A missile test launch hanger device with adjustable launch elevation angle and stop distance

Abstract

A missile test launching pylon device capable of adjusting the launch elevation angle and stop distance, including a launching pylon, a ground support, and a launcher; the launching pylon and the ground support are connected through a front support seat and a cushion block; The height of the spacer can realize different launch elevation angles of the launch hanger; the launch guide frame and the launch hanger are connected through the transfer lug; the transfer lug is installed and positioned through the lug guide plate in the beam groove, and the The detachable stop pin is connected with the beam body, which greatly improves the efficiency of replacing the guide frame and makes the experiment more secure; the guide frame is fixed by the stop plate on the stopper, and the stop plate is along the stopper. The track plate slides, which can be adapted to mount all guide frames whose stop distance meets the requirements of GJB‑1C, so it can be applied to ground static launch experiments of various types of air-to-air missiles, avoiding the scrapping of old launch racks in the past, and saving a lot of manpower , material and financial resources.

Description

technical field [0001] The invention relates to the technical field of an air-to-air missile ground static launch experiment device, in particular to a missile test launch hanger device capable of adjusting launch elevation angle and stop distance. Background technique [0002] When the air-to-air missile is performing a static launch test on the ground, it needs to be hung on the launch pylon together with the launcher for the launch test; because different types of air-to-air missiles need different launch elevation angles and guide frames when performing static launch tests, so Need to be equipped with different launch pylons; when a new type of air-to-air missile is developed, it means that a new launch pylon must be designed and produced at the same time, and the old launch pylon is scrapped because it is no longer used, thus wasting a lot of manpower, Material resources and financial resources; In addition, the transfer lugs of the original launch hanger are fixed and ...

AI Technical Summary

Problems solved by technology

[0002] When the air-to-air missile is performing a static launch test on the ground, it needs to be hung on the launch pylon together with the launcher for the launch test; because different types of air-to-air missiles need different launch elevation angles and guide frames when performing static launch tests, so Need to be equipped with different launch pylons; when a new type of air-to-air missile is developed, it means that a new launch pylon must be designed and produced at the same time, and the old launch pylon is scrapped because it is no longer used, thus wasting a lot of manpower, Material resources and financial resources; In addition, the transfer lugs of the original launch hanger are fixed and installed in the beam body groove through the support, bolts, and nuts, but the space of the beam body groove is small, and it is very inconvenient to operate when tightening the nuts, so each replacement The efficiency of the guide frame is extremely low, and the guarantee of mounting during the experiment is poor

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