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Dynamic runway for taking off and landing of airplane

A dynamic and aircraft technology, applied in the field of airstrips, can solve problems such as accidents, achieve the effects of improving safety, strong practicability, and reducing operational difficulty

Inactive Publication Date: 2022-05-06
卢伯林
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] But no matter what kind of take-off method, the engine of the aircraft needs to be at full load. Very fragile, any obstacles and disturbances may lead to accidents

Method used

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  • Dynamic runway for taking off and landing of airplane
  • Dynamic runway for taking off and landing of airplane
  • Dynamic runway for taking off and landing of airplane

Examples

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Embodiment Construction

[0027] combined with Figure 1~3 , a dynamic runway for aircraft take-off and landing, including a drive shaft 1, a load-bearing shaft 2, a circulating crawler belt 3, a speed-regulating motor 4, and a truss 5, and the two ends of the truss 5 are provided with the drive shaft 1 rotatably connected to it , the drive shafts 1 are two horizontally arranged front and rear, on which are wound endless crawler belts 3 connected to the transmission, between the two drive shafts 1 is provided with a load-bearing shaft 2 parallel to it horizontally, the load-bearing The shaft 2 is arranged in the middle part of the endless crawler 3, which is used to support the endless crawler 3, and the speed regulating motor 4 is fixedly arranged on the truss 5, and the speed regulating motor 4 is connected with the driving shaft 1 through transmission;

[0028] The dynamic airstrip also includes a control center 6, a speed measuring radar 8, and a deck sensor 7, the control center 6 is electrically ...

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Abstract

The invention discloses a dynamic runway for taking off and landing of an airplane, which comprises driving shafts, a bearing shaft, a circulating track, an adjustable-speed motor and a truss, the two ends of the truss are provided with the driving shafts which are rotatably connected with the truss, the two driving shafts are horizontally arranged in parallel front and back, and the circulating track which is in transmission connection with the driving shafts is wound on the driving shafts; a bearing shaft which is horizontally arranged in parallel with the two driving shafts is arranged between the two driving shafts, the bearing shaft is arranged in the middle of the circulating crawler belt and used for supporting the circulating crawler belt, a speed regulating motor is fixedly arranged on the truss, and the speed regulating motor is in transmission connection with the driving shafts. According to the invention, the circulating track and the airplane pulley rotate in opposite directions at the same speed, so that the airplane uniformly takes off in an accelerated manner and lands in a decelerated manner during take-off and landing; when the aircraft takes off, a long runway is not needed, and when the aircraft lands, emergency deceleration is not needed, so that the safety of the aircraft in taking off and landing is improved; the device can be used in various takeoff and landing environments with limited runway length, such as aircraft carriers and mountainous airports, and is wide in application range.

Description

technical field [0001] The invention relates to the technical field of aircraft runways, in particular to a dynamic runway for aircraft takeoff and landing. Background technique [0002] Aircraft in the world today are mainly fixed-wing aircraft. Fixed-wing aircraft take off and land generally need a section of runway. The aircraft takes off when it accelerates to the take-off speed on the runway; Then slow down and taxi for a certain distance on the runway to a complete stop. Therefore, the runway generally needs a certain length, and the heavier the aircraft, the longer the runway needed. [0003] Due to the limitation of the length and width of the aircraft carrier, the airstrip is extremely short. The take-off of carrier-based aircraft is mainly divided into: vertical take-off, ski-jump take-off, and catapult take-off; [0004] 1) Vertical take-off and landing: relatively advanced, but the design is difficult, cannot be fully loaded, consumes a lot of fuel, and has a s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/04B64F1/02
CPCB64F1/04B64F1/02
Inventor 卢伯林
Owner 卢伯林
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