Ignition device and fire control system
An ignition device and ignition control technology, which is applied in the field of rocket launch, can solve problems such as hidden safety hazards, misoperation of rockets, and real-time monitoring of the state of the ignition device that cannot be used, so as to avoid false triggering or misoperation, and improve the safety level.
Active Publication Date: 2022-04-08
BEIJING WATERTEK INFORMATION TECH
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Problems solved by technology
[0003] The ignition device in the related art realizes rocket communication, power supply, battery activation, ignition, and rocket launch through a power supply system, and cannot monitor the state of the ignition device in real time, which may easily cause rocket misoperation and cause safety hazards. Hidden danger
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[0022] In order to make the purpose, technical solution and advantages of the present invention more clear, the embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined arbitrarily with each other.
[0023] Unless otherwise defined, the technical terms or scientific terms disclosed and used in the embodiments of the present invention shall have the usual meanings understood by those with ordinary skill in the field of the present invention. "First", "second" and similar words used in the embodiments of the present invention do not indicate any order, quantity or importance, but are only used to distinguish different components. Words such as "comprising" or "comprising" always indicate that the elements or items listed before the word cover the elements or objects listed af...
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The application discloses an ignition device and a fire control system. The ignition device includes an ignition control circuit and an ignition channel, an activation channel, and a data loading channel respectively connected to the ignition control circuit. The ignition channel includes an ignition power supply system, and the ignition power supply system receives ignition control. The first power supply control signal of the circuit is to output or cut off the output power for the ignition channel; the activation channel includes activating the power supply system, and the activation power supply system receives the second power supply control signal of the ignition control circuit to output or cut off the output power for the activation channel; the data loading channel It includes a data loading power supply system, the data loading power supply system receives the third power supply control signal of the ignition control circuit, and outputs or cuts off the output power for the data loading channel. In this application, by using independent power supply systems in the ignition channel, activation channel and data loading channel respectively, problems such as false triggering or misoperation are avoided, and the safety level of the ignition device is improved.
Description
technical field [0001] Embodiments of the present invention relate to but are not limited to the technical field of rocket launching, and in particular relate to an ignition device and a fire control system. Background technique [0002] The fire control system is the equipment that controls the launch of rockets, mainly including fire control terminals, ignition devices, various sensors and power lights. The fire control system is connected to the rocket through the ignition device, and the ignition device realizes communication, power supply, battery activation, ignition and rocket launch of the rocket according to the control instructions of the fire control terminal. [0003] The ignition device in the related art realizes rocket communication, power supply, battery activation, ignition, and rocket launch through a power supply system, and cannot monitor the state of the ignition device in real time, which may easily cause rocket misoperation and cause safety hazards. H...
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IPC IPC(8): F41F1/00H02J4/00
CPCF41F1/00H02J4/00
Inventor 徐世文田国光张东辉赵平董烁
Owner BEIJING WATERTEK INFORMATION TECH