CN205924994U

CN205924994U - Folding wing air -drop aircraft

Info

Publication number: CN205924994U
Application number: CN201620868654.0U
Authority: CN
Inventors: 佘汉桐; 吴子轩; 仇浩然
Original assignee: GUANGZHOU NO5 MIDDLE SCHOOL
Current assignee: GUANGZHOU NO5 MIDDLE SCHOOL
Priority date: 2016-08-11
Filing date: 2016-08-11
Publication date: 2017-02-08
Anticipated expiration: 2026-08-11

Abstract

The utility model relates to a folding wing air -drop aircraft for the aircraft that the input formula was taken off, it discloses the wing adopt foldable articulating on the left and right both sides of organism, install fold -over clasp respectively on the wing on left and right both sides, the organism in the middle of the department install the extension steering wheel, the rotation platform both ends of extending the steering wheel are connected through fold -over clasp on extending connecting rod and left and right both sides wing respectively, the tail end in the organism axis is installed to the motor, and the head end in the organism axis is installed to the battery to make the big and tail end of weight of organism head end, be located the left and right both sides of motor in the bottom of organism tail end and install aslope respectively and slowly fall the board. The utility model has the advantage of reasonable structure, whole light in weight, occupation space are little, and the wing expandes rapidly, and flight is stable.

Description

Folding wings supply dropper aircraft

Technical field

The utility model is related to folding wings supply dropper aircraft, specifically a kind of throws in, by machine tool, the folding taken off in the air Formula aircraft.

Background technology

Have slidingtype to take off in the model of an airplane, hand-throw type takes off, vertical type takes off, hand throwing type takes off etc. the side of taking off Formula, in hand throwing type mode is taken off, the phenomenon such as wing area hour can bring control mode insensitive after take off, if area The air-drop storehouse taking machine tool when big will be done greatly, increased the manufacture difficulty of machine tool, and not open in the motor in a flash thrown in Run into distinguished and admirable greatly when dynamic, the failure direct requirement of taking off of aircraft can be allowed to plunge or directly damage, if adopt wing-folding formula, Can run into that the wind-force that freely falling body produces in air-drop makes wing cannot launch or duration of run is excessive causes directly to plunge, these Phenomenon is all the technological difficulties that hand throwing type aircraft needs overcome.

Utility model content

The purpose of this utility model is to provide folding wings supply dropper aircraft, and it adopts fold design, takes up room little, throws in Wing energy rapid deployment, and lightweight, take off fast, processing ease, flight stability.

Technical solution of the present utility model is the wing in body, empennage, and rudder is put, steering wheel, motor, battery, stretches rudder On the basis of machine, it is characterized in described wing using the collapsible left and right both sides being hinged on body, in the machine on left and right both sides Folding fastener is separately installed with the wing；In the middle of body, stretching, extension steering wheel is installed, the turntable two ends stretching steering wheel lead to respectively Cross extension link to be connected with folding fastener on the wing of left and right both sides；Motor is arranged on the tail end of body axis, and battery is arranged on The head end of body axis, and make body head end weight is big and tail end, be located at motor left and right two in the bottom of body tail end Side is obliquely provided with slow fall plate respectively.

Operation principle of the present utility model is using the design of nose heave tail light layout type, so that aircraft is carried out at once after input Vertical Free falling bodies state, designs two blocks of slow fall plates in tail and the freely falling body time is lengthened, allow wing have enough time exhibition Open, and wing is taken up room using the entirety that fold design reduces aircraft, thus reducing the manufacture difficulty of machine tool, and aircraft Open up as state with the wind on Vertical Free falling bodies state opportunity, using lightweight stretch steering wheel just can rapid deployment wing, do not exist Launch difficult and effectively mitigate body weight, delay the motive force lower stress balance that fall plate drives screw in motor after take off Body initial and end lays particular stress on situation, makes aircraft more energy-conservation and stable in flight.

The utility model has the advantages that rational in infrastructure, overall weight is light, it is little to take up room, and wing launches rapidly, and flight is steady Fixed.

Brief description

Fig. 1 is that the structural representation that takes off thrown in by the utility model composite aircraft；

Fig. 2 is structural representation after wing of the present utility model launches；

Fig. 3 is structural representation after wing-folding of the present utility model.

Specific embodiment

According to Fig. 1, Fig. 2, Fig. 3, the utility model is the handset 2 taken off by machine tool 1 releasing type, in body 3, machine The wing 4, empennage 8, rudder pendulum 7, steering wheel 6, motor 9, battery 8, on the basis of stretching steering wheel 5, the wing 4 being characterized in described adopts folding Stacked is hinged on the left and right both sides of body 3, is separately installed with folding fastener 9 on the wing 4 on left and right both sides；In body 3 Between place stretching, extension steering wheel 5 is installed, the turntable two ends stretching steering wheel 5 are passed through on extension link 11 and left and right both sides wing 4 respectively Folding fastener 9 be connected；Motor 9 is arranged on the tail end of body 3 axis, and battery 8 is arranged on the head end of body 3 axis, and And make body head end weight is big and tail end, be obliquely provided with respectively positioned at the left and right both sides of motor in the bottom of body 3 tail end Slow fall plate 10.

Claims

1. folding wings supply dropper aircraft, it is the handset taken off by machine tool releasing type, and including organism, wing, empennage, rudder is put, Steering wheel, motor, battery, stretch steering wheel, it is characterized in that described wing using the collapsible left and right both sides being hinged on body, It is separately installed with folding fastener on the wing on left and right both sides；In the middle of body, stretching, extension steering wheel is installed, stretches the rotation of steering wheel Platform two ends are connected with folding fastener on the wing of left and right both sides by extension link respectively；Motor is arranged on the tail of body axis End, battery is arranged on the head end of body axis, and make body head end weight is big and tail end, at the bottom position of body tail end In the left and right both sides of motor, slow fall plate is obliquely installed respectively.