CN2555079Y

CN2555079Y - Balance regulator for toy aircraft

Info

Publication number: CN2555079Y
Application number: CN 02256988
Authority: CN
Inventors: 陈腾
Original assignee: Individual
Current assignee: Individual
Priority date: 2002-10-14
Filing date: 2002-10-14
Publication date: 2003-06-11
Anticipated expiration: 2012-10-14

Abstract

The utility model relates to a balance regulator for a toy aircraft. A control switch can automatically start balancing mechanisms to adjust the balance of the toy aircraft. Being applicable for a balance regulator for various toy aircrafts, the utility model installed on the body of the aircraft has at least two groups of balancing mechanisms, wherein, one is a front-back adjustment balancing mechanism, and the other is a left-right adjustment balancing mechanism. Each balancing mechanism includes at least an electric motor installed on the body of the aircraft and a control switch set. The electric motor is connected with the power source through the control switch set. The balancing mechanisms conduct control through the control switch. The utility model is capable of adjusting the balance condition of the body so as to assure the normal flight of the aircraft.

Description

The balance adjusting device that is used for the toys aircraft

Technical field

The utility model relates to adjusts the adjustment control system that body tilts in the aircraft, for balance control device in a kind of aircraft, especially be applicable to the control device in the toys aircraft.

Background technology

Aircraft is in when flight, because meeting such as its body, wing or propeller change its state of flight because of the active force of outside, as inclination etc.In order to adjust its state of flight, often adopt the balance regulation system in the body.For large-scale aircraft, as helicopter, all adopt the adjustment control system of more complicated, adjust automatically by central control system.The structures of this class control system etc. are more complicated all, is not suitable for little toys aircraft.At present, general toys aircraft all adopts better simply frame for movement to make, as directly it being climbed by the rotation of driven by motor propeller, all do not consider for the tenesmus phenomenon that in its flight course, is subjected to external force and influences all generations, therefore, present toys aircraft is all seldom installed relevant balance control device.And adopt the complicated balance control device of structure, will be because of costing an arm and a leg etc. former thereby being abandoned.

Summary of the invention

The purpose of this utility model is the structure that is short of at existing toys aircraft and a kind of balance adjusting device that makes it to be adapted to such aircraft is provided, when the body gradient can be adjusted to plateau when setting the limit automatically, to guarantee the aircraft normal flight.

The balance adjusting device that is used for the toys aircraft of the present utility model is to start the adjustment that balanced controls carry out organism balance automatically by gauge tap.Be mainly used in the balance adjusting device in the toys aircraft, it is positioned on the body of aircraft, and it has two groups of balanced controls at least, and wherein one group is forward and backward adjustment balanced controls, and its another group is left and right adjustment balanced controls; Described balanced controls include motor and the gauge tap group that is positioned on the body at least, and this motor links to each other with power supply by the gauge tap group; These balanced controls are controlled by gauge tap.Can be used for adjusting organism balance by this device, to guarantee the aircraft normal flight.

The drawing explanation

Fig. 1 is applied to the structural representation of the preferred embodiment in the aircraft for the utility model;

Fig. 2 is the schematic perspective view of balanced controls in the adjusting device that is proposed according to the utility model principle;

Fig. 3 is the combination schematic perspective view of two groups of balanced controls;

Fig. 4 is for arranging schematic diagram at a kind of gauge tap that the foregoing description proposed;

Fig. 5 is a kind of circuit connection diagram of the foregoing description.

Embodiment

Referring to accompanying drawing 1, the utility model balance adjusting device is mainly used in the toys aircraft, also can be applicable to the small-sized aircraft of other, as model plane etc.It has two groups of balanced controls at least, and wherein one group is forward and backward adjustment balanced controls A, is used to adjust the heeling condition of body front and rear direction, and its another group is left and right adjustment balanced controls B, is used to adjust the heeling condition of the left and right direction of body.Described balanced controls include the motor 11 (shown in Figure 2) and gauge tap group 13 (relevant housing construction end illustrates among the figure) that is positioned on the body at least, and this motor 11 links to each other with power supply by gauge tap group 13; These balanced controls are controlled by the gauge tap group.This motor has following two kinds of versions: one, this motor fixedly is positioned on the body, and its motor shaft is connected with a counterweight 12 (Fig. 1 is to shown in Figure 3), when machine operation, drives counterweight 12 and rotates, and body is subjected to the effect of its steering force and realizes its adjustment.This working method is called positive rotating motor.Two, this motor shaft is positioned on the body regularly, and when electric motor starting, motor casing or main body are reversed around motor shaft, promptly this motor is for reversing motor, make motor play a part counterweight, the work by its steering force is in order to adjust the balance of body, and this working method is called reverse motors.When this steady mechanism is applied to aircraft, promptly play a part to adjust whole fuselage balance.

The above-mentioned counterweight that links to each other with motor shaft 12 is two or more.Its counterweight can be positioned on a side of motor, also can be positioned on the both sides of motor by the axle at motor two ends.

The motor of above-mentioned described every group of balanced controls can be selected for use a plurality of, is more than two or two.

Above-mentioned described reverse motor also can be two or more.

Join Fig. 1 again, embodied above-mentioned balanced controls among Fig. 1 and be applied to concrete structure in the aircraft.Above-mentioned two groups of balanced controls are pacified on the body respectively, referring to Fig. 3, wherein the counterweight 11 of front and back adjustment balanced controls A or the rotation direction face of reverse motors are parallel to the YOZ plane, when machine operation, this counterweight rotates in being parallel to the YOZ plane, by the effect of its steering force, tilt to reach the body of adjusting on this in-plane.Adjustment balanced controls B is positioned on front and back and adjusts in the perpendicular plane of balanced controls A about another group, promptly the rotation direction face of the counterweight of these balanced controls B or reverse motors is parallel to the XOZ face perpendicular with the YOZ face, by rotating counterweight or reverse motors to realize the body heeling condition on this in-plane.XYZ among Fig. 2 and Fig. 3 represents three-dimensional coordinate system, and wherein X, Y represent both direction perpendicular on the horizontal plane, and its Z is to the expression vertical direction.

Referring to Fig. 4 and Fig. 5, the gauge tap group 13 of above-mentioned described every group of balanced controls all is positioned on the horizontal buck plate and (promptly is parallel to the face of XOY, sees Fig. 1), is in plateau following time to guarantee fuselage, and gauge taps all in the switches set are in off-state.This gauge tap group allows fuselage to have certain gradient, is in this orientation ± 5 degree scopes as gauge tap, is in disconnection, in case surpass this scope, will connect gauge tap, and starter motor, carries out body or fuselage adjustment.Shown in Figure 4, the gauge tap group of every group of balanced controls includes K switch 1, K1` and K switch 2, K2`, they are with the orientation reversed arrangement, be respectively applied for two kinds of different conditions in this orientation of control, as when adjusting the K switch 1 of balanced controls A and K1` before and after being used for and being used to control the adjustment of leaning forward, then K switch 2 and the K2` adjustment of facing upward before just being used to control.In conjunction with Fig. 3, when body is downward-sloping in YOZ face edge+Y orientation (along a Y orientation to facing upward), K switch 1 and K1` connect, K switch 2 and K2` disconnect, this moment, motor just changeed along direction shown in Figure 5, adjusted fuselage to plateau (being in the setting range) by balanced controls, and K switch 1 and K1` disconnect, balanced controls quit work, otherwise then K switch 2 and K2` connect, and K1 and K1` disconnect, the motor counter-rotating is adjusted fuselage to plateau in the other direction.Equally, when fuselage edge+X orientation is downward-sloping (edge-X orientation is to facing upward), K switch 3 and K3` connect, K switch 4 and K4` disconnect, this moment, this control motor just changeed, and adjusted fuselage to plateau (being in the setting range) by balanced controls, and K switch 3 and K3` disconnect, balanced controls quit work, otherwise then K switch 4 and K4` connect, and K3 and K3` disconnect, this control motor counter-rotating is adjusted fuselage to plateau in the other direction.

The gauge tap of described every group of balanced controls is made of K1 and K2; When K1 connected, K2 disconnected, otherwise when K2 connected, K1 disconnected; K1 links to each other with motor with power supply respectively by IC gauge tap circuit with K2.This circuit theory is general prior art, and wherein IC gauge tap role no longer illustrates at this with equaling above-described K switch 1` and K2`.

Switch in the above-mentioned described gauge tap group is a ball switch.

Claims

1, the balance adjusting device that is used for the toys aircraft, it is positioned on the body of aircraft, it is characterized in that: it has two groups of balanced controls at least, and wherein one group is forward and backward adjustment balanced controls A, and its another group is left and right adjustment balanced controls B; Described balanced controls include motor 11 and the gauge tap group that is positioned on the body at least, and this motor 11 links to each other with power supply by the gauge tap group; These balanced controls are controlled by gauge tap.

2, balance adjusting device according to claim 1 is characterized in that: this motor fixedly is positioned on the body, and its motor shaft is connected with a counterweight 12, when machine operation, drives counterweight 12 and rotates.

3, balance adjusting device according to claim 2 is characterized in that: the above-mentioned counterweight that links to each other with motor shaft 12 is two or more.

4, according to claim 2 or 3 described balance adjusting devices, it is characterized in that: the motor of above-mentioned described every group of balanced controls is more than two or two.

5, balance adjusting device according to claim 1 is characterized in that: this motor shaft is positioned on the body regularly, and when electric motor starting, motor casing or main body are rotated around motor shaft, promptly reverse motor.

6, balance adjusting device according to claim 5 is characterized in that: above-mentioned motor (reverse motor) be two or more than.

7, according to claim 2 or 3 or 4 described balance adjusting devices, it is characterized in that: above-mentioned two groups of balanced controls are pacified respectively on the body, and wherein the rotation direction face of the counterweight 12 of front and back adjustment balanced controls A is parallel to the YOZ plane; The counterweight of adjustment balanced controls B or the rotation direction face of reverse motors are parallel to the XOZ face perpendicular with the YOZ face about another group, and wherein X, Y represent both direction perpendicular on the horizontal plane, and its Z is to the expression vertical direction.

8, according to claim 5 or 6 described balance adjusting devices, it is characterized in that: above-mentioned two groups of balanced controls are positioned on respectively on the body, and wherein reverse motors axle and the YOZ face of front and back adjustment balanced controls A are perpendicular; The motor shaft and the face XOZ that adjust balanced controls B about another group are perpendicular, and wherein X, Y represent both direction perpendicular on the horizontal plane, and its Z is to the expression vertical direction.

9, balance adjusting device according to claim 7 is characterized in that: the gauge tap group of every group of balanced controls includes K switch 1, K1` and K switch 2, K2`, and they are respectively applied for two kinds of different conditions in this orientation of control with the orientation reversed arrangement.

10, balance adjusting device according to claim 7 is characterized in that: the gauge tap of every group of balanced controls is made of K1 and K2; When K1 connected, K2 disconnected, otherwise when K2 connected, K1 disconnected; K1 links to each other with motor with power supply respectively by IC gauge tap circuit with K2.

11, according to claim 1 or 2 or 3 or 5 or 6 described balance adjusting devices, it is characterized in that: described gauge tap is a ball switch.