The invention discloses an aircraft
braking system dynamic
load spectrum integration test method. According to actual lifting force characteristics of an aircraft during landing, a dynamic
load spectrum of aircraft wheel loads on the speed of the aircraft can be established; in a
braking system integration test, the aircraft wheel loads are regulated in real time according to the dynamic
load spectrum, and a
braking system dynamic integration test is conducted. In the aircraft braking
system dynamic integration test, accurate
simulation of the actual lifting force characteristics of the aircraft during landing is realized by means of dynamic regulation of the aircraft wheel loads, and consistency between in-
plant test conditions and external-field actual working conditions is improved. By means of the aircraft braking
system dynamic load spectrum integration test method, performance tests can be conducted on braking systems of various models of aircrafts more strictly, accuracy and the
degree of confidence of braking
system test results are increased, as a result, the number of times of test gliding and test flights for installation of the braking systems can be greatly reduced, a large amount of expenditure is saved, and the
technical risk is lowered. Meanwhile, the aircraft braking system dynamic load spectrum integration test method can also provide accurate and comprehensive
test data for take-off and landing of the aircrafts under complicated meteorological conditions, and therefore safety and reliability of aircraft braking are improved.