорныевыступыи ответныеимустановочныепазы. Приэтомвыступынапластяхимеюттрапециевиднуюформу, выступыоднойстороныдоскисоответствуютпазамдругойстороныдоски. Выступынапротивоположныхпластяхсмещеныотносительнодругдруганавеличину ½ шагавыступа, высотавыступасоставляет 5 мм, шагвыступовсоставляет 14 мм, уголнаклонабоковойгранитрапециевидноговыступак вертикалисоставляет 37°. Кромкидоскивыполненыс взаимодействующимиэлементамизацепленияв видепаз-выступ. Такжеописанывариантдеревянногостроительногоэлемента, атакжедеревянныйстроительныйблок, включающийнескольковышеописанныхдеревянныхстроительныхэлементов. 3 н. и 3 з.п. ф-лы, 6 ил.