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Multifunctional high-speed sailing aircraft

A multi-functional, aircraft technology, applied in the field of aircraft, can solve the lagging of comprehensive technologies such as safety, performance, high speed, long-distance voyage, heavy load, energy saving, consumption reduction, environmental protection, etc., new energy-saving technologies have not been fully considered and applied, and large consumption Problems such as non-renewable energy and harmful gases have achieved the effect of high comprehensive cost performance, exquisite and elegant design, and high cost performance

Active Publication Date: 2014-02-19
LIUZHOU JINGYANG ENERGY SAVING TECH RES DEV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The development of modern military and civil aviation should be dominated by improving the comprehensive technical strength of aviation, strengthening and improving the combat power of the air force, safe and fast landing and high-speed navigation, long-distance and heavy-duty direct flights, energy saving, consumption reduction and efficiency improvement, and energy environment protection. All kinds of domestic and foreign military and civilian aircraft are still lagging behind in comprehensive technologies such as safety, performance, high speed, long-distance voyage, heavy load, energy saving, consumption reduction, and environmental protection, and the aircraft need to consume a large amount of non-renewable energy and emit a large amount of harmful Gas, especially the comprehensive technical performance and benefit expectations of overall energy saving and consumption reduction, direct lifting, safe high-speed, long-distance direct flight, etc. are very low. Therefore, it is necessary to further strengthen research and create high-tech comprehensive technologies in this field to promote military and civil aviation. rapid development
For example, the new energy multifunctional aircraft described in the Chinese invention patent application with the application number 201110151370.1 published on August 31, 2011, its new energy is not new, but a simple borrowing of common solar energy technology, and new types of wind energy such as motorized wind energy can be greatly utilized. Energy-saving technology is not fully considered and applied
And there are not many so-called multi-functions, and it is just a superficial reference of general technical functions such as batteries with poor safety performance, hydraulic expansion, vertical lift, etc., that is, the overall comprehensive technical performance of the aircraft needs to be further improved and improved

Method used

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  • Multifunctional high-speed sailing aircraft

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Embodiment Construction

[0022] Such as figure 1 As shown, the multifunctional high-speed voyage aircraft (hereinafter referred to as "aircraft") of the present invention includes a cabin device, a power device, a lifting device, and a flying device.

[0023] The cabin device includes a loading cabin 36, a lower cabin 19, and an upper cabin 46. The loading compartment 36 is located in the middle of the machine body, and the loading compartment 36 can be set into single or multiple compartments of different grades and purposes according to needs; the lower engine compartment 19 is located at the bottom of the lower exhaust duct 5 under the loading compartment 36 for placing the front The wind motor 2 and its exhaust pipe, the lower lifter A12, the lower lifter B15, the lower lifter C20, the lower engine A10, the lower engine B14, the lower engine C21, etc.; the upper nacelle 46 is located on the upper part of the loading bay 36 for Place the main power storage plate 40 and the upper elevator A53, the upp...

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Abstract

The invention discloses a multifunctional high-speed sailing aircraft, and relates to an aircraft. The aircraft comprises a cabin device, a power device, a lifting device, a flying device and a part device, wherein the cabin device comprises a loading cabin, an embarking cabin and a disembarking cabin; the embarking cabin and the disembarking cabin are positioned on the upper part and the lower part of the loading cabin; the power device comprises an engine unit, a wind turbine unit and spray thrusters; the engine unit comprises a main engine, an auxiliary engine and a lower engine; the wind turbine unit comprises a wind energy generator, a front wind turbine, an upper wind turbine, a wing wind turbine and a wind energy and solar energy accumulator plate; the lifting device comprises an upper lifter, a lower lifter, an upper transmission shaft and a lower transmission shaft; and the flying device comprises a head, an air inlet grid, upper and lower wings, an automatic empennage, a driving control room, a lifting frame and a dual-purpose wheel. The aircraft has superior performance, a wide application range and long service life, is high-efficiency, energy-saving and environment-friendly, performs vertical lifting safely and quickly, performs high-speed and heavy-duty sailing, is low in cost, and has extremely high comprehensive cost performance.

Description

Technical field [0001] The invention relates to an aircraft, in particular to a multifunctional high-speed long-distance voyage aircraft. Background technique [0002] The development of modern military and civil aviation should be led by improving the comprehensive technical strength of aviation, strengthening and improving the combat power of the air force, safe and fast lifting and high-speed navigation, long-distance heavy-load direct flight, energy saving, consumption reduction and efficiency increase, and protection of energy environment. Various military and civilian aircraft at home and abroad still lag behind in comprehensive technologies such as safety, performance, high speed, long voyage, heavy load, energy saving, consumption reduction, and environmental protection, and the aircraft needs to consume a large amount of non-renewable energy and emit a large amount of harmful Gas, especially the overall technical performance and benefit expectations of energy saving and ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D27/24B64D27/16B64D33/04
Inventor 韦战
Owner LIUZHOU JINGYANG ENERGY SAVING TECH RES DEV
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