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Flying method on Mars, and Mars flying device

A flying device, the technology of Mars, applied in the field of flight, can solve the problems that the electric drive wheel device is prone to accidents, and the electric drive wheel device cannot be observed and sampled nearby

Pending Publication Date: 2020-08-11
NINGBO INST OF MATERIALS TECH & ENG CHINESE ACADEMY OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] However, due to the soft soil in many areas on Mars, it is necessary to overcome greater resistance when moving on Mars, especially when encountering complex landforms, the electric drive wheel device is prone to accidents
In addition, for steep or high landforms, the electric drive wheel device cannot observe and sample nearby
Therefore, the exploration and investigation of Mars are facing great difficulties

Method used

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  • Flying method on Mars, and Mars flying device
  • Flying method on Mars, and Mars flying device
  • Flying method on Mars, and Mars flying device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0044] A Martian flying device, such as figure 1 As shown, the flight body 1 is included, and the flight body 1 includes a power supply 16 , a high-speed motor 12 , an impeller 13 and a soil storage container 14 .

[0045]During the working state, the power supply 16 supplies power to the high-speed motor 12, and the high-speed motor 12 works to drive the impeller 13 to rotate at a high speed. The soil 8 falls from the soil storage container 14 to the impeller 13, is accelerated by the high-speed rotating impeller 13, and is thrown out through the nozzle 6 to generate The reaction force overcomes the gravity of Mars and drives the flying device to take off on Mars.

[0046] The flight device also includes Probe A3 and Probe B4 for detection research.

[0047] The flying device also includes a communicator 5 for communication.

[0048] The flying device also includes a central controller 15 for coordinated control of the entire flying device.

[0049] In this embodiment, the...

Embodiment 2

[0051] A Martian flying device, such as figure 2 As shown, the flight body 1 is included, and the flight body 1 includes a power supply 11 , a high-speed motor 12 , an impeller 13 and a soil storage container 14 .

[0052] During the working state, the power supply 11 is powered by a high-speed motor, and the high-speed motor 12 works to drive the impeller 13 to rotate at a high speed. The soil 8 falls from the soil storage container 14 to the impeller 13, is accelerated by the high-speed rotating impeller 13, and is thrown out through the nozzle 6, resulting in The reaction force overcomes the gravity of Mars and drives the flying device to take off on Mars.

[0053] In this embodiment, the power supply 11 is a storage battery, and the onboard storage battery can be quickly charged through the Mars solar power station 9 if necessary.

[0054] In addition, in this embodiment, the soil 8 is grabbed into the soil storage container 14 from the outside of the flying device by th...

Embodiment 3

[0059] In this embodiment, the structure of the Mars flying device is basically the same as that of Embodiment 2, the difference is that the solar power station 9 is replaced by the solar panel 2, and the solar panel 2 is arranged on the flying device, so when the power is insufficient, the flying device The battery 11 is charged by the solar panel 2 .

[0060] In this embodiment, the flying method of the flying device is the same as that in Embodiment 1.

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Abstract

The invention discloses a flying method on Mars, and a Mars flying device. According to the method, a medium on the surface of Mars and a medium acceleration unit are adopted; under the action of electric power, the medium acceleration unit works, the medium is conveyed to the medium acceleration unit, and is separated from the medium acceleration unit after being accelerated by the medium acceleration unit, and reactive force is generated due to momentum conservation and overcomes Mars attraction to drive a load to take off. The method is novel and unique, is suitable for the Mars environmentwhich does not have atmosphere and cannot fly by means of atmospheric buoyancy, breaks through the obstacle of Mars morphology to scientific investigation, and can expand the detection, investigationand development capacity of human beings to Mars.

Description

technical field [0001] The invention belongs to the technical field of flight, and in particular relates to a flight method on Mars and a Mars flight device. Background technique [0002] Unlike the Earth, which has a dense atmosphere, the atmosphere on the surface of Mars is very thin, and it is impossible to fly on Mars with the help of atmospheric buoyancy. [0003] At present, the landing and return to Mars mainly rely on the principle of rockets, that is, the aircraft carries its own reactive substances, and the medium impulse is generated through chemical reactions to overcome the gravitational constraints. However, due to the limited rocket fuel, it is difficult to use rocket fuel in the Martian environment for a long time. Other means of propulsion, such as electric propulsion, plasma propulsion, etc., still require a large amount of auxiliary energy, structure and medium consumption, so flying on Mars is very difficult. [0004] For this reason, it can be consider...

Claims

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Application Information

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IPC IPC(8): B64G1/10B64G1/44B64G1/66
CPCB64G1/105B64G1/44B64G1/66B64G1/10B64D27/02
Inventor 张文武王玉峰
Owner NINGBO INST OF MATERIALS TECH & ENG CHINESE ACADEMY OF SCI
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