Engine compartment flammable fluid drainage system
AssigneeBell Helicopter Textron Inc.
InventorsThomas Dewey Parsons, Chris James Ludtke, Andrew Jordan Birkenheuer, Eric Christopher Terry
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AssigneeBell Helicopter Textron Inc.
InventorsThomas Dewey Parsons, Chris James Ludtke, Andrew Jordan Birkenheuer, Eric Christopher Terry
Estimating the term…
The present invention achieves technical advantages as an engine compartment drainage system that allows fluid on an engine deck to exit an engine compartment, while shielding fluid from airflow. A fluid drainage apparatus utilizes a funnel member to direct fluid to an external drain line. A drain shield circumscribes the top end of the funnel member and upwardly extending therefrom and directs airflow away from the funnel member. A plurality of deck holes are disposed in the drain shield, such that fluid on the deck can enter the funnel member and exit the engine compartment. A fluid drainage system, disposes the fluid drainage apparatus in an engine deck to allow fluid on the deck to enter a funnel member of the apparatus and direct it toward the external drain line.
An aircraft fluid drainage configured to allow fluid on an engine deck of an aircraft engine compartment to exit the compartment, while shielding airborne aircraft fluid from airflow, comprising:
An aircraft fluid drainage system configured to allow fluid on an engine deck of an aircraft engine compartment to exit the compartment, while shielding airborne aircraft fluid from airflow, comprising:
An aircraft inlet shield system configured to allow fluid on an engine deck of an aircraft engine compartment to exit the compartment, while shielding airborne aircraft fluid from airflow, comprising:
Dependencies are inferred from the claim text.