Rocket engine torch ignition remote control instruction end control method and electronic equipment
A rocket engine and control method technology, applied to rocket engine devices, mechanical equipment, machines/engines, etc., can solve problems such as repeated development, poor portability, and poor reliability
Active Publication Date: 2021-12-07
江苏深蓝航天有限公司
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Problems solved by technology
The traditional engine flare ignition solution is generally designed based on the Microsoft development environment of the Windows platform, which has poor reliability, poor portability, and will cause repeated development.
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[0019] The embodiments of the present invention will be further described in detail below in conjunction with the drawings and implementation methods. It should be understood that the specific implementation manners described here are only used to explain relevant content, rather than to limit the embodiments of the present invention. It should also be noted that, for ease of description, only parts related to the embodiments of the present invention are shown in the drawings.
[0020] It should be noted that, in the case of no conflict, implementation manners and features in the implementation manners in the embodiments of the present invention may be combined with each other. Embodiments of the present invention will be described in detail below with reference to the drawings and in combination with implementation manners.
[0021] It should be noted that the numbering of the steps in the text is only for the convenience of explanation of the specific embodiments, and does ...
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The embodiment of the invention provides a rocket engine torch ignition remote control instruction end control method and electronic equipment. The remote control instruction end control method comprises the steps that in response to a starting instruction, a remote control instruction end sends an initial detection instruction to a control end; in response to a return command returned by the control end, the remote control instruction end executes interface display and prompts a user to carry out time sequence parameter binding or not; in response to the time sequence parameter binding instruction, the remote control instruction end reads xml configuration files to perform item configuration, and a configuration item corresponding to the xml configuration files is formed; the remote control instruction end sends a control instruction corresponding to the configuration item to the control end; and the remote control instruction end receives the periodic time sequence data returned by the processing control end. Configuration items are defined by configuring the xml configuration files, the configuration items can be tested according to service requirements, and the problems that traditional engine torch ignition is frequently changed, and development is repeated are solved.
Description
technical field [0001] The invention relates to the technical field of liquid carrier rocket propulsion systems, in particular to a method for controlling a rocket engine torch ignition remote control command end and electronic equipment. Background technique [0002] At present, all liquid rocket engines in service in China use gas turbine pump devices as the propellant supply system. There is no substantive research and engineering realization of the application of electric pump devices on liquid rockets in China. It is suitable for torch ignition of liquid rockets with variable thrust electric engines. The scenes are also in the laboratory. The traditional engine flare ignition solution is generally designed based on the Microsoft development environment of the Windows platform, which has poor reliability, poor portability, and will cause repeated development. Contents of the invention [0003] In order to solve at least one of the above technical problems, an embodime...
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IPC IPC(8): F02K9/95
CPCF02K9/95Y02P90/02
Inventor 钱清华霍亮
Owner 江苏深蓝航天有限公司