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Pedaling spacecraft

A technology of spacecraft and wings, which is applied in the field of spacecraft, can solve the problems of not being able to realize the freedom of personal wishes to return to the destination, the crash of the plane, and the death of the plane, and achieve the effect of light weight, free and convenient travel, and easy to carry and use

Inactive Publication Date: 2014-01-15
嘉善联睿电子科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional aircraft and spacecraft are affected by time, climate and fuel, etc., and cannot freely travel to and from destinations according to individual wishes
Aircraft crashes are also often caused by weather, fuel and mechanical failures

Method used

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Embodiment Construction

[0013] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0014] like figure 1 , figure 2 and image 3 As shown, the propulsion spacecraft of the present invention includes a fuselage, lift-off propeller 1 and accumulator 4; On the base plate, two columns side by side are arranged on the base plate, and the middle and lower part of the column is provided with a cross support 3; the above-mentioned cockpit is similar to a rickshaw sitting and pedaling posture, and is used as a cushion for an astronaut. Its structural feature is that it also includes a parachute bird wing opening and closing device, a pedal force transmission part, and a bouncer. The parachute bird wing opening and closing device includes a parachute 2, two side-by-side column tops are provided with wings, the wings are preferably bird wings, and two bird wings form a bird wing type parachute, and the bird wing type parachute of the bird win...

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PUM

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Abstract

The invention discloses a pedaling spacecraft. The pedaling spacecraft comprises a machine body, rising propellers and a storage battery, and is characterized by further comprising a parachute bird wing opening and closing device and a pedaling transmission component, wherein the pedaling transmission component comprises a pedal, a chain plate and a chain plate shaft; the pedal of the pedaling transmission component is pedaled to rotate so as to allow the two rising propellers to fly; a crank handle is rocked to open and close a parachute like a bird wing, so that the bird-wing-type parachute flaps up and down to fly in a boosting way; the crank handle is rocked to rotate a driven wheel so as to drive a driven gear arranged on a wing opening and closing transmission rod to rotate; a chain wheel with a bevel gear is driven to rotate by another chain; the chain wheel with the bevel gear rotates to drive a bevel gear of a booster to rotate; the bevel gear of the booster rotates to drive a rotating shaft of the booster to rotate; the rotating shaft of the booster rotates to drive a boosting propeller to rotate; and the boosting propeller rotates to drive the spacecraft to fly forward. Both hands and both feet of a person are used for operating and pedaling the spacecraft for takeoff, so that the spacecraft can freely fly in the sky like a bird.

Description

technical field [0001] The invention relates to a spaceship, in particular to a spaceship which utilizes human body's feet and hands to operate pedaling force to take off. It can not only save energy but also exercise physical fitness, and it can fly freely in the sky like a bird. Overcome the constraints of time, space, climate, etc. on human activities. If you really want to fly, you can fly, and if you want to reach, you can reach. Background technique [0002] Traditional aircraft and spacecraft are affected by time, climate, and fuel, and cannot freely travel to and from destinations according to individual wishes. Aircraft crashes are also often caused by weather, fuel and mechanical failures. Contents of the invention [0003] The object of the present invention is to provide a push-force spacecraft operated by the movement of the human body's feet and hands in view of the above-mentioned shortcomings. [0004] The object of the present invention is achieved in ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C31/04B64C33/00
Inventor 柯依坤
Owner 嘉善联睿电子科技有限公司
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