Test method for indirect igniter for aeroengine

The invention relates to a test method for an indirect igniter for an aeroengine. According to the test method, by installing and debugging a testing device, a test content is set, a judgment standard of a test of the indirect igniter is normalized, the qualification criterions of the indirect igniter are put forward according to the ignition requirements in a main combustion chamber of the engine, so that the test method is practical and efficient and can completely meet the ground test requirement for the indirect igniter. According to the test method, in the test process, an ignition command and the time sequence requirement are completely simulated, and the variations of various states of the engine from the ground to high altitude are simulated; and in a singleton state, the work reliability of the indirect igniter on the engine and the restarting reliability of the engine in the air are ensured.