Engine compartment flammable fluid drainage system
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.
1. 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: a funnel member having a top opening and a bottom opening, the funnel member adapted to receive fluid in the top opening and direct the fluid to an external drain line through the bottom opening; a drain shield circumscribing the top end of the funnel member and extending only vertically therefrom, the drain shield configured to direct airflow away from the funnel member; a plurality of shield openings disposed in the drain shield such that the fluid can enter the funnel member therethrough; and a deck flange disposed substantially around the top opening of the funnel member, the deck flange having a plurality of flange openings configured so that each of the shield openings extend into one of the flange openings, such that the fluid can exit through the funnel member via the flange openings unimpeded by the deck flange.
2. The fluid drainage apparatus of claim 1 , wherein the drain shield partially circumscribes the top end of the funnel member.
3. The fluid drainage apparatus of claim 1 , wherein the apparatus is made of a metal.
4. The fluid drainage apparatus of claim 1 , wherein the apparatus is made of a metal alloy.
5. The fluid drainage apparatus of claim 1 , wherein the flange opening is tapered.
6. The fluid drainage apparatus of claim 1 , wherein a top portion of the drain shield partially overhangs the top opening of the funnel member.
7. 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: a cooling inlet adapted to direct an airflow throughout an engine compartment having an engine deck; an internal drain line for directing a fluid toward an external drain line; and a fluid drainage apparatus, comprising: a funnel member having a top opening and a bottom opening, the funnel member adapted to receive the fluid in the top opening and direct the fluid to the external drain line through the bottom opening; a drain shield coupled to the funnel member and extending only vertically therefrom, the drain shield adapted to shield the fluid from airflow; and a plurality of shield openings disposed in the drain shield such that the fluid can exit through the funnel member from the engine deck.
8. The fluid drainage system of claim 7 , further comprising a deck flange disposed substantially around the top opening of the funnel member, the deck flange having a plurality of flange openings configured so that each of the shield openings extend into one of the flange openings, such that the fluid can exit through the funnel member via the flange openings unimpeded by the deck flange.
9. The fluid drainage system of claim 8 , wherein the flange opening is tapered.
10. The fluid drainage system of claim 7 , further comprising a rubber grommet disposed around the internal drain line.
11. The fluid drainage system of claim 7 , further comprising a flexible tube cover disposed around the internal drain line.
12. The fluid drainage system of claim 11 , wherein the flexible tube cover extends from the internal drain line to the top opening of the funnel member.
13. The fluid drainage system of claim 7 , wherein the apparatus is made of a metal.
14. The fluid drainage system of claim 7 , wherein the apparatus is made of a metal alloy.
15. The fluid drainage apparatus of claim 7 , wherein the drain shield partially circumscribes the top end of the funnel member.
16. 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: a cooling inlet adapted to direct an airflow in an engine compartment having an engine deck; an engine inlet screen adapted to protect an engine from debris and allow the airflow to access the engine; an internal drain line for directing a fluid away from the engine; a drain hole coupled to an external drain line, the external drain line adapted to direct the fluid out of the engine compartment; and an inlet shield coupled to the engine deck and positioned shield the fluid exiting the internal drain line from the airflow, comprising: a funnel member having a top opening and a bottom opening, the funnel member adapted to receive the fluid in the top opening and direct the fluid to the external drain line through the bottom opening; a drain shield coupled to the funnel member and extending only vertically therefrom, the drain shield adapted to shield the fluid from airflow; and a plurality of shield openings disposed in the drain shield such that the fluid can exit through the funnel member from the engine deck.
17. The inlet shield system of claim 16 , wherein the inlet shield further includes an inlet opening disposed in the inlet shield such that the fluid can enter the drain hole therethrough.
18. The inlet shield system of claim 16 , further comprising a rubber grommet disposed around the internal drain line.
19. The inlet shield system of claim 16 , further comprising a flexible tube cover disposed around the internal drain line.
20. The inlet shield system of claim 16 , wherein the inlet shield partially circumscribes the drain hole.