ANTI-AIRCRAFT MISSILES AND MISSILE LAUNCHERS INSPECTION METHOD Russian patent published in 2018 - IPC F42B35/00 

FIELD: military equipment.

SUBSTANCE: invention relates to defense equipment and, in particular, to the guided anti-aircraft missiles and launchers electrical parameters integrated monitoring means. Verification method consists in the fact that before checking the electrical parameters, the device units to be tested are connected according to the appropriate arrangement. For the check the device self-test mode is performed. After the positive result obtaining, the device units to be tested are connected according to the arrangement with connection of the actually monitored article, and the monitored article electrical system parameters automated monitoring mode is performed. Visual information about the test results is displayed. After completion of the missile system combat equipment, the missile and the launch mechanism (LM), preparation for the maintenance, the connection arrangement assembly during the TCE self-test performance, setting the PC into operating position, loading the operating system, launching the TCE operation program, selecting the verification mode, starting the verification process, which is accompanied by the verification sequence displaying with the number indication, name of the monitored parameter and its measurement result, the sound signal reception and displaying on the screen a line about the need to perform a manual operation. Message to the operator at the external workplace, with the help of an intercom, about the need to perform a manual operation and after it is completion, continuation of the verification process. At the end of the test, the sound signal reception and displaying the “GOOD” test result on the screen. Next, performing the missile system LM functioning check in a similar manner. During the test, performing the sound presence in the checked LM phone periodic listening. Next, performing the missile system missile operation check in a similar manner. At that, after the TCE operation program launching, installing the missile and the target simulator, the tested missile attachment to the connectors, selecting the test mode, the verification process starting is accompanied by the verification process with indication of the number, monitored parameter name and its test result. During the test, listening to the presence of the gyroscope rotating rotor sound, the tested missile rudders operation, the indicators glow during the manual operation. Obtaining the “FAILURE” result in any type of tests indicates the article being inspected malfunction; after the checks completion, the MCP tear-down is performed.

EFFECT: technical result consists in the mobile control post checking method formation, providing the automated, quantitative assessment of finding the article parameters values within the specified limits, indication of the verification process completion with a statement of its result and the ability to view the obtained parameter values on the PC screen.

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