Storage and supply device for rocket engine igniter
A rocket engine and supply device technology, applied to rocket engine devices, machines/engines, jet propulsion devices, etc., can solve problems such as inability to realize liquid supply management, inability to achieve gas-liquid isolation of igniting agent and pressurized gas, and inability to replace them
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[0031] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.
[0032] The structural composition of the present invention includes: shell assembly 1, metal bellows assembly 2, gas path isolation assembly 3, liquid path isolation assembly 4, gas path filling valve 5, liquid path filling valve 6, filter 7, gas path Redundant sealing joint 8 and redundant sealing joint 9 of liquid circuit.
[0033] The shell assembly 1 includes a shell column section 1-1, a gas path head 1-2, and a liq...
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