초록 ▼

The present invention relates to a tester, its use and a method for testing signal lines of a flight control system for a trimmable horizontal stabilizer (THS) motor of an aircraft. The tester comprises at least one test-relay (52, 54) to be connected with a relay socket of the flight control system

The present invention relates to a tester, its use and a method for testing signal lines of a flight control system for a trimmable horizontal stabilizer (THS) motor of an aircraft. The tester comprises at least one test-relay (52, 54) to be connected with a relay socket of the flight control system, when the signal lines of the flight control system are to be tested, and at least one indicator (60, 70, 80, 90) being electrically connected with the at least one test-relay (52, 54) for indicating whether a voltage being applied to the test-relay (52, 54) is equal to or larger than a predetermined voltage. The method according to the invention comprises the steps of connecting at least one test-relay (52, 54) of a tester (1), in place of the original relay, with the relay socket of the flight control system, applying a voltage to the at least one test-relay (52, 54) and determining whether a voltage being applied to the at least one test-relay (52, 54) is equal to or larger than a predetermined voltage.

대표청구항 ▼

1. Test arrangement for testing signal lines of a flight control system for a trimmable horizontal stabilizer motor of an aircraft, the flight control system including at least one relay inserted into a corresponding relay socket, the test arrangement comprising: a simulation system which during gro

1. Test arrangement for testing signal lines of a flight control system for a trimmable horizontal stabilizer motor of an aircraft, the flight control system including at least one relay inserted into a corresponding relay socket, the test arrangement comprising: a simulation system which during ground tests of the aircraft provides a control signal to the signal lines of the flight control system to be tested so as to simulate a predefined flight situation, anda tester including at least one test-relay, wherein the test relay is configured to be inserted into a relay socket of the flight control system to connect the test-relay to the relay socket in place of the relay of the flight control system, when the signal lines of the flight control system are to be tested, anda first indicator as well as a second indicator being electrically connected to the at least one test-relay, wherein the first indicator configured to indicate whether a voltage being applied to the at least one test-relay in response to a control signal provided by the simulation system is equal to or larger than a predetermined voltage, and the second indicator is configured to indicate whether the voltage is less than the predetermined voltage. 2. Test arrangement as claimed in claim 1, wherein the at least one test-relay comprises a first test-relay and a second test-relay to be connected with corresponding relay sockets of the flight control system, when the signal lines of the flight control system are to be tested, each of the first test-relay and the second test-relay being electrically connected with first and second indicators, respectively. 3. Test arrangement as claimed in claim 2, wherein each of the first indicators is electrically connected to driving contacts of the first and second test-relays, respectively, and wherein each of the second indicators is electrically connected to an armature contact of the first and second test-relays, respectively. 4. Test arrangement as claimed in claim 1, wherein each indicator outputs a visual signal. 5. Test arrangement as claimed in claim 1, wherein each indicator is a light emitting diode, and wherein the first and the second light emitting diodes emit light of a different colour. 6. Test arrangement as claimed in claim 1, wherein the predetermined voltage is 28 V. 7. Test arrangement as claimed in claim 1, wherein each test relay is connected to a test-relay plug which is to be inserted into a corresponding relay socket of the flight control system to be tested. 8. Method for testing signal lines of a flight control system for a trimmable horizontal stabilizer motor of an aircraft, the flight control system including at least one relay inserted into a corresponding relay socket, the method comprising the steps of: inserting a test-relay of a tester into a relay socket of the flight control system to connect the test-relay to the relay socket in place of the relay of the flight control system,providing a control signal of a simulation system to the signal lines of the flight control system to be tested so as to simulate a predefined flight situation, wherein a voltage is applied to the at least one test-relay in response to the control signal provided by the simulation system,determining whether the voltage being applied to the at least one test-relay is equal to or larger than a predetermined voltage or less than the predetermined voltage,activating a first indicator, if the voltage being applied to the at least one test-relay is equal to or larger than the predetermined voltage, andactivating a second indicator, if the voltage being applied to the at least one test-relay is less than the predetermined voltage. 9. Method according to claim 8, further comprising the step of:simultaneously determining whether voltages being applied to two test-relays which are connected to two corresponding serially connected relay sockets of the flight control system are equal to or larger than a predetermined voltage.