WO2014026574A1 - Flight control device for double-spiral saucer-shaped aircraft - Google Patents
Flight control device for double-spiral saucer-shaped aircraft Download PDFInfo
- Publication number
- WO2014026574A1 WO2014026574A1 PCT/CN2013/081260 CN2013081260W WO2014026574A1 WO 2014026574 A1 WO2014026574 A1 WO 2014026574A1 CN 2013081260 W CN2013081260 W CN 2013081260W WO 2014026574 A1 WO2014026574 A1 WO 2014026574A1
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- steering
- flying
- blade
- wheel
- frame
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
Definitions
- the present invention relates to a control device for an aircraft, and more particularly to a flight control device for a double-helical disk-shaped aircraft. Background technique
- the invention provides a flight control device for a double-helical disk-shaped aircraft, which has a simple structure, stable performance and simple use.
- the technical solution adopted by the present invention is to provide a flight control device for a double-helical disk-shaped aircraft for controlling flight and steering of a double-helical disk-shaped aircraft.
- the control device is composed of a steering operating system, a flight operating system and a driving mechanism disposed under the double spiral disk provided in the cockpit of the aircraft, and is characterized by:
- the driving mechanism includes a cross-shaped side frame disposed under the spiral disk of the fuselage, the cross-shaped side frame is mounted with a set of flying blades at a front and a rear portions thereof in a symmetrical manner and a set of steerings are respectively arranged on the left and right sides thereof.
- Wind blades are mounted with a set of flying blades at a front and a rear portions thereof in a symmetrical manner and a set of steerings are respectively arranged on the left and right sides thereof.
- the steering vane includes a steering main vane and a multi-turn steering sub-window, the steering vane and the cross-shaped side frame forming a steering air hole, the steering main vane and the steering wind
- the central shaft of the hole is connected, and the upper and lower ends of the main fan and the steering sub-blade are rotatably connected by a connecting line, and the steering vane steering wheel is mounted on the central shaft of the steering air hole;
- the flying blade and the cross-shaped side frame constitute a flying air hole, and the central axis driving wheel is mounted on the central axis of the flying air hole, and the flying flying blade is mounted on the flying blade shaft on both sides of the central axis of the flying air hole.
- a driven wheel wherein a flying blade shaft driving wheel matched with the center shaft driving wheel is mounted on a flying blade shaft on the right side; a flying blade is mounted on a flying blade shaft on both sides of the central axis of the flying air hole, and the flying
- the central axis of the air hole separates the flying blades from the left and right parts, and the upper and lower ends of the blades in each part are rotatably connected by a connecting line;
- the steering operating system includes a steering steering wheel, a steering bevel gear, a cable pulley, and a steering wheel.
- the steering steering wheel is connected with a connecting rod.
- the connecting rod end is mounted with a steering wheel, and the steering wheel is driven by a matching bevel gear. Pulling the wire wheel, the pulling wheel is connected with the steering vane steering wheel cable;
- the flight operating system includes a flight balance operation lever, an operation lever frame, a pull wire, and a flying blade steering wheel.
- the lower end of the operation lever frame is fixed with an isosceles triangular frame, and the two corners of the isosceles triangular frame are two spheres.
- the ball is provided with a groove for placing the wire puller
- the operation bar frame is a concave groove
- the concave groove is provided at both ends with a groove for receiving two balls on the fixed isosceles triangle frame
- the isosceles triangular frame is mounted on the operating rod frame by a lever return spring, one end of the pulling wire is fixed on the ball groove by the wire pulling head, and the other end is connected with the flying steering wheel side, and the flying blade turning wheel is another
- a return spring is connected to one side, and the flying vane steering wheel is mounted on the central axis of the flying air hole to drive the central shaft driving wheel mounted on the central axis of the flying air hole.
- the flight control device for the double-helical disk-shaped aircraft further includes eight oblique-pull positioning frames, one end of the diagonal-pull positioning frame is fixedly connected with the body, and the other end is fixedly connected with the frame of the cross-side frame;
- a wind tunnel central shaft protection connecting frame is mounted on the central shaft of the air hole; and the number of the turning blades is an odd number.
- the flight control device for the double spiral disk shaped aircraft of the present invention has a simple structure, The performance is stable, the operator can quickly familiarize with the relevant operations, and the maintenance is convenient and fast, and the cost is low.
- Figure 1 is a schematic view showing the structure of a flight control device for a double-helical disk-shaped aircraft according to the present invention.
- Figure 2 is a schematic view showing the structure of a cross-shaped side frame in the flight control device shown in Figure 1.
- Figure 3 is a plan view of the steering vane in the flight control device of Figure 1.
- Figure 4 is a front elevational view of the steering vane of Figure 2;
- Figure 5 is a plan view of a flying blade in the flight control device of Figure 1.
- Figure 6 is a front elevational view of the flying blade shown in Figure 5.
- Figure 7 is a schematic illustration of the steering operating system in the flight control device of Figure 1.
- Figure 8 is a schematic cross-sectional view of the steering operating system taken along line A-A of Figure 7.
- Figure 9 is a schematic illustration of a flight operating system in the flight control device of Figure 1.
- Figure 10 is a cross-sectional view along line A-A of the schematic diagram of the flight operating system shown in Figure 9.
- Figure 11 is a schematic view showing the installation of the steering vane and the steering operating system in the flight control device shown in Figure 1.
- Figure 12 is a front elevational view of the flying blade steering wheel of the flight control device of Figure 1.
- Figure 13 is a top plan view of the flying blade steering wheel of Figure 12; detailed description
- a flight control device for a double-helical disk-shaped aircraft consists mainly of a steering operating system, a flight operating system, and a drive mechanism disposed below the double-screw disk in the cockpit of the aircraft.
- the driving mechanism comprises a cross-shaped side frame 1 disposed under the spiral disk of the fuselage, and a set of flying blades 2 are symmetrically mounted on the cross-shaped side frame 1; the cross-shaped side frame 1 is symmetrically mounted on the left and right sides. Turn to the blade 3.
- the steering vane 3 includes a steering main vane 31 and a multi-turn steering sub-window 32. Steering wind The leaf 3 and the cross-shaped side frame 1 therein constitute a steering air hole. Further, the steering main blade 31 is connected to the steering air hole center shaft 39, and is rotatably connected to the upper and lower ends of the steering sub-blade 32 by a connecting wire. A steering vane steering wheel 38 is mounted on the steering hole center shaft 39.
- the flying blade 2 and the cruciform side frame 1 therein constitute a flying air hole.
- a central axle drive wheel 291 is mounted on the flight vent central axis 29, and a flying flight vane driven wheel 281 is mounted on the flight vane shaft 28 on both sides of the flight vent central axis 29, wherein the right side of the flying wind
- a flying blade spindle drive wheel 282 that cooperates with a center axle drive wheel 291 is mounted on the blade shaft 28.
- flight blades 2 are mounted on the flight vane shaft 28 on either side of the flight vent central axis 29.
- the flying air hole central axis 29 divides the flying blade 2 into two parts, and the upper and lower ends of the blade in each part are rotatably connected by a connecting line.
- the flight control apparatus further includes a steering operating system including a steering steering wheel 41, a directional bevel gear 42, a cable pulley 43, and a steering wheel 44, wherein the steering wheel 41 is coupled to a connecting rod 46, the connecting rod A directional wheel 44 is mounted at the end of the 46.
- the directional wheel 44 drives the cable pulley 43 to move by the matching bevel gear 42.
- the cable pulley 43 is connected to the steering blade steering wheel 38.
- the flight operating system further includes a flight balance operating lever 5, an operating lever frame 51, a pull wire 52, and a flying blade steering wheel, wherein the lower end of the operating lever frame 51 is fixed with an isosceles triangular frame 511, the isosceles triangle
- the two bottom corners of the frame are two spheres 512, and the spheres 512 are provided with grooves for placing the wire ends.
- the operation lever frame 51 is a concave groove, and both ends of the concave groove are provided with grooves for receiving two balls on the fixed isosceles triangular frame.
- the isosceles triangular frame 511 is mounted on the operating lever frame 51 via a lever return spring 53.
- One end of the pull wire 52 is fixed to the spherical groove by the wire puller, and the other end is connected to the side of the flying steering wheel.
- a return spring 54 is coupled to the other side of the flying vane steering wheel 55.
- the flying vane steering wheel 55 is mounted on the flight vent central axis 29 to drive the central axle drive wheel 291 mounted on the flight vent central axis.
- the flight operating system according to the present invention further includes eight diagonally pulled positioning frames 6, One end of the diagonal pull positioning frame 6 is fixedly connected with the body 7, and the other end is fixedly connected with the frame of the cross frame.
- a wind tunnel central shaft protection connecting bracket is mounted on the central shaft of the wind hole.
- the number of steering blades inside the steering hole is an odd number.
- the steering wheel 41 When in use, turn the steering wheel 41 clockwise. Since the steering wheel 41 and the steering wheel 44 are coaxially connected, the steering wheel 44 rotates simultaneously with the steering wheel 41, and engages the driving direction of the bevel gear 42 while rotating clockwise. Further, since the direction bevel gear 42 and the cable pulley 43 are also coaxially connected, the direction bevel gear 42 also drives the wire pulley 43 to rotate clockwise.
- the pull pulley 43 is connected to the steering vane steering wheel 38 via a pull wire, so that the steering vane steering wheel 38 is also rotated in a clockwise direction.
- the steering vane steering wheel 38 is coaxially coupled to the main steering vane 31, and the main vane 31 is turned clockwise.
- the steering main vane 31 is rotatably coupled to the upper and lower ends of the steering sub-blade 32, so that the steering sub-blade 32 also collapses clockwise with the main vane 31. Then, the wind of the spiral disk is blown counterclockwise by the steering blade, and the reaction force pushes the body to rotate clockwise to the right, that is, to the right, and vice versa. Pushing the steering wheel 41 forward, the steering blades of the two steering vents simultaneously fall forward, and the wind of the spiral disk is blown back through the blades, and the reaction force pushes the aircraft to move horizontally forward.
- the flight blade steered wheel 55 drives the coaxially connected central axle driving wheel 291 to move, the central axle driving wheel 291 drives the flying blade spindle driving wheel 282 that cooperates with the right side, and the flying blade spindle driving wheel 282 drives the The coaxially mounted flight vane driven wheel 281 moves, and the flying vane driven wheel 281 drives the other side of the flying vane driven wheel 281 to move. As a result, the flying blades on either side of the flight center axis 29 will fall toward each other.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
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Abstract
A flight control device for a double-spiral saucer-shaped aircraft, for controlling the flight and steering of the double-spiral saucer-shaped aircraft; the device comprises a steering operation system and a flight operation system disposed in the cockpit of the aircraft, and a driving mechanism disposed under the double-spiral saucer. The device has a simple structure and stable performance, enabling an operator to quickly get familiarized with relevant operations; furthermore the device allows convenient and quick maintenance and is low in cost.
Description
一种用于双螺旋盘碟形飞行器的飞行控制装置 技术领域 Flight control device for double spiral disk shaped aircraft
本发明涉及一种用于飞行器的控制装置,特别是涉及一种用于 双螺旋盘碟形飞行器的飞行控制装置。 背景技术 The present invention relates to a control device for an aircraft, and more particularly to a flight control device for a double-helical disk-shaped aircraft. Background technique
在航空飞行领域中,双螺旋盘碟形飞行器并不多见。 由于双螺 旋盘碟形飞行器不同于普通飞行器, 所以其转向、 飞行控制也有 异于普通飞行器, 需要不断调整飞行器各方向的平衡才能保证碟 形飞行器的正常运作, 稍有不慎就可能出现飞行事故。 因此, 提 供一种稳定、 简单的用于双螺旋碟形飞行器的飞行控制装置是非 常重要的。 发明内容 In the field of aviation flight, double-helical disc-shaped aircraft is rare. Since the double-helical disc-shaped aircraft is different from the ordinary aircraft, its steering and flight control are different from those of ordinary aircraft. It is necessary to constantly adjust the balance of the aircraft in all directions to ensure the normal operation of the dish. A slight accident may result in a flight accident. . Therefore, it is very important to provide a stable and simple flight control device for a double-helical dish. Summary of the invention
本发明提供了一种用于双螺旋盘碟形飞行器的飞行控制装置, 该控制装置结构简单, 性能稳定, 使用简便。 The invention provides a flight control device for a double-helical disk-shaped aircraft, which has a simple structure, stable performance and simple use.
为解决上述问题,本发明所采取的技术方案是: 提供一种用于 双螺旋盘碟形飞行器的飞行控制装置, 以用于控制双螺旋盘碟形 飞行器的飞行和转向。 所述控制装置由设在飞行器驾驶舱内的转 向操作系统、 飞行操作系统和设在双螺旋盘下方的驱动机构组成, 其特征是: In order to solve the above problems, the technical solution adopted by the present invention is to provide a flight control device for a double-helical disk-shaped aircraft for controlling flight and steering of a double-helical disk-shaped aircraft. The control device is composed of a steering operating system, a flight operating system and a driving mechanism disposed under the double spiral disk provided in the cockpit of the aircraft, and is characterized by:
所述驱动机构包括一个设置在机身下螺旋盘下方的十字形边 架, 该十字形边架上以对称方式在其前后部各安装有一组飞行风 叶并在其左右侧各安装有一组转向风叶; The driving mechanism includes a cross-shaped side frame disposed under the spiral disk of the fuselage, the cross-shaped side frame is mounted with a set of flying blades at a front and a rear portions thereof in a symmetrical manner and a set of steerings are respectively arranged on the left and right sides thereof. Wind blade
所述转向风叶包括转向主风叶和多才 转向副风叶,所述转向风 叶与所在的十字形边架构成转向风孔, 所述转向主风叶与转向风
孔中心轴连接, 转向主风叶与转向副风叶的上下两端通过连接线 可旋转连接, 所述转向风孔中心轴上安装有转向风叶转向轮; The steering vane includes a steering main vane and a multi-turn steering sub-window, the steering vane and the cross-shaped side frame forming a steering air hole, the steering main vane and the steering wind The central shaft of the hole is connected, and the upper and lower ends of the main fan and the steering sub-blade are rotatably connected by a connecting line, and the steering vane steering wheel is mounted on the central shaft of the steering air hole;
所述飞行风叶与所在的十字形边架构成飞行风孔,飞行风孔中 心轴上安装有中心轴主动轮, 飞行风孔中心轴两侧的飞行风叶轴 上安装相互配合的飞行风叶从动轮, 其中右侧的飞行风叶轴上安 装有与所述中心轴主动轮配合的飞行风叶轴主动轮; 飞行风孔中 心轴两侧的飞行风叶轴上安装有飞行风叶, 飞行风孔中心轴将飞 行风叶分出左右两部分, 每部分中的风叶上下两端通过连接线可 旋转连接; The flying blade and the cross-shaped side frame constitute a flying air hole, and the central axis driving wheel is mounted on the central axis of the flying air hole, and the flying flying blade is mounted on the flying blade shaft on both sides of the central axis of the flying air hole. a driven wheel, wherein a flying blade shaft driving wheel matched with the center shaft driving wheel is mounted on a flying blade shaft on the right side; a flying blade is mounted on a flying blade shaft on both sides of the central axis of the flying air hole, and the flying The central axis of the air hole separates the flying blades from the left and right parts, and the upper and lower ends of the blades in each part are rotatably connected by a connecting line;
所述转向操作系统包括转向方向盘、 方向伞齿轮、 拉线轮、 方 向轮, 所述转向方向盘连接有一个连接杆, 该连接杆末端安装有 方向轮, 该方向轮通过与之配合的方向伞齿轮带动拉线轮运动, 所述拉线轮与转向风叶转向轮拉线连接; The steering operating system includes a steering steering wheel, a steering bevel gear, a cable pulley, and a steering wheel. The steering steering wheel is connected with a connecting rod. The connecting rod end is mounted with a steering wheel, and the steering wheel is driven by a matching bevel gear. Pulling the wire wheel, the pulling wheel is connected with the steering vane steering wheel cable;
所述飞行操作系统包括飞行平衡操作杆、操作杆架、 拉线、 飞 行风叶转向轮, 所述操作杆架下端固定有一个等腰三角形框架, 所述等腰三角形框架两底角为两个球体, 所述球体上设有用于放 置拉线头的凹槽, 所述操作杆架为一凹形槽, 该凹形槽两端设有 用于容纳固定等腰三角形框架上两球体的凹槽, 所述等腰三角形 框架通过一个操作杆回位弹簧安装在操作杆架上, 所述拉线一端 通过拉线头固定在球体凹槽上, 另一端与飞行转向轮一侧连接, 所述飞行风叶转向轮另一侧连接有复位弹簧, 飞行风叶转向轮安 装在飞行风孔中心轴上带动安装在飞行风孔中心轴上的中心轴主 动轮运动。 The flight operating system includes a flight balance operation lever, an operation lever frame, a pull wire, and a flying blade steering wheel. The lower end of the operation lever frame is fixed with an isosceles triangular frame, and the two corners of the isosceles triangular frame are two spheres. The ball is provided with a groove for placing the wire puller, the operation bar frame is a concave groove, and the concave groove is provided at both ends with a groove for receiving two balls on the fixed isosceles triangle frame, The isosceles triangular frame is mounted on the operating rod frame by a lever return spring, one end of the pulling wire is fixed on the ball groove by the wire pulling head, and the other end is connected with the flying steering wheel side, and the flying blade turning wheel is another A return spring is connected to one side, and the flying vane steering wheel is mounted on the central axis of the flying air hole to drive the central shaft driving wheel mounted on the central axis of the flying air hole.
此外,所述的用于双螺旋盘碟形飞行器的飞行控制装置还包括 八条斜拉定位架, 所述斜拉定位架的一端与机身固定连接, 另一 端与十字边架的边框固定连接; 所述风孔中心轴上安装有风孔中 心轴保护连接架; 而且转向风叶的个数为奇数。 In addition, the flight control device for the double-helical disk-shaped aircraft further includes eight oblique-pull positioning frames, one end of the diagonal-pull positioning frame is fixedly connected with the body, and the other end is fixedly connected with the frame of the cross-side frame; A wind tunnel central shaft protection connecting frame is mounted on the central shaft of the air hole; and the number of the turning blades is an odd number.
本发明的用于双螺旋盘碟形飞行器的飞行控制装置结构简单、
性能稳定、 操作人员可以很快的熟悉相关操作, 并且维护方便快 捷、 费用低廉。 附图说明 The flight control device for the double spiral disk shaped aircraft of the present invention has a simple structure, The performance is stable, the operator can quickly familiarize with the relevant operations, and the maintenance is convenient and fast, and the cost is low. DRAWINGS
图 1 是根据本发明的用于双螺旋盘碟形飞行器的飞行控制装 置的结构示意图。 BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a schematic view showing the structure of a flight control device for a double-helical disk-shaped aircraft according to the present invention.
图 2是图 1所示飞行控制装置中的十字形边架的结构示意图。 图 3是图 1所示飞行控制装置中的转向风叶的俯视图。 Figure 2 is a schematic view showing the structure of a cross-shaped side frame in the flight control device shown in Figure 1. Figure 3 is a plan view of the steering vane in the flight control device of Figure 1.
图 4是图 2所示转向风叶的主视图。 Figure 4 is a front elevational view of the steering vane of Figure 2;
图 5是图 1所示飞行控制装置中的飞行风叶的俯视图。 Figure 5 is a plan view of a flying blade in the flight control device of Figure 1.
图 6是图 5所示飞行风叶的主视图。 Figure 6 is a front elevational view of the flying blade shown in Figure 5.
图 7是图 1所示飞行控制装置中的转向操作系统的示意图。 图 8是沿图 7中的 A-A线的转向操作系统的示意剖视图。 图 9是图 1所示飞行控制装置中的飞行操作系统的示意图。 图 10是图 9所示飞行操作系统示意图的 A-A剖视图。 Figure 7 is a schematic illustration of the steering operating system in the flight control device of Figure 1. Figure 8 is a schematic cross-sectional view of the steering operating system taken along line A-A of Figure 7. Figure 9 is a schematic illustration of a flight operating system in the flight control device of Figure 1. Figure 10 is a cross-sectional view along line A-A of the schematic diagram of the flight operating system shown in Figure 9.
图 11是图 1所示飞行控制装置中的转向风叶与转向操作系统 的安装示意图。 Figure 11 is a schematic view showing the installation of the steering vane and the steering operating system in the flight control device shown in Figure 1.
图 12是图 1所示飞行控制装置中的飞行风叶转向轮的主视图。 图 13是图 12所示飞行风叶转向轮的俯视图。 具体实施方式 Figure 12 is a front elevational view of the flying blade steering wheel of the flight control device of Figure 1. Figure 13 is a top plan view of the flying blade steering wheel of Figure 12; detailed description
如图 1-13所示, 一种用于双螺旋盘碟形飞行器的飞行控制装 置主要由设在飞行器驾驶舱内的转向操作系统、 飞行操作系统和 设在双螺旋盘下方的驱动机构组成, 其中, 驱动机构包括一个设 置在机身下螺旋盘下方的十字形边架 1,十字形边架 1上前后各对 称安装有一组飞行风叶 2;十字形边架 1上左右各对称安装有一组 转向风叶 3。 As shown in Figure 1-13, a flight control device for a double-helical disk-shaped aircraft consists mainly of a steering operating system, a flight operating system, and a drive mechanism disposed below the double-screw disk in the cockpit of the aircraft. Wherein, the driving mechanism comprises a cross-shaped side frame 1 disposed under the spiral disk of the fuselage, and a set of flying blades 2 are symmetrically mounted on the cross-shaped side frame 1; the cross-shaped side frame 1 is symmetrically mounted on the left and right sides. Turn to the blade 3.
转向风叶 3包括转向主风叶 31和多才 转向副风叶 32。转向风
叶 3与所在的十字形边架 1构成转向风孔。 另外, 转向主风叶 31 与转向风孔中心轴 39连接, 并且与转向副风叶 32的上下两端通 过连接线可旋转连接。 转向风孔中心轴 39上安装有转向风叶转向 轮 38。 The steering vane 3 includes a steering main vane 31 and a multi-turn steering sub-window 32. Steering wind The leaf 3 and the cross-shaped side frame 1 therein constitute a steering air hole. Further, the steering main blade 31 is connected to the steering air hole center shaft 39, and is rotatably connected to the upper and lower ends of the steering sub-blade 32 by a connecting wire. A steering vane steering wheel 38 is mounted on the steering hole center shaft 39.
飞行风叶 2与所在的十字形边架 1构成飞行风孔。飞行风孔中 心轴 29 上安装有中心轴主动轮 291 , 而且该飞行风孔中心轴 29 两侧的飞行风叶轴 28上安装有相互配合的飞行风叶从动轮 281 , 其中右侧的飞行风叶轴 28上安装有与中心轴主动轮 291配合的飞 行风叶轴主动轮 282。 此外, 飞行风孔中心轴 29两侧的飞行风叶 轴 28上安装有飞行风叶 2。飞行风孔中心轴 29将飞行风叶 2分出 左右两部分, 每部分中的风叶上下两端通过连接线可旋转连接。 The flying blade 2 and the cruciform side frame 1 therein constitute a flying air hole. A central axle drive wheel 291 is mounted on the flight vent central axis 29, and a flying flight vane driven wheel 281 is mounted on the flight vane shaft 28 on both sides of the flight vent central axis 29, wherein the right side of the flying wind A flying blade spindle drive wheel 282 that cooperates with a center axle drive wheel 291 is mounted on the blade shaft 28. In addition, flight blades 2 are mounted on the flight vane shaft 28 on either side of the flight vent central axis 29. The flying air hole central axis 29 divides the flying blade 2 into two parts, and the upper and lower ends of the blade in each part are rotatably connected by a connecting line.
根据本发明的飞行控制装置还包括一个转向操作系统,该转向 操作系统包括转向方向盘 41、 方向伞齿轮 42、 拉线轮 43、 方向轮 44, 其中, 方向盘 41连接有一个连接杆 46, 该连接杆 46的末端 安装有方向轮 44, 方向轮 44通过与之配合的方向伞齿轮 42带动 拉线轮 43运动; 拉线轮 43与转向风叶转向轮 38拉线连接。 The flight control apparatus according to the present invention further includes a steering operating system including a steering steering wheel 41, a directional bevel gear 42, a cable pulley 43, and a steering wheel 44, wherein the steering wheel 41 is coupled to a connecting rod 46, the connecting rod A directional wheel 44 is mounted at the end of the 46. The directional wheel 44 drives the cable pulley 43 to move by the matching bevel gear 42. The cable pulley 43 is connected to the steering blade steering wheel 38.
根据本发明的飞行操作系统进一步包括飞行平衡操作杆 5、操 作杆架 51、 拉线 52、 飞行风叶转向轮, 其中, 操作杆架 51 的下 端固定有一个等腰三角形框架 511,该等腰三角形框架的两底角为 两个球体 512, 而且所述的球体 512上设有用于放置拉线头的凹 槽。 所述的操作杆架 51为一凹形槽, 凹形槽的两端设有用于容纳 固定等腰三角形框架上的两球体的凹槽。 等腰三角形框架 511 通 过一个操作杆回位弹簧 53安装在操作杆架 51上。 拉线 52的一端 通过拉线头固定在球体凹槽上, 另一端与飞行转向轮一侧连接。 所述的飞行风叶转向轮 55的另一侧连接有复位弹簧 54。飞行风叶 转向轮 55安装在飞行风孔中心轴 29上, 带动安装在飞行风孔中 心轴上的中心轴主动轮 291运动。 The flight operating system according to the present invention further includes a flight balance operating lever 5, an operating lever frame 51, a pull wire 52, and a flying blade steering wheel, wherein the lower end of the operating lever frame 51 is fixed with an isosceles triangular frame 511, the isosceles triangle The two bottom corners of the frame are two spheres 512, and the spheres 512 are provided with grooves for placing the wire ends. The operation lever frame 51 is a concave groove, and both ends of the concave groove are provided with grooves for receiving two balls on the fixed isosceles triangular frame. The isosceles triangular frame 511 is mounted on the operating lever frame 51 via a lever return spring 53. One end of the pull wire 52 is fixed to the spherical groove by the wire puller, and the other end is connected to the side of the flying steering wheel. A return spring 54 is coupled to the other side of the flying vane steering wheel 55. The flying vane steering wheel 55 is mounted on the flight vent central axis 29 to drive the central axle drive wheel 291 mounted on the flight vent central axis.
根据本发明的飞行操作系统进一步还包括八条斜拉定位架 6,
该斜拉定位架 6的一端与机身 7 固定连接, 另一端与十字边架的 边框固定连接。 所述的风孔中心轴上安装有风孔中心轴保护连接 架。 另外, 转向风孔内部的转向风叶个数为奇数。 The flight operating system according to the present invention further includes eight diagonally pulled positioning frames 6, One end of the diagonal pull positioning frame 6 is fixedly connected with the body 7, and the other end is fixedly connected with the frame of the cross frame. A wind tunnel central shaft protection connecting bracket is mounted on the central shaft of the wind hole. In addition, the number of steering blades inside the steering hole is an odd number.
使用时, 按顺时针方向转动方向盘 41。 由于方向盘 41与方向 轮 44属于同轴连接, 方向轮 44会随方向盘 41同时转动, 并啮合 带动方向伞齿轮 42同时做顺时针方向转动。又由于方向伞齿轮 42 与拉线轮 43也属同轴连接, 方向伞齿轮 42也带动拉线轮 43同时 做顺时针方向转动。 拉线轮 43通过拉线与转向风叶转向轮 38连 接, 所以带动转向风叶转向轮 38也做顺时针方向旋转。 转向风叶 转向轮 38与转向主风叶 31同轴连接, 转向主风叶 31向顺时针方 向倒伏。 转向主风叶 31与转向副风叶 32的上下两端可旋转地连 接, 因此转向副风叶 32也随同转向主风叶 31向顺时针方向倒伏。 于是, 螺旋盘的风力通过转向风叶向逆时针方向吹去, 其反作用 力推动机身向右顺时针方向旋转即向右旋转, 反之则向左旋转。 向前推动方向盘 41, 两转向风孔的转向风叶同时向前倒伏, 螺旋 盘的风力通过风叶向后吹去, 其反作用力推动飞行器向前做水平 方向移动。 When in use, turn the steering wheel 41 clockwise. Since the steering wheel 41 and the steering wheel 44 are coaxially connected, the steering wheel 44 rotates simultaneously with the steering wheel 41, and engages the driving direction of the bevel gear 42 while rotating clockwise. Further, since the direction bevel gear 42 and the cable pulley 43 are also coaxially connected, the direction bevel gear 42 also drives the wire pulley 43 to rotate clockwise. The pull pulley 43 is connected to the steering vane steering wheel 38 via a pull wire, so that the steering vane steering wheel 38 is also rotated in a clockwise direction. The steering vane steering wheel 38 is coaxially coupled to the main steering vane 31, and the main vane 31 is turned clockwise. The steering main vane 31 is rotatably coupled to the upper and lower ends of the steering sub-blade 32, so that the steering sub-blade 32 also collapses clockwise with the main vane 31. Then, the wind of the spiral disk is blown counterclockwise by the steering blade, and the reaction force pushes the body to rotate clockwise to the right, that is, to the right, and vice versa. Pushing the steering wheel 41 forward, the steering blades of the two steering vents simultaneously fall forward, and the wind of the spiral disk is blown back through the blades, and the reaction force pushes the aircraft to move horizontally forward.
在向前推动飞行平衡操纵杆 5时,由于飞行平衡操纵杆 5末端 的等腰三角形框架上 511的球体 512与飞行风叶转向轮 55通过拉 线连接, 所以飞行风叶转向轮 55也进行运动。 因此, 飞行风叶转 向轮 55带动同轴连接的中心轴主动轮 291运动,中心轴主动轮 291 带动与右侧之配合的飞行风叶轴主动轮 282运动, 飞行风叶轴主 动轮 282带动其同轴安装的飞行风叶从动轮 281运动, 飞行风叶 从动轮 281 带动与之配合的另一侧的飞行风叶从动轮 281运动。 由此, 飞行中心轴 29两侧的飞行风叶将相向倒伏。 当风叶的倒伏 角度达到 90° 时, 前方的飞行风孔将被完全关闭, 使得飞行器由 此使这部分失去升力, 因此本飞行器就会向前倾斜飞行。 如果想 要停止向前飞行, 只需向后拉动操纵杆 5, 该飞行器就可迅速恢复
平衡。 When the flight balance lever 5 is pushed forward, since the ball 512 on the isosceles triangle frame 511 at the end of the flight balance lever 5 is connected to the flight blade steered wheel 55 by the wire, the flight blade steered wheel 55 also moves. Therefore, the flying blade steering wheel 55 drives the coaxially connected central axle driving wheel 291 to move, the central axle driving wheel 291 drives the flying blade spindle driving wheel 282 that cooperates with the right side, and the flying blade spindle driving wheel 282 drives the The coaxially mounted flight vane driven wheel 281 moves, and the flying vane driven wheel 281 drives the other side of the flying vane driven wheel 281 to move. As a result, the flying blades on either side of the flight center axis 29 will fall toward each other. When the falling angle of the blade reaches 90°, the flying air hole in the front will be completely closed, so that the aircraft will lose the lift in this part, so the aircraft will fly forward. If you want to stop flying forward, simply pull the joystick 5 backwards and the aircraft can be quickly restored. Balance.
在这里需要特别注意的是,在具体的操作过程中, 只要适当关 闭飞行风孔, 使飞行器的倾斜角度达到理想的飞行状态即可。 在 这时, 必须立刻松开操纵杆 5, 操纵杆 5会在操纵杆回位弹簧 53 的作用下迅速回复原位。 同时, 飞行风叶也会在飞行风叶回位弹 簧 54的作用下迅速恢复原位。 只有如此操作, 飞行器才能在理想 的倾斜角度状态下, 长时间稳定的依照理想状态飞行。 否则, 该 飞行器就会不断向前倾斜直至向前翻转。
It is important to note here that during the specific operation, as long as the flight vortex is properly closed, the angle of inclination of the aircraft can be achieved in an ideal flight state. At this time, the joystick 5 must be released immediately, and the joystick 5 will quickly return to its original position under the action of the joystick return spring 53. At the same time, the flying blades will quickly return to their original position under the action of the flying blade return spring 54. Only in this way, the aircraft can fly in an ideal state for a long time under the ideal tilt angle. Otherwise, the aircraft will continue to tilt forward until it flips forward.
Claims
1. 一种用于双螺旋盘碟形飞行器的飞行控制装置, 用于控制 双螺旋盘碟形飞行器的飞行和转向, 所述飞行控制装置包括设在 飞行器驾驶舱内的转向操作系统、 飞行操作系统和设在双螺旋盘 下方的驱动机构, 其特征是: 1. A flight control device for a double-helical disk-shaped aircraft for controlling flight and steering of a double-helical disk-shaped aircraft, the flight control device comprising a steering operating system, flight operation provided in an aircraft cockpit The system and the drive mechanism disposed under the double spiral disk are characterized by:
所述的驱动机构包括一个设置在机身下螺旋盘下方的十字形 边架, 该十字形边架上前后各对称安装有一组飞行风叶, 而且其 左右各对称安装有一组转向风叶; The driving mechanism comprises a cross-shaped side frame disposed under the spiral disk of the fuselage, wherein the cross-shaped side frame is symmetrically mounted with a set of flying blades, and a pair of steering blades are symmetrically mounted on the left and right sides;
所述转向风叶包括转向主风叶和多才 转向副风叶,所述转向风 叶与所在的所述十字形边架构成转向风孔, 所述转向主风叶与转 向风孔中心轴连接, 而且所述转向主风叶与转向副风叶的上下两 端通过连接线可旋转地连接, 所述转向风孔中心轴上安装有转向 风叶转向轮; The steering vane includes a steering main vane and a multi-turn steering sub-window, the steering vane and the cross-shaped side frame forming a steering air hole, and the steering main vane is connected to a central shaft of the steering air hole, The upper and lower ends of the steering main vane and the steering sub-blade are rotatably connected by a connecting line, and the steering vane steering wheel is mounted on the central shaft of the steering air hole;
所述飞行风叶与所在的所述十字形边架构成飞行风孔,飞行风 孔中心轴上安装有中心轴主动轮, 所述飞行风孔中心轴两侧的飞 行风叶轴上安装相互配合的飞行风叶从动轮, 其中右侧的飞行风 叶轴上安装有与中心轴主动轮配合的飞行风叶轴主动轮; 所述飞 行风孔中心轴两侧的飞行风叶轴上安装有飞行风叶, 所述飞行风 孔中心轴将所述飞行风叶分出左右两部分, 每部分中的风叶上下 两端通过连接线可旋转连接; The flying blade and the cruciform side frame forming the flying air hole, the central axis driving wheel is mounted on the central axis of the flying air hole, and the flying wind blade shafts on both sides of the central axis of the flying air hole are fitted with each other. a flying blade driven wheel, wherein a flying blade shaft driving wheel matched with a center shaft driving wheel is mounted on a flying blade shaft on the right side; a flying blade shaft is mounted on both sides of the central axis of the flying air hole a wind blade, the central axis of the flight vent hole separates the flying fan blade from the left and right portions, and the upper and lower ends of the blade in each portion are rotatably connected by a connecting line;
所述的转向操作系统包括转向方向盘、 方向伞齿轮、 拉线轮、 方向轮, 所述的方向盘连接有一个连接杆, 所述连接杆的末端安 述拉线轮运动, 所述拉线轮与所述转向风叶转向轮拉线连接; The steering operating system includes a steering steering wheel, a steering bevel gear, a cable pulley, and a steering wheel. The steering wheel is connected with a connecting rod, and the end of the connecting rod is connected to the cable pulling wheel movement, and the pulling wheel and the steering wheel Wind blade steering wheel cable connection;
所述的飞行操作系统包括飞行平衡操作杆、 操作杆架、 拉线、 飞行风叶转向轮, 所述的操作杆架的下端固定有一个等腰三角形 框架, 所述的等腰三角形框架两底角为两个球体, 所述的球体上
设有用于放置拉线头的凹槽, 所述的操作杆架为一凹形槽, 该凹 形槽的两端设有用于容纳固定等腰三角形框架上两球体的凹槽, 所述的等腰三角形框架通过一个操作杆回位弹簧安装在操作杆架 上, 所述的拉线一端通过拉线头固定在球体凹槽上, 另一端与所 述飞行转向轮一侧连接, 所述的飞行风叶转向轮另一侧连接有复 位弹簧, 所述飞行风叶转向轮安装在所述飞行风孔中心轴上, 带 动安装在所述飞行风孔中心轴上的所述中心轴主动轮运动。 The flight operating system includes a flight balance operating lever, a lever frame, a pull wire, and a flying blade steering wheel. The lower end of the operating lever frame is fixed with an isosceles triangular frame, and the isosceles triangular frame has two bottom corners. For two spheres, on the sphere Providing a groove for placing the wire rod, the operation rod frame is a concave groove, and the two ends of the concave groove are provided with grooves for receiving two balls on the fixed isosceles triangle frame, the isosceles The triangular frame is mounted on the operating rod frame by a lever return spring, one end of the pulling wire is fixed on the ball groove by the wire pulling head, and the other end is connected to one side of the flying steering wheel, and the flying blade is turned A return spring is connected to the other side of the wheel, and the flying vane steering wheel is mounted on the central axis of the flying air hole to drive the central shaft driving wheel mounted on the central axis of the flying air hole.
2. 根据权利要求 1 所述的用于双螺旋盘碟形飞行器的飞行控 制装置, 其特征在于: 还包括八条斜拉定位架, 所述的斜拉定位 架的一端与机身固定连接, 另一端与十字形边架的边框固定连接。 2. The flight control device for a double-helical disk-shaped aircraft according to claim 1, further comprising: eight oblique-pull positioning frames, one end of the diagonal-pull positioning frame is fixedly connected to the body, and One end is fixedly connected to the frame of the cross-shaped side frame.
3. 根据权利要求 1 所述的用于双螺旋盘碟形飞行器的飞行控 制装置, 其特征在于: 所述转向风叶的个数为奇数。 3. The flight control device for a double-helical disk-shaped aircraft according to claim 1, wherein: the number of the steering blades is an odd number.
4. 根据权利要求 1 所述的用于双螺旋盘碟形飞行器的飞行控 制装置, 其特征在于: 所述的风孔中心轴上安装有风孔中心轴保 护连接架。
4. The flight control device for a double-helical disk-shaped aircraft according to claim 1, wherein: the wind tunnel center shaft is mounted with a wind hole central shaft protection connector.
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CN102774497B (en) * | 2012-08-16 | 2014-11-19 | 柴贵景 | Driving device of double-helical panel saucer-shaped aircraft |
CN103057699A (en) * | 2012-12-26 | 2013-04-24 | 徐四旺 | Flying machine with new structure |
CN103171388B (en) * | 2013-03-18 | 2015-04-22 | 中国人民解放军装甲兵工程学院 | Vertical lifting land-air dual-purpose vehicle |
CN108448478B (en) * | 2017-10-27 | 2024-01-05 | 广东电网有限责任公司揭阳供电局 | Automatic adjust focus circuit foreign matter clearing device |
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CN102774497A (en) | 2012-11-14 |
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