Protective cover for rocket propellant operation

A rocket propellant and protective cover technology, which is applied in the direction of respiratory protection containers, cleaning methods and appliances, cleaning methods using tools, etc., can solve problems such as affecting the staff's line of sight, narrow staff's field of vision, and fogging of the inspection window, and achieve Avoid the effect of lowering the head and being restricted, improving the field of vision and ensuring clarity

Active Publication Date: 2022-04-26
中国人民解放军火箭军特色医学中心
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a protective cover for rocket propellant operation, which is used to solve the problem that the weight of the protective mask in the prior art is borne by the worker's head, which is very easy to fatigue, and the worker's field of vision is narrow, and the inspection window is fogged , incomplete, scratches and other problems that affect the staff's sight

Method used

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  • Protective cover for rocket propellant operation
  • Protective cover for rocket propellant operation
  • Protective cover for rocket propellant operation

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Embodiment Construction

[0030] The present invention will be described in detail below in conjunction with the drawings and specific embodiments. It should be noted that in the drawings or descriptions, similar or identical parts use the same figure numbers, and implementations that are not shown or described in the drawings The method is a form known to those of ordinary skill in the art. In addition, the directional terms mentioned in the embodiments, such as "upper", "lower", "top", "bottom", "left", "right", "front", "rear", etc., are only for reference to the accompanying drawings. The directions are not intended to limit the protection scope of the present invention.

[0031] Such as Figure 1 to Figure 7 As shown, a protective cover for rocket propellant operation of the present invention includes a cover body 1, a fixing device, a poison filter assembly and a breathing assembly 4, and the cover body 1 includes a top cover 11, an inspection window 12 and a ring seat 13, and the top cover 11 ...

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Abstract

The invention belongs to the field of wearable protective devices, and in particular relates to a protective cover for rocket propellant operation, which includes a cover body, a fixing device, a poison filter assembly and a breathing assembly. There is a connecting groove on the top, a connecting ring is integrally formed at the bottom of the inspection window, an airbag ring is fixedly connected to the inner side of the ring seat, an inflatable head is provided at the bottom of the airbag ring, and a clearing assembly is fixedly connected to the ring seat, and the clearing assembly includes two pieces of arc Two arc-shaped clearing plates are respectively located on the inner and outer sides of the inspection window. The fixing device includes a jacket. The jacket includes a shoulder strap and a chest strap. The shoulder strap and the chest strap are fixedly connected. The ring seat and the shoulder strap With sliding connection, the front side of the shoulder strap is fixedly connected with a support bar. It is used to solve the problems in the prior art that the weight of the protective mask is borne by the head of the staff, which is extremely prone to fatigue, and the staff's vision is narrow, and the inspection window is fogged, incomplete, scratched, etc., which affect the staff's sight.

Description

technical field [0001] The invention belongs to the field of wearable protective devices, in particular to a protective cover for rocket propellant operation. Background technique [0002] At present, the liquid rocket propellants used in my country are mainly nitro oxidants (27S nitric acid, dinitrogen tetroxide) and hydrazine fuels (unsymmetrical dimethylhydrazine, methylhydrazine and anhydrous hydrazine). Hydrazine-based fuels and nitro-oxidants have low boiling points, are volatile, and have strong corrosiveness and adsorption penetration. Therefore, when working with liquid propellants, in order to prevent poisoning, the staff need to use corresponding personal safety protective equipment. Personal protective equipment is divided into respiratory protective equipment and skin protective equipment, as well as protective masks and protective clothing. [0003] However, when the staff wore protective masks for propellant operations, they found the following problems: ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): A62B18/02A62B18/08F26B5/14B08B1/00
CPCA62B18/02A62B18/082A62B18/08F26B5/14B08B1/006
Inventor 屈明玥胡红芳郭宝石邓致荣王凯曾浩
Owner 中国人民解放军火箭军特色医学中心
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