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Aircraft model launching tube adapter and model launching test system

A test system and adapter technology, which is applied in entertainment, toys, toy airplanes, etc., can solve problems such as adapter inseparability, aircraft model attitude and launch path interference, and achieve the effect of avoiding interference and high promotion value

Active Publication Date: 2019-09-03
BEIJING RES INST OF MECHANICAL & ELECTRICAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The invention provides an aircraft model launch tube adapter and a model launch test system, which can solve the technical problem in the prior art that the adapter cannot be quickly separated from the aircraft model and cause interference to the attitude and launch path of the aircraft model

Method used

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  • Aircraft model launching tube adapter and model launching test system
  • Aircraft model launching tube adapter and model launching test system
  • Aircraft model launching tube adapter and model launching test system

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Embodiment Construction

[0023] 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.

[0024] It should be noted that the terminology used here is only used to describe specific implementations, and is not intended to limit...

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Abstract

The invention provides an aircraft model launching tube adapter and a model launching test system. The adapter comprises a plurality of adapter units. The adapter units form a rotary body structure together. The rotary body structure is provided with a containing groove, and an aircraft model is arranged in the containing groove. One end of the rotary body structure is provided with a separation unit, and the separation unit is used for separating the adapter from the aircraft model through aerodynamic force after the adapter leaves the launching pipe. According to the technical scheme, the technical problem that in the prior art, an adapter cannot be rapidly separated from an aircraft model, and consequently the attitude and the emission path of the aircraft model are interfered is solved.

Description

technical field [0001] The invention relates to the technical field of aircraft model launch tests, in particular to an aircraft model launch tube adapter and a model launch test system. Background technique [0002] At present, there are two launching methods for the unpowered scale model launch test of the aircraft: the launch tube and the launch stand. For the revolving aircraft with a circular cross section, it is easy to match with the launch tube, so the launch tube is generally used for launch. For aircraft with complex configurations with non-circular cross-sections, since it is difficult to fit into the launch tube and adapt to the constraints, it is generally launched in the form of a launch stand, but the launch quality and launch speed it can withstand are greatly limited. Therefore, for aircraft models with complex configurations that have a large launch mass and require higher launch speeds, there is no matching adapter for launch tube launches. At the same t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/14
CPCA63H27/14
Inventor 刘乐华王亚东韩颖骏赵蛟龙杨晓光
Owner BEIJING RES INST OF MECHANICAL & ELECTRICAL TECH