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Mars aircraft capable of inflating and injecting take-off and gliding recovery and using method thereof

An aircraft, Mars technology, applied in the field of Mars aircraft, can solve the problems of insufficient thrust, excessive weight, complex power system structure, etc., and achieve the effect of prolonging the service life, light structure and wide land range.

Active Publication Date: 2019-08-23
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In view of this, the present invention provides an inflatable jet take-off and gliding recovery Mars aircraft and its use method, which are used to solve the problem of insufficient thrust of traditional aircraft in the Martian atmospheric environment and at the same time solve the problem of complex structure and heavy weight of the power system. To provide a reusable, energy-dense and lighter aircraft

Method used

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  • Mars aircraft capable of inflating and injecting take-off and gliding recovery and using method thereof
  • Mars aircraft capable of inflating and injecting take-off and gliding recovery and using method thereof
  • Mars aircraft capable of inflating and injecting take-off and gliding recovery and using method thereof

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Embodiment Construction

[0042] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are merely examples and are not intended to limit the present application.

[0043] An embodiment of the present invention provides a Martian aircraft with a gas-filled jet take-off and gliding recovery, such as Figure 1-Figure 6 As shown, figure 1 with Figure 4 Is the front view of the Martian vehicle, figure 2 with Figure 5 Is the side view of the Martian vehicle, image 3 with Image 6 It is a top view of the Martian vehicle, including: the fuselage 1, the wing 2 connected to the top of the fuselage 1, and the tail 3 connected to the tail of the fuselage 1; Figure 7 As shown, Figure 7 It is a cross-sectional view of the fuselage 1, and also includes: an inflatable jet part 4 located inside the fuselage 1;

[0044] The inflatable jet part ...

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Abstract

The invention discloses a mars aircraft capable of inflating and injecting take-off and gliding recovery and an using method thereof. According to the mars aircraft and the using method thereof, the compressed gas is used as power, a complex rotating mechanism can be omitted for the aircraft, the characteristic that the structure is light in weight is realized, so that the problem that the lift force is difficult to meet the endurance requirement due to the fact that the mars thin atmosphere is limited is solved; moreover, the compressed gas has relatively high energy density and propulsion power, the compressed gas not only can provide enough thrust for the aircraft in a mars environment which is thin in atmosphere, the problem of insufficient thrust of a traditional propeller in the marsatmospheric environment is overcome, and the aircraft can also be driven to obtain higher flight height for gliding flight, and the cruising time of aircraft remaining in air is prolonged; in addition, the compressed gas is taken from the mars atmosphere, the compressed gas does not need to be carried in advance, and can realize the repeated inflation and air injection circulation process. Compared with an existing one-time gliding landing aircraft, the number of tasks of the aircraft can be increased, the service life of the aircraft is prolonged, and a wider land range is detected.

Description

Technical field [0001] The invention relates to the technical field of aircraft aerodynamic layout design, and in particular to a Martian aircraft with an air-filled jet take-off and gliding recovery and a use method thereof. Background technique [0002] Compared with traditional satellites or ground patrol devices, Mars aircraft has the advantages of large measurement range and strong maneuverability. The United States, Europe, Japan and other countries have put forward many designs for Martian aircraft, such as NASA’s "Prandtl-m" aircraft and "Martian Helicopter" aircraft, and Japan’s JAXA’s "Sample Martian Aircraft" aircraft. [0003] Due to the extremely thin atmosphere of Mars, the density of its surface atmosphere is only equivalent to that of the earth at a height of 27km. This thin atmosphere brings great challenges to aircraft design. The low atmospheric density combined with the low Reynolds number effect caused by the low density will cause the thrust generated by the ...

Claims

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Application Information

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IPC IPC(8): B64G1/10B64G1/40
CPCB64G1/105B64G1/40B64G1/1071
Inventor 蒋崇文李志豪许晨豪高振勋李椿萱
Owner BEIHANG UNIV