Patent ID: 7013651

Claim:
A gas turbine engine comprising: an air-cooled device having: an outer periphery; a mounting flange; and a cooling air outlet, wherein the mounting flange and the cooling air outlet are disposed adjacent one another and wherein the mounting flange and a cooling air outlet are radially inward of the outer periphery of the air-cooled device, the mounting flange being spaced a distance from a remainder of the air-cooled device; a mount on the engine, the mount adapted to connect with the mounting flange radially inward of the outer periphery of the air-cooled device, wherein a peripheral recess is defined relative to the outer periphery of the device when the mount and mounting flange are connected; a securing assembly adapted to connect the mounting flange to the mount; a cooling air exhaust collection shroud adapted to surround and substantially cover the peripheral recess, the shroud having an air discharge outlet communicating with the cooling air outlet of the air-cooled device, the shroud having a periphery generally aligned with the outer periphery of the air-cooled device.