Patent ID: 11939076
Assignee: LOCKHEED MARTIN CORPORATION
Field: Transport (Mechanical engineering)
Classification: CPC B  F  A | IPC A  B  F

Claim 11:
12. An engine cooling system for an aircraft, comprising:
a fire resistant bulkhead having a forward wall and a lower wall coupled to the forward wall and angled with respect to the forward wall, the forward wall and the lower wall together defining an at least partially enclosed space sized to receive an engine therein;
a fluid conduit coupled at a proximal end of the fluid conduit to one of the forward wall or the lower wall and extending away from the at least partially enclosed space to a distal end of the fluid conduit;
a valve coupled to the proximal end of the fluid conduit proximate the fire resistant bulkhead and configured to control a flow of air through the fluid conduit; and
an air driver coupled to the distal end of the fluid conduit opposite the proximal end.