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WO2001008777A1 - Avion telecommande electrique - Google Patents

Avion telecommande electrique Download PDF

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Publication number
WO2001008777A1
WO2001008777A1 PCT/CN2000/000193 CN0000193W WO0108777A1 WO 2001008777 A1 WO2001008777 A1 WO 2001008777A1 CN 0000193 W CN0000193 W CN 0000193W WO 0108777 A1 WO0108777 A1 WO 0108777A1
Authority
WO
WIPO (PCT)
Prior art keywords
rudder
compensation
tail
turning
stabilizer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CN2000/000193
Other languages
English (en)
Chinese (zh)
Inventor
Yu Tian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to AU58012/00A priority Critical patent/AU5801200A/en
Publication of WO2001008777A1 publication Critical patent/WO2001008777A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/12—Adjustable control surfaces or members, e.g. rudders surfaces of different type or function being simultaneously adjusted
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/02—Model aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
    • A63H30/02—Electrical arrangements
    • A63H30/04—Electrical arrangements using wireless transmission

Definitions

  • the invention relates to an aviation model aircraft, in particular to an electric remote-control aircraft. Background technique
  • the tail of a traditional aviation model aircraft generally consists of a stabilizer surface and a control rudder surface.
  • the control rudder surface uses a single structure and is controlled by two servos. Differentiated from the tail, they are generally divided into two categories.
  • the vertical and horizontal tail of this model aircraft are controlled by two steering gears installed in the remote control device in the fuselage.
  • When the aircraft turns In order to prevent the aircraft from entering the spiral, it is necessary to adjust not only the vertical tail, but also the horizontal tail at the same time. This operation is more complicated, and it is easy to make mistakes to make the aircraft enter the spiral, which affects flight. It is not suitable for beginners.
  • Another type is The V-shaped rear wing is controlled by a steering gear, but when the aircraft turns, the control surfaces of the left and right rear fins can only go up and down at the same time, which makes it easy for the airplane to enter the spiral.
  • An object of the present invention is to provide an electric remote-control aircraft which is easy to operate and can keep the aircraft flying smoothly when turning, and is particularly suitable for beginners.
  • An electric remote-control aircraft includes a fuselage, wings, a power unit, a remote control device, and a V-shaped tail, which are characterized in that the left and right tails of the V-shape are respectively provided with turning lift.
  • An automatic compensation mechanism which includes left and right turning rudder surfaces and left and right turning compensation rudder surfaces; a left bracket is provided on the surface of the left turning rudder surface, and a right bracket is provided on the table below the right turning rudder surface; a fork shape
  • One end of the rod is connected to the remote control device through a cable, and the left and right arms at the other end are above and below the left and right tail wings respectively, and are connected to the left and right brackets respectively;
  • the lower surfaces of the right stabilizer surface and the left and right turn rudder surfaces are provided with baffles respectively; the lower surfaces of the left and right turn compensation rudder surfaces are respectively provided with a reset mechanism, and one end of the reset mechanism is fixed on the lower surface of the stabilizer stabilizer surface. The other end is fixed on the lower surface of the turning compensation rudder surface.
  • the reset mechanism is a rubber band.
  • the present invention has obvious advantages, because the tail lift is provided with a turning lift automatic compensation mechanism, and only a steering gear is needed to operate, so it has a simple structure, convenient operation, and does not enter when the aircraft turns Spiral and other advantages.
  • FIG. 1 is a schematic structural diagram of a preferred embodiment of the present invention.
  • FIG. 2 is a schematic side view of the structure of FIG. 1.
  • FIG. 3 is a schematic rear view of FIG. 1.
  • FIG. 4 is an enlarged perspective view of the rear wing of FIG. 1.
  • FIG. 5 is a schematic enlarged perspective view of the tail wing when the embodiment of FIG. 1 makes a left turn.
  • FIG. 6 is a schematic enlarged perspective view of the tail wing when the vehicle turns right in the embodiment in FIG. 1.
  • the present invention includes a fuselage 50, a wing 60, a power unit 70, a remote control device 40, and a V-shaped tail. Since this part is a prior art, it will not be described in detail.
  • the improved structure of the present invention is that the left and right tail wings 10 and 20 constituting the V-shaped body are respectively provided with a turning lift automatic compensation mechanism, and the automatic compensation mechanism includes left and right turning rudder surfaces 11, 21 and left and right turning compensation rudder surfaces 12 22 ⁇
  • the left surface of the left turning rudder surface 11 is provided with a left bracket 13, and the lower surface of the right turning rudder surface 21 is provided with a right bracket 23.
  • a fork-shaped rod 30 is connected to a steering gear in the remote control device through a steel cable.
  • the left arm 31 of the fork-shaped rod 30 is above the left tail wing 10 and is connected to the left bracket 13; the right arm 32 of the fork-shaped rod 30 It is located below the right rear wing 20 and connected to the right bracket 23.
  • One end of the baffle plate 14 is fixed on the lower surface of the stabilizer surface of the left tail wing 10, and the other end extends below the left turn compensation rudder surface 12.
  • baffle plate 15 is fixed on the lower surface of the left turn rudder surface 11, The other end extends below the left turn compensation rudder surface 12; one end of the baffle 25 is fixed on the lower surface of the right tail 20 stabilizer surface, and the other end extends below the right turn compensation rudder surface 22; one end of the baffle 24 is fixed on the right turn On the lower surface of rudder surface .21, the other end extends below right turn compensation rudder surface 22.
  • the left and right turn compensation rudder surfaces 12, 22 are respectively provided with a reset mechanism 16, 26 on the lower surface.
  • the reset mechanism can use a rubber band with better elasticity, one end of which is fixed on the lower surface of the stabilizer's stable surface, and the other end of which is fixed. On the lower surface of the turn-compensated rudder surface.
  • the stabilizer surface of the left tail wing 10 When the electric remote control aircraft of the present invention is flying straight, as shown in FIG. 4, the stabilizer surface of the left tail wing 10, the left turn rudder surface 11 and the right turn compensation rudder surface 12 are all on one plane, and the stability surface of the right tail wing 20, The right turn rudder surface 21 and the right turn compensation rudder surface 22 are also on the same plane.
  • the steel cable When the aircraft turns to the left, as shown in FIG. 5, the steel cable is pushed by the remote control device, the steel cable pushes the fork bar 30, and the fork bar 30 simultaneously pushes the left and right turning rudder surfaces through its two arms to move in opposite directions; right The arm 32 pushes the right turning rudder surface 21 upward through the right bracket 23, and the right turning rudder surface 21 pushes the right turning compensation rudder surface 22 upward at the same time through the baffle 24 fixed thereto; and the left arm 31 pushes the left turning rudder surface 11 through the left bracket 13 Downward, while the left turn compensation rudder surface 12 remains in place due to the baffle plate 14 fixed to the left tail wing 10.
  • the left and right turning rudder surfaces 11, 21 are reset by the two arms and the cable, and the right turning compensation rudder surface is reset by the elastic force of the reset mechanism 26.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

L'invention concerne un avion télécommandé électrique à empennage en V présentant de part et d'autre un mécanisme de compensation automatique de la portance qui comprend une gouverne à droite, une gouverne à gauche, une gouverne de compensation à gauche et une gouverne de compensation à droite, les deux gouvernes de compensation présentant des supports. La paroi de la moitié de la partie gauche de l'empennage, se présentant sous forme de fourche, est reliée au support à droite et la paroi de la moitié de la partie droite de l'empennage, en forme de fourche, est reliée au support à droite, les éléments en forme de fourche étant connectés au dispositif de commande grâce à des câbles en fil d'acier. On prévoit encore des stabilisateurs, l'un placé sur les moitiés gauche et droite de l'empennage et l'autre sur les gouvernes gauche et droite ainsi qu'un mécanisme de repositionnement placé sur les deux gouvernes de compensation.
PCT/CN2000/000193 1999-08-02 2000-07-11 Avion telecommande electrique Ceased WO2001008777A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU58012/00A AU5801200A (en) 1999-08-02 2000-07-11 Electric remote control aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN99239162U CN2384863Y (zh) 1999-08-02 1999-08-02 电动遥控飞机
CN99239162.8 1999-08-02

Publications (1)

Publication Number Publication Date
WO2001008777A1 true WO2001008777A1 (fr) 2001-02-08

Family

ID=5315470

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2000/000193 Ceased WO2001008777A1 (fr) 1999-08-02 2000-07-11 Avion telecommande electrique

Country Status (3)

Country Link
CN (1) CN2384863Y (fr)
AU (1) AU5801200A (fr)
WO (1) WO2001008777A1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1878478A1 (fr) * 2006-07-12 2008-01-16 Tomy Company, Ltd. Jouet-avion
CN103192984A (zh) * 2013-03-19 2013-07-10 北京航空航天大学 一种适用于跨海空两栖无人机的v型尾翼装置
CN103661923A (zh) * 2013-11-28 2014-03-26 江西洪都航空工业集团有限责任公司 一种半隐藏式升降舵摇臂
CN106669178A (zh) * 2015-11-05 2017-05-17 郑华耀 空中悬浮及可编程运动的方法、系统及玩具飞行器

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102490903A (zh) * 2010-03-16 2012-06-13 北京航空航天大学 一种小型多用途无人机
CN106364662A (zh) * 2016-10-19 2017-02-01 吴瑞霞 一种飞机俯仰、侧翻、偏航控制系统

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2055729A (en) * 1979-08-08 1981-03-11 British Aerospace Aircraft
US4381091A (en) * 1979-08-08 1983-04-26 British Aerospace Public Limited Company Control-effect enhancement of tiltable aircraft stabilizing member
DE3934840A1 (de) * 1989-10-19 1991-04-25 Wagener Gmbh Fritz Modellflugzeug mit leitwerkvorrichtung
CN1052084A (zh) * 1990-05-31 1991-06-12 邢麟祥 分动式翼型双垂尾
CN2253239Y (zh) * 1996-04-19 1997-04-30 李晓阳 橡筋动力自由飞仿真飞机模型
CN1169935A (zh) * 1996-07-10 1998-01-14 邢麟祥 分动式翼型双平尾

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2055729A (en) * 1979-08-08 1981-03-11 British Aerospace Aircraft
US4381091A (en) * 1979-08-08 1983-04-26 British Aerospace Public Limited Company Control-effect enhancement of tiltable aircraft stabilizing member
DE3934840A1 (de) * 1989-10-19 1991-04-25 Wagener Gmbh Fritz Modellflugzeug mit leitwerkvorrichtung
CN1052084A (zh) * 1990-05-31 1991-06-12 邢麟祥 分动式翼型双垂尾
CN2253239Y (zh) * 1996-04-19 1997-04-30 李晓阳 橡筋动力自由飞仿真飞机模型
CN1169935A (zh) * 1996-07-10 1998-01-14 邢麟祥 分动式翼型双平尾

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1878478A1 (fr) * 2006-07-12 2008-01-16 Tomy Company, Ltd. Jouet-avion
CN103192984A (zh) * 2013-03-19 2013-07-10 北京航空航天大学 一种适用于跨海空两栖无人机的v型尾翼装置
CN103192984B (zh) * 2013-03-19 2015-01-21 北京航空航天大学 一种适用于跨海空两栖无人机的v型尾翼装置
CN103661923A (zh) * 2013-11-28 2014-03-26 江西洪都航空工业集团有限责任公司 一种半隐藏式升降舵摇臂
CN106669178A (zh) * 2015-11-05 2017-05-17 郑华耀 空中悬浮及可编程运动的方法、系统及玩具飞行器

Also Published As

Publication number Publication date
AU5801200A (en) 2001-02-19
CN2384863Y (zh) 2000-06-28

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