WO2016154976A1 - Aéronef - Google Patents

Aéronef Download PDF

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Publication number
WO2016154976A1
WO2016154976A1 PCT/CN2015/075735 CN2015075735W WO2016154976A1 WO 2016154976 A1 WO2016154976 A1 WO 2016154976A1 CN 2015075735 W CN2015075735 W CN 2015075735W WO 2016154976 A1 WO2016154976 A1 WO 2016154976A1
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
stabilizer bar
propeller
disposed
upper casing
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/CN2015/075735
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English (en)
Chinese (zh)
Inventor
尚平
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 PCT/CN2015/075735 priority Critical patent/WO2016154976A1/fr
Publication of WO2016154976A1 publication Critical patent/WO2016154976A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • 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

Definitions

  • the present invention relates to the field of toys and, more particularly, to an aircraft.
  • the technical problem to be solved by the present invention is to provide an aircraft capable of stable flight.
  • an aircraft comprising a main body, a propeller and a driving device for driving the propeller, further comprising a stabilizer bar disposed in a direction of a center of gravity of the aircraft, the stabilizer bar Located at the upper end of the aircraft.
  • the center of gravity of the aircraft is at its structural center position.
  • the main body together with the stabilizer bar has a conical structure as a whole, so that the stabilizer bar is disposed at the center of the aircraft to make the stabilizer bar more effective for the stable flight of the aircraft.
  • the propeller is disposed below the driving device.
  • the main body includes an upper casing and a lower casing
  • the upper casing is provided with a fixing hole for fixing the stabilizer bar
  • the stabilizer bar is provided with a limiting portion that cooperates with the fixing hole.
  • the limiting portion of the stabilizer bar is fixedly fixed with the fixing hole at the center position of the upper casing, and the limiting portion securely fixes the stabilizer bar to the upper casing.
  • a plurality of sensing devices for sensing obstacles are disposed around the lower case.
  • An inductive device for sensing obstacles is provided around the lower casing to facilitate the flight of the aircraft, preventing the aircraft from continuing to fly in the direction of obstacles.
  • the sensing device comprises a first sensing device for sensing a horizontal obstacle and a second sensing device for sensing a vertical obstacle. Prevent the aircraft from flying too low and prevent the aircraft from being too close to the surrounding obstacles while flying.
  • the driving device is disposed in the upper casing; the lower casing surrounds the propeller and is horizontally disposed with the propeller. This setting prevents the propeller from being exposed.
  • the main body is provided with a plurality of evenly spaced air inlets.
  • the propeller rotates downward to the wind, and the main body is provided with an air inlet to ensure that the propeller can rotate normally.
  • the upper casing extends along the fixing hole with an extension for being sleeved on the stabilizer bar.
  • the extension part is sleeved on the stabilizer bar to increase the contact area of the upper case and the stabilizer bar, and the limit effect on the stabilizer bar is better, so that the stabilizer bar is fixed more firmly.
  • the limiting portion is provided with a slot in the axial direction of the stabilizer bar.
  • the limiting portion is provided with a slot in the axial direction of the stabilizer bar, and the side walls on both sides of the slot at the pressing limit portion extend and contract the limiting portion, so that the limiting portion is inserted into the fixing hole of the upper casing and protrudes from the upper casing, so that the upper casing is protruded If the slotted portion is not restricted by the fixing hole, the original shape will be restored, and the fixing hole will be limited, so that the stabilizer bar is firmly fixed; and the installation and disassembly are convenient.
  • the invention is provided with a stabilizer bar for the stable flight of the aircraft in the direction of the center of gravity of the aircraft, so that the stabilizer bar can ensure its stability and balance when the aircraft is flying, so that the flight is safer.
  • FIG. 1 is a schematic exploded view of an aircraft according to an embodiment of the present invention.
  • FIG. 2 is a cross-sectional view of an aircraft in accordance with an embodiment of the present invention.
  • 100 main body; 110, stabilizer bar; 111, slotted; 120, upper case; 121, extension; 130, lower case; 131, air intake hole; 140, driving device; 150, propeller; Inductor; 170, second sensor.
  • An aircraft as shown in FIGS. 1 and 2, includes a main body 100, a propeller 150, and a driving device 140 for driving the propeller 150, and further includes a center of gravity of the aircraft
  • the stabilizer bar 110 On the upper stabilizer bar 110, the stabilizer bar 110 is disposed at the upper end of the aircraft.
  • the stabilizer bar 110 can ensure its stability and balance during flight, making it safer to fly.
  • the main body 100 of the aircraft together with the stabilizer bar 110 as a whole has a cone structure, and its internal weight is uniform, so that the center of gravity of the aircraft is on the center of gravity of the main body; and the aircraft and The center of gravity of the body 100 is in its center direction, so that the stabilizer bar 110 is disposed at the center of the body 100 to better stabilize the stabilizer bar 110 for the aircraft to fly stably.
  • the driving device 140 is disposed in the main body 100.
  • the propeller 150 is disposed below the driving device 140, and the propeller 150 is surrounded by the main body, so that the propeller 140 rotates.
  • the air is discharged downward, and the main body 100 is provided with a plurality of uniformly distributed air inlets 131, thereby ensuring that the propeller 150 can normally enter the air and then rotate normally.
  • the main body includes an upper casing 120 and a lower casing 130.
  • the upper casing 120 is centrally provided with a fixing hole for fixing the stabilizer bar 110, and the stabilizer bar 110 is provided with a limiting portion that cooperates with the fixing hole;
  • the limiting portion of the stabilizer bar 110 is fixedly coupled to the fixing hole at the center of the upper casing 120, and the limiting portion securely fixes the stabilizer bar 110 to the upper casing 120.
  • the limiting portion is provided with a slot 111 axially to the stabilizer bar 110.
  • the limiting portion is provided with a slot 111 in the axial direction of the stabilizer bar, and the two sides of the slot 111 at the pressing limit portion are The side wall makes the limiting portion expand and contract, and the limiting portion is inserted into the fixing hole of the upper casing, and the upper casing is protruded, so that the grooved portion is not restricted by the fixing hole, and the original shape is restored, and then the fixing hole is fixed.
  • the limit is set so that the stabilizer bar is firmly fixed; and it is easy to install and remove.
  • the stabilizer bar can also be fixed in other ways, such as by a snap.
  • the aircraft further includes an sensing device for sensing an obstacle.
  • the sensing device is plural, and includes a first sensing device 160 for sensing an obstacle in a horizontal direction and a second sensing device for sensing an obstacle in a vertical direction.
  • the sensing device 170 prevents the aircraft from flying too low and prevents the aircraft from being too close to the surrounding obstacles during flight.
  • the sensing device is evenly disposed at the bottom of the lower casing 120, and an inductive device is disposed around the lower casing to prevent the aircraft from continuing to fly in the direction of obstacles.
  • the sensing device is infrared sensing.
  • the driving device 140 is disposed in the upper casing 120.
  • the driving device includes a driving motor, a driving gear fixed on an output shaft of the driving motor, a transmission gear meshing with the driving gear, and being fixed at a driven gear on the propeller, the driven gear meshes with the transmission gear, and a battery is fixed in the main body of the aircraft, and the battery is connected with the driving motor to supply power to the driving motor, and the output shaft of the driving motor rotates to drive the driving gear to rotate.
  • the driving gear drives the transmission gear and the driven gear to rotate, thereby rotating the propeller, thereby realizing the flight of the aircraft.
  • the flight of the aircraft is made more stable by the stabilizing action of the stabilizer bar during the flight of the aircraft.
  • the lower casing 130 surrounds the propeller 150 and is disposed horizontally with the propeller 150 such that the propeller is prevented from being exposed.
  • the upper casing 120 extends along the fixing hole with an extending portion 121 for socketing on the stabilizer bar 110.
  • the extending portion 121 is sleeved on the stabilizer bar 110 and is adapted to the stabilizer bar.
  • the extending portion 121 increases the contact area of the upper casing and the stabilizer bar, and the limiting effect on the stabilizer bar 110 is better, so that the stabilizer bar is fixed more firmly.
  • the extending portion 121 is located on the outer surface of the upper portion of the upper casing.
  • the extending portion may also be disposed on the inner surface of the upper casing; however, the driving device is installed inside the upper casing, and the extension portion is disposed inside the upper casing.
  • the space inside the upper shell increases the space of the aircraft, which is not conducive to flight, so that the extension 121 is disposed on the outer surface of the upper portion of the upper casing to conveniently set the height of the extension without affecting the overall arrangement of the aircraft.

Landscapes

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

Abstract

L'invention concerne un aéronef, comprenant un corps principal, une hélice et un appareil d'entraînement configuré pour entraîner l'hélice. L'aéronef comprend en outre une barre stabilisatrice disposée dans une direction de centre de gravité de l'aéronef, la barre stabilisatrice étant disposée au niveau de l'extrémité supérieure de l'aéronef. Dans la présente invention, une barre stabilisatrice configurée pour permettre à l'aéronef de voler de manière stable est disposée dans la direction de centre de gravité de l'aéronef, de telle sorte que la barre stabilisatrice peut assurer la stabilité et l'équilibre de l'aéronef pendant le vol, ce qui permet de rendre le vol plus sûr.
PCT/CN2015/075735 2015-04-01 2015-04-01 Aéronef Ceased WO2016154976A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2015/075735 WO2016154976A1 (fr) 2015-04-01 2015-04-01 Aéronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2015/075735 WO2016154976A1 (fr) 2015-04-01 2015-04-01 Aéronef

Publications (1)

Publication Number Publication Date
WO2016154976A1 true WO2016154976A1 (fr) 2016-10-06

Family

ID=57006532

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2015/075735 Ceased WO2016154976A1 (fr) 2015-04-01 2015-04-01 Aéronef

Country Status (1)

Country Link
WO (1) WO2016154976A1 (fr)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2213553Y (zh) * 1995-03-25 1995-11-29 郑炜煌 遥控飞碟
CN1618501A (zh) * 2003-03-11 2005-05-25 史提夫·戴维斯 自稳定旋转玩具
US20060038061A1 (en) * 2003-10-02 2006-02-23 Blevio Henry L Sr Aerodynamically stable, high-lift, vertical takeoff aircraft
CN101428687A (zh) * 2008-12-12 2009-05-13 吉风旺 一种通用动力飞碟
CN103466095A (zh) * 2013-09-25 2013-12-25 蘧恒江 碟形飞行器

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2213553Y (zh) * 1995-03-25 1995-11-29 郑炜煌 遥控飞碟
CN1618501A (zh) * 2003-03-11 2005-05-25 史提夫·戴维斯 自稳定旋转玩具
US20060038061A1 (en) * 2003-10-02 2006-02-23 Blevio Henry L Sr Aerodynamically stable, high-lift, vertical takeoff aircraft
CN101428687A (zh) * 2008-12-12 2009-05-13 吉风旺 一种通用动力飞碟
CN103466095A (zh) * 2013-09-25 2013-12-25 蘧恒江 碟形飞行器

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