Method for mounting an aircraft component and aircraft assembly
A method for mounting an aircraft component, which in the mounted state is movable between a first and a second operating position and is taken up in its first operating position in a mounting area, comprises the measuring of the mounting area, in order to obtain data characteristic of the shape and/or the dimensions of the mounting area. The data characteristic of the shape and/or the dimensions of the mounting area are projected onto the aircraft component arranged in its second operating position. Finally, the aircraft component arranged in its second operating position is adjusted with reference to the projection of the data characteristic of the shape and/or the dimensions of the mounting area.
1. A method for mounting an aircraft component on an aircraft, wherein in a mounted state the aircraft component is movable between a first operating position and a second operating position and wherein in the second operating position the aircraft component is mounted on the aircraft and extended from a mounting area of the aircraft and in the first operating position the aircraft component is mounted on the aircraft and taken up and received within the mounting area, wherein the method comprises:
measuring the mounting area, in order to obtain data characteristic of at least one of the shape and the dimensions of the mounting area;
projecting the data characteristic of the at least one of the shape and the dimensions of the mounting area onto the aircraft component arranged in the second operating position; and
adjusting the aircraft component when arranged in the second operating position with reference to the projection of the data characteristic of the at least one of the shape and the dimensions of the mounting area.
2. A method according to claim 1 , wherein the mounting area is measured by means of a laser measurement method.
3. A method according to claim 1 , wherein at least one of points and lines are projected as the data onto the aircraft component arranged in the second operating position.
4. A method according to claim 1 , wherein the aircraft component is a component of an aircraft landing gear.
5. A method according to claim 1 , wherein, when adjusting the aircraft component arranged in its second operating position, a first guide device provided on the aircraft component interacts with a complementary second guide device, which is attached to a supporting component provided for connection to the aircraft component.
6. A method according to claim 5 , wherein the first and the second guide devices comprise a guide rail and a guide element.
7. A method according to claim 1 , wherein the projection of the data characteristic of the shape of the mounting area is created by means of a laser projection method.
8. A method according to claim 4 , wherein the aircraft component comprises at least one of a landing gear fairing and a landing gear door.
9. A method according to claim 6 , wherein the guide element is in the shape of a mushroom head, provided for take-up in the guide rail.
10. A method according to claim 1 , wherein the projection of the data characteristic of the shape of the mounting area comprises creating a laser projection based on a representational function dependent on a known movement path of the aircraft component between the first operating position and the second operating position.
11. A method according to claim 1 , wherein, in the mounted position, the aircraft component is movably mounted to the aircraft.