The Boeing Company
Combustion device test apparatus and method

Abstract:

A combustion device test apparatus including a combustion device, a holding station configured to hold the combustion device, a fuel supply conduit, and a pressure wave fuse coupling the fuel supply conduit to the combustion device, the pressure wave fuse being frictionally coupled to one or more of the combustion device and the fuel supply conduit at a frictional coupling such that the pressure wave fuse is configured to disengage one or more of the combustion device and the fuel supply conduit at the frictional coupling upon traversal of a flame front pressure wave through the pressure wave fuse.