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Launching control test box

A technology for testing boxes and boxes, which is applied in the test of ammunition, weapon accessories, ammunition, etc., can solve the problems of harsh external environment, poor portability, and increased system complexity, and achieves low system redundancy, high degree of specialization, The effect of convenient docking and use

Pending Publication Date: 2019-01-18
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, the resources introduced by redundant system test items will increase the complexity of the system and reduce the fault tolerance rate of the system
[0006] Difficulty in maneuvering transition caused by huge equipment
Missile launches often require maneuvering transitions, and the field environment is harsh, and the huge equipment will inevitably cause transportation difficulties and poor portability

Method used

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Embodiment Construction

[0034] In order to make the purpose, technical solutions and advantages of the implementation of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below in conjunction with the drawings in the embodiments of the present application. In the drawings, the same or similar reference numerals indicate the same or similar elements or elements with the same or similar functions. The described embodiments are part of the embodiments of the present application, but not all of the embodiments. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the application, but should not be understood as a limitation to the application. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of this application. The embodiments of the p...

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Abstract

The invention provides a launching control test box. The launching control test box includes a main box body, a damping frame, a test box body, an operating platform, an upper cover assembly and a support assembly. The main box body includes a first frame; the damping frame is installed in the main box body; the test box body is installed in the damping frame; the operating platform is installed in the first frame of the main box body; the upper cover assembly is detachably connected to the first frame; the support assembly is mounted on the upper cover assembly. The launching control test boxis provided with a retractable pull rod and a roller, convenience is provided for transportation and motorized transfer, and the launching control test box is light and convenient; a retractable support assembly is designed, the main box body of the launching control test box is placed on a support platform for testing, the system redundancy is low, the specialization degree is high, and convenience is provided for users during docking and use.

Description

Technical field [0001] The application belongs to the technical field of missile launch control test equipment, and particularly relates to a launch control test box. Background technique [0002] Missile flight control test equipment is an important equipment in the missile development and test stage. It shortens the missile test time, especially in the face of high-strength, high-consumption and aggressive battlefield conditions. It is extremely difficult to complete the missile launch preparation in a short time. How to quickly deploy and complete the test is to adapt to the objective requirements of future wars. [0003] At present, there are many types of airborne missile testing equipment, which generally have the following notable features: [0004] The test equipment is bulky due to the wide test coverage. Missile testing often needs to cover frequency measurement, voltage and current measurement, power consumption measurement, inertial function test, steering gear function...

Claims

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Application Information

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IPC IPC(8): F42B35/02
CPCF42B35/02
Inventor 嵇治刚李永丛晖沙群吴志文
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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