Deep space exploration aircraft

A technology for deep space exploration and aircraft, applied in the field of aerospace

Inactive Publication Date: 2011-03-30
臧铁成
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] This technical invention is to solve the technical problem of ultra-long-distance deep space detection that internal combustion recoil power cannot achieve

Method used

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Embodiment Construction

[0034] Attached to the overall structure of the deep space exploration vehicle figure 1Among them, its front end is the control room, which is equipped with gear gear meshing indicator light 1, gear fault indicator light 2, and alarm indicator 3 in the automatic transmission in the mechanical power assembly body, because there are eight gear gears in the transmission. So there are eight display lights each. Because the internal transmission structures of all mechanical power assemblies except the steering structure are uniformly controlled, the control of the internal engine of the mechanical power assembly only has two positive and negative switches 4 for speed-up and deceleration. When the rotational power of all the engines engages a transmission gear, the gear display light 1 in the control room will light up. When a certain engine or related structure breaks down and affects gear engagement, the fault display lamp 2 and the warning display 3 will give an alarm display. ...

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Abstract

The invention relates to a deep space exploration aircraft, which is mainly applied to deep space exploration technology. An anthropogenic load power engine in the aircraft can replace internal combustion power and solar energy, so that the power and energy supply of the aircraft achieve permanent balance; meanwhile, the engine also can be used for various power machines. The aircraft has the main technical characteristics that: the engine makes a fixing plate at the upper end of each telescopic rod apply downward pressure to the telescopic rod by using the applied force of fixed air pressure, so that a plurality of telescopic rods on a crankshaft in the aircraft extend substantially and retract insubstantially in a circulating mode, the crankshaft is pushed to rotate, and the fixing plate at the upper end of each telescopic rod is fixed; the crankshaft rotates to drive a fan blade wind wheel in a closed air chamber to rotate in an air spraying cylinder to generate recoil airflow, so the fan blade wind wheel rotates to make a mechanical power assembly apply pushing force to the aircraft; and the recoil airflow is converted into rotation power by a recoil airflow converter, the rotation power drives a generator to generate electricity, and the airflow returns to the front end of the wind wheel to be recycled after being converted.

Description

Technical field: [0001] The technology of the invention belongs to the field of aerospace technology, especially a deep space exploration aircraft. In addition, its internal engine is an artificially loaded power engine instead of internal combustion power, which can be used in various technical fields corresponding to internal combustion engines. Background technique: [0002] The various resources of the earth on which we depend are becoming increasingly depleted, greenhouse gas emissions are difficult to control, and the living environment is deteriorating. Therefore, people are constantly looking for new alternative energy sources. But it's all looking around internal combustion power technology. In addition, in recent years, developed countries have been continuously exploring other planets to find new living environments. However, the existing technology is difficult to meet the needs of deep space exploration. Invention content: [0003] The technical inventio...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/42B64G1/40F01B29/00F01B23/00F16H37/12
Inventor 臧铁成
Owner 臧铁成
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