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Aircraft launching system, launching method and aircraft

A launch system and aircraft technology, which is applied in the fields of spacecraft manufacturing, aircraft manufacturing, and launch, can solve the problems that affect the speed of human progress, the difficulty of rocket technology, and the high cost of launch, so as to achieve rich equipment operation experience, reduce the use of rockets, and launch low cost effect

Pending Publication Date: 2021-06-11
张志刚
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] It is precisely because of the technical difficulty of rocket development, high launch cost, and small payload that only large countries or companies with strong capital and advanced technology have the ability to launch spaceflights. This has affected the speed at which humans move toward the stars

Method used

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  • Aircraft launching system, launching method and aircraft
  • Aircraft launching system, launching method and aircraft
  • Aircraft launching system, launching method and aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0127] Embodiment 1: Aircraft launch system and launch method when the traction device is a heavy object

[0128] refer to figure 2 , when the traction device is a heavy object, the launch system includes: pulley block (1), steering fixed pulley (2), flexible cable (3), runway (4), aircraft (5), separation device (6), decoupling slow-down device (7), temperature control device (8), brake device (9), reset traction device (10), weight (11), buffer pool (12), base (18), grounding device (22);

[0129] Described: block pulley (1) fixed pulley side, steering fixed pulley (2), separation device (6), temperature control device (8), braking device (9), reset traction device (10) are all connected with their base (18) are connected; pulley block (1), steering fixed pulley (2), separation device (6), braking device (9), reset traction device (10) are all connected to each other with their own grounding device; pulley block (1) movable pulley side Connect with the heavy object (11), ...

Embodiment 2

[0139] Embodiment 2: Aircraft launch system and launch method when the traction device is a launch tractor

[0140] refer to image 3 , when the traction device is a launch tractor, the launch system includes: pulley block (1), steering fixed pulley (2), flexible cable (3), runway (4), aircraft (5), separation device (6), decoupling slow down Device (7), temperature control device (8), braking device (9), reset traction device (10), launching tractor (13), inclined road surface (17), base (18), grounding device (22) ;

[0141] Described: block pulley (1) fixed pulley side, steering fixed pulley (2), separation device (6), temperature control device (8), braking device (9), reset traction device (10) are all connected with their base (18) are connected; pulley block (1), steering fixed pulley (2), separation device (6), braking device (9), reset traction device (10), launching tractor (13) are all connected to each other with their own grounding device The pulley block (1) m...

Embodiment 3

[0153] Embodiment 3: Aircraft launch system and launch method when the traction device is a launch tractor

[0154] refer to Figure 4 , when the traction device is the launching tractor, the launch system includes: pulley block (1), steering fixed pulley (2), flexible cable (3), runway (4), aircraft (5), separation device (6), decoupling slow down Device (7), temperature control device (8), braking device (9), reset traction device (10), launching tractor (14), base (18), grounding device (22);

[0155] Described: pulley block (1) fixed pulley side, steering fixed pulley (2), separation device (6), temperature control device (8), brake device (9), reset traction device (10), launch tractor (14 ) are all linked to each other with their own base (18); block pulley (1), steering fixed pulley (2), separating device (6), braking device (9), reset traction device (10), launching tractor (14) They are all connected with their own grounding devices; the movable pulley side of the p...

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Abstract

The invention discloses an aircraft launching system, a launching method and an aircraft. A huge traction force is applied to the movable pulley side of a pulley block, so that the movable pulley side of the pulley block obtains a high moving speed, and the free end of a flexible cable of the pulley block obtains a large traction force and a particularly high moving speed by utilizing the amplification effect of the pulley block; the free end of the flexible cable of the pulley block is connected with an aircraft which has a certain aerodynamic configuration and is subjected to heat-proof treatment on the surface, and the aircraft obtains advancing power through traction of the flexible cable, obtains lift force through the aerodynamic configuration and flies at a high altitude like flying a kite; after the aircraft reaches a designed speed, an unhooking slow descending device is unhooked from the aircraft, and the aircraft reaches a preset orbit by utilizing inertia or self power; after the aircraft reaches a safe distance, the unhooking slow descending device is opened, so that the flexible cable slowly descends to the ground; meanwhile, a braking device performs braking, so that a traction device stops slowly; and the traction force and the speed can be obtained through the free falling motion of an heavy object.

Description

technical field [0001] The invention relates to the fields of aircraft manufacture and launch, in particular to the fields of spacecraft manufacture and launch. Background technique [0002] The future of mankind lies in space. At present, the enthusiasm for space exploration in various countries is high. However, due to the launch cost of launch vehicle technology and the development of rocket technology, our space exploration is still at an early stage. [0003] The cost of a launch of my country's Long March 3B carrier rocket is about 400-500 million yuan; due to the small batch production of rockets in Europe, the cost of a launch is about 300-400 million US dollars; the cost of American Atlas and Delta rockets is 140-200 million US dollars , The total cost of a launch is about 430 million US dollars. [0004] At present, the mainstream large-scale launch vehicle in the world has a low-earth orbit carrying capacity of about 20 tons, and a synchronous orbit carrying capac...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/10
CPCB64F1/04B64F1/10
Inventor 张志刚
Owner 张志刚
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