CN102553255A

CN102553255A - Deformation gyro helicopter

Info

Publication number: CN102553255A
Application number: CN2012100296533A
Authority: CN
Inventors: 章新江
Original assignee: Individual
Current assignee: Individual
Priority date: 2012-02-01
Filing date: 2012-02-01
Publication date: 2012-07-11

Abstract

The invention relates to a deformation gyro helicopter which comprises a deformation gyro aircraft, a remote controller, a charger and a tray. The deformation gyro aircraft comprises two groups of opposite propellers and a fuselage. The deformation gyro aircraft is structurally characterized in that a motor is directly welded and fixed at the center of a remote control PCB (printed circuit board); a lithium battery is arranged on the lower surface of the remote control PCB; the remote control PCB is coincided with the lithium battery; the motor, the remote control PCB and the lithium battery are all fixed in a plastic enclosure; upper and lower plastic enclosures are fixed by screws; upper and lower butterfly-shaped outer covers are fixed on the upper surface and the lower surface of the plastic enclosure; a motor spindle extends out upwards; the two groups of opposite propellers are respectively fixed on the motor spindle and on the periphery of a center hole on the upper surface of the fuselage; the bottom of the fuselage is of a spherical shape; and the deformation gyro aircraft is arranged on the tray. When the deformation gyro aircraft rotates or rotationally flies, the motor spindle and the propellers on the motor spindle rotate toward the forward direction or toward the opposite direction and simultaneously, the fuselage and the propellers on the fuselage rotate toward the opposite direction or toward the forward direction.

Description

Variant gyro helicopter

Technical field

The core technology of this distortion spiral shell helicopter is: the motor of deformation peg-top aircraft is contained in the center of remote control pcb board and battery all the time; Remote control pcb board and battery be contained in motor around or be contained in motor below; Fuselage will keep certain balance, and fuselage bottom is done globulate.

Background technology

The variant gyro helicopter principle is: the reaction of motor force distance, and the effect of equilibrant force, screw produces the effect to climbing power.

Summary of the invention

This variant gyro helicopter comprises deformation peg-top aircraft, pallet, remote controller and charger, and the deformation peg-top aircraft comprises two groups of opposite helical oars and fuselage, and fuselage is done and further comprised motor, remote control pcb board and rechargeable battery; The structural feature of deformation peg-top aircraft is: motor is contained in the center of remote control pcb board and rechargeable battery, remote control pcb board and rechargeable battery be contained in the following of motor or be contained in motor around, casing motor, remote control pcb board and rechargeable battery completely be contained in the inside; And completely fix; Upper and lower casing is fixed together with screw, and electric machine main shaft upwards stretches out, and fuselage bottom is done globulate; Fuselage will keep certain balance; Two groups of opposite helical oars, a group leader propeller aircraft is fixed on the electric machine main shaft, and the propeller aircraft of one group of weak point is fixed on around the electric machine main shaft hole above the fuselage; Do camber above the deformation peg-top aircraft is placed on, make below and be stabilized on the ground pallet.

The technical characterictic of this variant gyro helicopter is: the deformation peg-top aircraft is in rotation or revolve when flying; Be that electric machine main shaft drives screw on the electric machine main shaft to the positive direction rotation or to opposite spin, the screw that drives on fuselage and the fuselage of motor housing rotates to opposite spin or to positive direction simultaneously.

Description of drawings

Fig. 1 is a deformation peg-top aircraft internal plane accessory sketch map: the positive and negative electrode of 1.1 lithium batteries is welded on the 1.3 remote control pcb boards; 1.2 directly being weldingly fixed on, does on the circular 1.3 remote control pcb boards by motor; 1.5 power switch is weldingly fixed on the 1.3 remote control pcb boards, 1.4 charging sockets are weldingly fixed on the 1.3 remote control pcb boards.

Fig. 2 is with (butterfly is an example) deformation peg-top aircraft and pallet integral planar structural representation: 4 motors directly are weldingly fixed on the center of doing circular 5 remote control pcb boards, load onto 6 lithium batteries below the 5 remote control pcb boards, and 5 remote control pcb boards and 6 lithium batteries coincide together; Make columniform 8 cabinets and completely be contained in the inside to 4 motors, 5 remote control pcb boards and 6 lithium batteries, and completely fix, 8 upper and lower cabinets are fixed together with screw; On 7 butterflies box out in the cover center; Globulate is done in 10 butterfly bottoms of the next cover, on 7 butterflies cover with 10 butterflies under the cover be separately fixed at the top of 8 cabinets and below, 3 electric machine main shafts upwards stretch out; 1 and 2 two group of opposite helical oar; One group leader's rotor 1 screw is fixed on 3 electric machine main shafts, and rotor 2 screws of one group of weak point are fixed on around the centre bore above 9 fuselages, and 9 fuselages will keep certain balance; Do camber above the deformation peg-top aircraft is placed on, make below on 11 plastic pallets on plane.

Fig. 3 is a variant gyro helicopter remote-control transmitting floor map: 3.1 antennas make remote-control transmitting apart from increase, and 3.2 upper and lower switches are controlled the positive and negative rotation of motor, and 3.3 speed-regulating switch are controlled rotating speed of motor, and electricity has been used up with 3.4 chargers and charged.

The specific embodiment

The variant gyro helicopter embodiment is: the deformation peg-top aircraft turns on the power switch; Remote control transmitter sends instruction; Screw fast rotational on the electric machine main shaft produces to climbing power, and the deformation peg-top aircraft weight is alleviated, be contained in simultaneously on the fuselage screw also fast rotational produce to climbing power; Two groups of positive and negative rotations of screw upwards fly up the deformation peg-top aircraft, control the duty of deformation peg-top aircraft with positive and negative switch and speed-regulating switch.

Claims

1. the structural feature of the deformation peg-top aircraft of variant gyro helicopter is: motor is contained in the center of remote control pcb board and rechargeable battery, remote control pcb board and rechargeable battery be contained in the following of motor or be contained in motor around, casing motor, remote control pcb board and rechargeable battery completely be contained in the inside; And completely fix; Upper and lower casing is fixed together with screw, and electric machine main shaft upwards stretches out, and fuselage bottom is done globulate; Fuselage will keep certain balance; Two groups of opposite helical oars, a group leader propeller aircraft is fixed on the electric machine main shaft, and the propeller aircraft of one group of weak point is fixed on around the electric machine main shaft hole above the fuselage.

Claim 2 ' be claim 1 ' the subordinate claim; Its additional technical feature is: the deformation peg-top aircraft of this variant gyro helicopter is in rotation or revolve when flying; Be that electric machine main shaft drives screw on the electric machine main shaft to the positive direction rotation or to opposite spin, the screw that drives on fuselage and the fuselage of motor housing rotates to opposite spin or to positive direction simultaneously.