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Left-internal and right-internal ejection balance cable hook towed machine aircraft carrier electromagnetic flywheel ejector

A technology of balance wheel and internal balance, applied in the direction of launch/drag transmission device, etc., can solve the problems of difficulty in dragging the balance device, bumping of the rotating car, etc., and achieve the effect of simple design and easy manufacture.

Pending Publication Date: 2018-11-02
攸县天帆电池制造有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The existing short-distance rotating hook tractor is fixed between the front end and the rear end of the frame of the hook tractor by the head and tail of a single steel cable, and is dragged by the hook provided at the upper end of the hook tractor. When the transfer vehicle is moving forward or backward, it is difficult to set the left inner and right inner drag balancing devices on the front end of the rotating hook tractor. When the heavy load is being transferred, the left and right of the hook tractor shake, causing the turning vehicle to run bumpy

Method used

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  • Left-internal and right-internal ejection balance cable hook towed machine aircraft carrier electromagnetic flywheel ejector
  • Left-internal and right-internal ejection balance cable hook towed machine aircraft carrier electromagnetic flywheel ejector
  • Left-internal and right-internal ejection balance cable hook towed machine aircraft carrier electromagnetic flywheel ejector

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Effect test

Embodiment Construction

[0014] 1: Left inner cable balance wheel (2)

[0015] The upper end of the cable balance wheel of the left inner cable balance wheel (2) is located below the right end of the front concave edge of the left upper beam plate (3), and the outer circle of the cable balance wheel of the left inner cable balance wheel (2) The right end is set at: the left end of the front beam seat of the left beam (4), and the lower end of the cable balance wheel of the left inner cable balance wheel (2) is set at: the front concave edge of the left lower beam plate (5) Above the right end, the center above the cable balance wheel of the left inner cable balance wheel (2) is provided with: the balance wheel shaft hole of the left inner balance wheel shaft hole (6) is located in: the balance wheel shaft outer circle of the left inner balance wheel shaft (7) middle. The balance wheel shaft excircle upper end of the left inner balance wheel shaft (7) is located at: the left inner shaft hole inner cir...

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PUM

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Abstract

The invention relates to a left-internal and right-internal ejection balance cable hook towed machine aircraft carrier electromagnetic flywheel ejector. A left-internal and right-internal ejection balance cable hook towed machine can be used in the defense technology and serves as left-internal and right-internal ejection balance cable device in a hook towed machine of the ejector used by an aircraft carrier ejection plane. The left-internal and right-internal ejection balance cable hook towed machine can be arranged under an aircraft carrier flat deck hook groove and can also be arranged under a bow aircraft carrier deck, and towing ejection is carried out in a rack rail in a cabin; a left-internal and right-internal ejection balance cable is arranged on a left inner wheel groove at the front end of a towing force mergence balanced left beam to rotate and on a right inner wheel groove at the front end of a towing force mergence balanced right beam to rotate, and can be arranged and under the aircraft carrier flat deck hook groove and performs skewed edge shaking of a towing ejection left-internal and right-internal towing ejection cable belt, and movable decks do not need to be installed at both sides of the aircraft carrier flat deck ejection hook groove.

Description

1. Technical field [0001] The present invention relates to an electromagnetic catapult for a left-inner and right-inner ejection balance steel cable hook tractor aircraft carrier. [0002] 1. The present invention: left inner right inner ejection balance steel cable hook tractor, can be used in national defense technology, in the hook tractor of a kind of catapult used as aircraft carrier catapult aircraft, left inner right inner ejection balance steel cable device . [0003] 2. In the present invention: left inner right inner eject balance steel cable hook drag machine, can be installed in the rack track in the machine room below the plane deck hook groove of aircraft carrier drag ejection, left inner right inner eject balance steel cable, install On the right side of the front end of the left crossbeam of the drag force combined balance and the left side of the front end of the drag force combined balance right beam, it can be installed under the hook groove of the plane de...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 李运初
Owner 攸县天帆电池制造有限公司