Landing flap drive system
View Patent ↗A landing flap drive system, in one example, includes a first drive motor for operating a landing flap. In this arrangement, the landing flap drive system is integrated in a track of the landing flap such that final assembly and integration of the system are facilitated to a significant extent.
1. A track for an aircraft having a wing and a landing flap, the track comprising a track structure, a first attachment region coupled to the track structure, a second attachment region, and a track-integrated landing flap drive system integrated in the track structure and coupled to the second attachment region, wherein the first attachment region attaches the track to the wing of the aircraft, when the track is installed on the aircraft, and the track-integrated landing flap drive system is integrated within the track without separate structural attachment to the wing, such that the track-integrated landing flap drive system is attached to the wing as a unit with the track, when the track is installed on the aircraft, and the track-integrated landing flap drive system comprises:
a track-integrated first drive motor;
a track-integrated actuator coupled to the second attachment region, the second attachment region coupling the landing flap of the aircraft to the track-integrated actuator, when the track is installed on the aircraft, and when the track is installed on the aircraft, the track integrated actuator couples the first drive motor and the landing flap, wherein the landing flap is movably coupled to the wing of the aircraft; and
track-integrated motor control electronics electrically coupling the first drive motor of the track-integrated landing flap drive system to the aircraft, wherein the track-integrated motor control electronics synchronize operation of the track-integrated first drive motor and a second independent drive motor of a second track without mechanical coupling between the track-integrated first drive motor and the second drive motor when the track is installed on the aircraft.
2. The track of claim 1 , further comprising:
a step-down gear arrangement for reducing an operation speed of the landing flap.
3. The track of claim 1 , further comprising:
a brake device for setting the position of the landing flap.
4. The track of claim 1 , further comprising:
a safety load path to ensure structural integrity;
wherein the safety load path is capable of holding the landing flap in the case of structural failure.
5. The track of claim 1 , wherein the track-integrated motor control electronics comprise:
a first interface for connecting the landing flap drive system to an energy supply;
a second interface for connecting the landing flap drive system to a signal line for controlling the landing flap drive system.
6. The track of claim 1 , wherein the first drive motor is an electromechanical motor.
7. An aircraft with a track of claim 1 .
8. The track of claim 1 , wherein the actuator is self braking.
9. The track of claim 8 , wherein the actuator is a fail-safe spindle drive.
10. The track of claim 1 , wherein the track-integrated motor control electronics of the track-integrated landing flap drive system of the track are capable of synchronizing operation of the track-integrated first drive motor with the second independent drive motor, when the track is installed as a unit on the aircraft by attaching the first attachment region to the wing, coupling the second attachment region to the landing flap and connecting the track-integrated motor control electronics to an electrical supply line and signal lines of the aircraft, without any mechanical lead-through in a structural fuselage of the aircraft for the landing flap drive system.
11. The track of claim 1 , wherein the actuator is arranged inside the track.