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Water surface aircraft model water landing buffer shock absorber and water surface aircraft model

A technology of shock absorbing device and aircraft, which is applied in the direction of toy airplanes, toys, entertainment, etc., and can solve the problem of not being able to effectively realize the cushioning and shock absorption of aircraft models

Active Publication Date: 2020-12-08
BEIJING RES INST OF MECHANICAL & ELECTRICAL TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The invention provides a water surface aircraft model water landing buffer and shock absorbing device and a water surface aircraft model, which can solve the technical problem in the prior art that only relying on buffer slides cannot effectively realize the buffer and shock absorption of the aircraft model in the water landing process

Method used

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  • Water surface aircraft model water landing buffer shock absorber and water surface aircraft model
  • Water surface aircraft model water landing buffer shock absorber and water surface aircraft model
  • Water surface aircraft model water landing buffer shock absorber and water surface aircraft model

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Embodiment Construction

[0021] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0022] It should be noted that the terminology used here is only for describing specific implementations, and is not intended to limit t...

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Abstract

The invention provides a water surface aircraft model landing buffer damping device and a water surface aircraft model. The water surface aircraft model landing buffer damping device comprises a sliding plate assembly and a locking release mechanism. The locking release mechanism comprises an ejector rod, a first elastic damping part, a second elastic damping part, a clamping end part and a clamping pin assembly, wherein the first elastic damping part is arranged on the ejector rod in a sleeving manner; the second elastic damping part is arranged in a groove of the ejector rod; and the clamping pin assembly is used for being matched with the clamping end part to realize buffering and damping through the first elastic damping part and the second elastic damping part. By applying the technical scheme, the technical problem that in the prior art, the buffering and damping of an aircraft model cannot be effectively realized only by means of the buffering sliding plate is solved.

Description

technical field [0001] The invention relates to the technical field of aircraft test model design, in particular to a water landing buffer and shock absorber for a water surface aircraft model and a water surface aircraft model. Background technique [0002] The near-surface aircraft can make full use of the weak link of surface ships in the near-water space defense, combine the advantages of flight, penetration and damage in air and water media, and achieve efficient strikes against the enemy's surface ships with strong terminal defense capabilities , which can effectively solve the problems faced in the development of anti-ship missile penetration capabilities. In order to simulate the glide process of a near-water vehicle, model tests are usually carried out under pool conditions to verify the rationality of the glide weapon configuration and to determine the glide window. In the pool test, the aircraft model near the water surface had a large vertical overload at the mo...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): A63H27/00A63H27/14
CPCA63H27/00A63H27/14
Inventor 刘乐华魏毅寅赵蛟龙王亚东韩颖骏杨晓光
Owner BEIJING RES INST OF MECHANICAL & ELECTRICAL TECH
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