A method for landing and landing of a v-shaped chute with directional speed control for an aircraft

An aircraft and chute technology, applied in the field of aircraft, can solve the problems that the front wheels cannot control the direction at the first time, the landing gear is prone to failure, etc., and achieve the effect of avoiding danger

Active Publication Date: 2022-02-08
李模萍
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the embodiments of the present invention is to provide a landing method of a directional speed control V-shaped chute for an aircraft, which is used to solve the problem that the landing gear of the existing aircraft is prone to failure when landing, and the front wheels cannot control the direction at the first time when landing.

Method used

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  • A method for landing and landing of a v-shaped chute with directional speed control for an aircraft
  • A method for landing and landing of a v-shaped chute with directional speed control for an aircraft
  • A method for landing and landing of a v-shaped chute with directional speed control for an aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0057] Space Shuttle:

[0058] 1. Two landing shuttles with a small included angle are installed at the bottom of the space shuttle.

[0059] 2. It is equipped with two small-angle aircraft take-off and landing shuttles at the bottom of the space shuttle, and two V-shaped chutes for directional and speed-controlled aircraft special take-off are laid on the runway.

[0060] 3. Install the aircraft start chute at the bottom of the directional speed control V chute of the aircraft.

[0061] 4. Set up a fuel supply point near the aircraft start chute.

[0062] 5. Build a V-shaped chute platform with 0 buoyancy force landing aircraft on the sea for directional speed control.

[0063] 6. The fuel needed for the space shuttle to prepare for takeoff is supplied by the fuel supply point.

[0064] 7. Start the space shuttle at full speed.

[0065] 8. Disconnect the fuel supply interface, and at the same time control the jack-up aircraft to start the chute.

[0066] 9. The space shu...

Embodiment 2

[0071] Jet carrier aircraft:

[0072] 1. Two landing shuttles with a small included angle are installed at the bottom of the jet carrier aircraft.

[0073] 2. Lay a V-shaped chute for directional speed control of small-angle aircraft on the runway of the aircraft carrier.

[0074] 3. Install the aircraft start slider at the bottom of the front and rear center of gravity of the jet carrier aircraft.

[0075] 4. When the jet carrier-based aircraft lands, the first landing point of the fuselage is installed with a high-strength aircraft landing shock absorber.

[0076] 5. When the jet carrier-based aircraft takes off, the pilot first turns on the full horsepower, and then turns on the aircraft start slider.

[0077] 6. The jet carrier-based aircraft can lift off safely in the shorter aircraft directional speed control V-shaped chute.

[0078] 7. The jet carrier-based aircraft is ready to land, and the high-strength aircraft landing shock absorber is turned on.

[0079] 8. The...

Embodiment 3

[0081] Large airliner:

[0082] 1. Three large-angle aircraft landing and landing shuttles are installed at the bottom of the large passenger aircraft.

[0083] 2. Cover the existing runway with a V-shaped chute for directional speed control of aircraft with a large angle.

[0084] 3. At the bottom of the center of gravity of the front and rear of the large passenger aircraft, install the aircraft start skateboard.

[0085] 4. When a large passenger plane lands, a suitable position is selected on the abscissa of the fuselage at the first landing point of the aircraft shuttle, and a high-strength aircraft landing shock absorber is installed.

[0086] 5. Before the large passenger plane takes off, turn on the aircraft and start the skateboard, so that the taxiing is more stable and comfortable, and it takes off smoothly.

[0087] 6. When a large passenger plane lands, the landing damping plate of the aircraft is opened immediately. Because of the large angle and inertia, it is...

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Abstract

The embodiment of the present invention discloses a landing method of a directional speed control V-shaped chute for an aircraft, which includes the following steps: Step 1, according to the glide distance on the runway when the aircraft lands or takes off, the aircraft runway is covered with isometric contours A plurality of V-shaped chutes connected; step 2, at least one landing shuttle is installed at the bottom of the aircraft, the landing shuttle at the bottom of the aircraft can slide directionally in the V-shaped chute on the runway, and the V-shaped chute on the runway of the aircraft The number of chutes is greater than the actual number used by the aircraft. An aircraft chute directional landing method provided by the embodiment of the present invention, by laying the chute on the runway, and setting the landing shuttle used in conjunction with the chute at the bottom of the aircraft, so that the application can be realized without setting the landing gear at the bottom of the aircraft The landing or lifting of the aircraft solves the problem that the landing gear of the existing aircraft is prone to failure when the aircraft lands.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a method for landing and landing of a directional speed-controlled V-shaped chute of an aircraft. Background technique [0002] Existing aircraft usually use landing gear when landing, but the landing gear bears a large load, large size, and complex structure, so it has a large mass and is prone to damage. Life poses a major threat, and when the existing aircraft lands, the rear wheels generally touch the ground first, and the front wheels cannot control the direction. Contents of the invention [0003] The purpose of the embodiments of the present invention is to provide a landing method of a directional speed control V-shaped chute for an aircraft, which is used to solve the problem that the landing gear of the existing aircraft is prone to failure when the aircraft lands, and the front wheels cannot control the direction at the first time when landing. [0004] In order to achieve t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/52B64F1/00
CPCB64C25/52B64F1/00
Inventor 李阳
Owner 李模萍
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