US 12,252,256 B2
Discharge system
Tarkan Turnacilar, Kahramankazan/Ankara (TR); Okan Erol, Kahramankazan/Ankara (TR); and Halit Oruc, Kahramankazan/Ankara (TR)
Assigned to TUSAS—TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI, Ankara (TR)
Appl. No. 18/695,743
Filed by TUSAS—TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI, Kahramankazan/Ankara (TR)
PCT Filed Sep. 20, 2022, PCT No. PCT/TR2022/051017
§ 371(c)(1), (2) Date Mar. 26, 2024,
PCT Pub. No. WO2023/055322, PCT Pub. Date Apr. 6, 2023.
Claims priority of application No. 2021/05265 (TR), filed on Sep. 20, 2022.
Prior Publication US 2024/0391594 A1, Nov. 28, 2024
Int. Cl. B64D 15/10 (2006.01)
CPC B64D 15/10 (2013.01) 14 Claims
OG exemplary drawing
 
1. A discharge system (1) comprising:
a body (2) which is located on an air vehicle;
at least one wing (3) extending outward from the body (2), which comes into contact with air to provide a lift force to the body (2);
a first cover (4) in a skirt form surrounding the at least one wing (3), wherein a first end of the first cover (4) is connected to the body (2), and a second end of the first cover (4) extends outward from the body (2) so as to have a distance with the wing (3);
an opening (A) which is located between the first cover (4) and the wing (3), thus directing a fluid (F) on the wing (3) between the wing (3) and the body (2); and
a discharge line (5) located on the body (2) facing the opening (A), allowing the fluid (F) directed through the opening (A) to be removed from the wing (3).