US 12,344,367 B2
Adjustable landing gear
Burhan Sahin, Ankara (TR)
Assigned to Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi, Kahramankazan (TR)
Appl. No. 18/724,726
Filed by Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi, Ankara (TR)
PCT Filed Nov. 9, 2022, PCT No. PCT/TR2022/051262
§ 371(c)(1), (2) Date Jun. 27, 2024,
PCT Pub. No. WO2023/129006, PCT Pub. Date Jul. 6, 2023.
Claims priority of application No. 2021/021414 (TR), filed on Dec. 28, 2021.
Prior Publication US 2025/0066016 A1, Feb. 27, 2025
Int. Cl. B64C 25/00 (2006.01); B64C 25/26 (2006.01); B64C 25/32 (2006.01)
CPC B64C 25/26 (2013.01) [B64C 25/32 (2013.01); B64C 2025/325 (2013.01)] 12 Claims
OG exemplary drawing
 
1. An adjustable landing gear provided on an air vehicle having a fuselage, the landing gear comprising:
at least a first mount configured to move along a longitudinal direction of the first mount, and which carries the air vehicle by contacting the ground when the air vehicle lands;
at least a second mount fixed on the fuselage;
the landing gear configured to have: an open position (I) in which the first mount extends out of the fuselage and carries the air vehicle; and a closed position (II), wherein the first mount is moved in the fuselage to be brought from the open position (I) to the closed position (II);
at least one motor that moves the first mount between the open position (I) and the closed position (II),
at least one rack gear located on the second mount, which enables the first mount to move from the open position (I) to the closed position (II) or from the closed position (II) to the open position (I) by moving along the second mount and;
at least one pinion gear located on the first mount and acting on the rackgear, thus enabling the first mount to move on the second mount;
wherein the motor is located on the first mount and enables the pinion gear to act on the at least one rack gear.