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Aircraft capable of effectively improving endurance

A technology of aircraft and capability, applied in the field of aircraft, can solve the problems of increasing the overall weight of the fuselage, insensitive steering mechanism, complex fuselage structure, etc., and achieve the effect of novel appearance, weight reduction and prolonging flight time

Inactive Publication Date: 2016-10-19
杨文兵
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The general aircraft model aircraft can drive the rotation of the entire steering mechanism through belt transmission or gear transmission. In the belt transmission, the long-term friction of the belt causes greater wear and tear, making the entire steering mechanism insensitive; and the power assembly of the gear transmission is composed of several gears. , wherein two main gears with equal diameters are superimposed through the main shaft in parallel and rotate synchronously with the shaft, one of the main gears drives the propeller unit installed on the main shaft to rotate synchronously, and the gear at the end of the transmission shaft is connected with the other main gear Engagement, through the large gear to drive the tail steering unit to rotate synchronously with the shaft, so that the structure of the fuselage is more complicated, and the overall weight of the fuselage is increased, and the increase in weight will increase energy consumption

Method used

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  • Aircraft capable of effectively improving endurance

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Embodiment Construction

[0011] The present invention will be further described below in conjunction with the accompanying drawings.

[0012] refer to figure 1 As shown, the power assembly 100 of the present invention is installed in the middle of the aircraft model, one end of which is connected to the steering unit, and the other end is connected to the empennage steering assembly, and the transmission of the power assembly drives the steering unit and the empennage steering assembly to rotate synchronously.

[0013] The aircraft capable of effectively improving endurance includes a first power unit 1 , a second power unit 2 and a transmission shaft 3 , and the first power unit 1 and the second power unit 2 are connected through the transmission shaft 3 . Wherein, the first power unit 1 includes a main shaft 10, a gear set 11 and a fixed sleeve 12. The main shaft 10 is also covered with a main shaft sleeve 101. The gear set 11 includes a motor gear 110 and a steering gear 112. On the panel of the m...

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Abstract

The invention provides an aircraft capable of effectively improving the endurance. The aircraft includes a first power device, a second power device, and a transmission shaft, and the first power device and the second power device are connected through the transmission shaft. Such a remote control aircraft toy greatly simplifies the integral structure of a model aircraft, but also reduces the weight of the fuselage, thereby effectively reducing the energy consumption and prolonging the flight time.

Description

technical field [0001] The invention relates to the field of model airplanes, in particular to an aircraft capable of effectively improving endurance. Background technique [0002] The general aircraft model aircraft can drive the rotation of the entire steering mechanism through belt transmission or gear transmission. In the belt transmission, the long-term friction of the belt causes greater wear and tear, making the entire steering mechanism insensitive; and the power assembly of the gear transmission is composed of several gears. , wherein two main gears with equal diameters are superimposed through the main shaft in parallel and rotate synchronously with the shaft, one of the main gears drives the propeller unit installed on the main shaft to rotate synchronously, and the gear at the end of the transmission shaft is connected with the other main gear Engagement, drive the empennage steering unit to rotate synchronously with the shaft through the large gear, so that the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/14A63H29/22A63H31/08
Inventor 杨文兵
Owner 杨文兵