Housing for aircraft mounted components
A traffic collision avoidance system (TCAS) device is provided. The device includes a radome having an antenna. A chassis is bonded to said radome about a periphery by a skirt layer. A housing is adhesively bonded to the radome, the skirt layer and the chassis. The housing has a substantially flat bottom portion with a wall extended about a periphery, the wall forming a lap joint with the chassis and radome.
1. A method of producing a device that will be mounted to an exterior of an aircraft comprising:
receiving an assembly having a radome, a chassis mounted to one side of the radome and a skirt member;
forming a first flat housing layer having a first end, a second end, a first side and a second side;
placing the assembly onto the first flat housing layer;
bending the first end, the second end, the first side and the second side about the assembly to form a housing, the housing being arranged in a lap joint arrangement with the radome and the chassis; and,
curing the housing.
2. The method of claim 1 further comprising:
forming a second flat housing layer having a third end, a fourth end, a third side and a fourth side; and,
wherein the housing is formed by bending the second flat housing layer around the first flat housing layer after the first flat housing layer is bent around the assembly.
3. The method of claim 2 further comprising:
determining the location of voids in the assembly;
forming holes adjacent the voids;
drying the assembly; and
inserting epoxy into the holes prior to forming the housing.
4. The method of claim 3 wherein the first end and the second end each have a first plurality of darts.
5. The method of claim 4 wherein the third end and the fourth end each have a second plurality of darts.
6. The method of claim 5 wherein the first plurality of darts and the second plurality of darts are positioned in a non-overlapping arrangement when bent around the assembly.