Aircraft landing gear assembly
View Patent ↗An aircraft landing gear assembly comprises a four bar linkage arranged to be pivotably attached to an aircraft fuselage and movable between a deployed position and a retracted position, wherein when in the retracted position at least a first portion of the landing gear assembly is housed within a wing at the aircraft.
1. An aircraft landing gear assembly, comprising:
a landing gear leg,
a main arm pivotably attached at a first end to the landing gear leg and arranged to be pivotably attached at a second end to an aircraft fuselage,
a side brace pivotably attached at a first end to the landing gear leg and arranged to be pivotably attached at a second end to the aircraft fuselage, wherein the landing gear leg, the main arm, the side brace, and the aircraft fuselage form a four bar linkage pivotably attached to the aircraft fuselage and movable between a deployed position and a retracted position, wherein at least a first portion of said landing gear assembly is housed within a wing of said aircraft when in the retracted position.
2. An aircraft landing gear assembly according to claim 1 , wherein at least a second portion of the landing gear assembly is housed within the aircraft fuselage when in the retracted position.
3. An aircraft landing gear assembly according to claim 1 , wherein a greater part of the main arm is housed within the aircraft wing when in said retracted position.
4. An aircraft landing gear assembly according to claim 1 , wherein the landing gear leg is arranged to have at least one landing wheel mounted thereon and wherein when the landing gear assembly is in the retracted position a greater part of the landing wheel is housed within the aircraft fuselage.
5. An aircraft landing gear assembly according to claim 1 , further comprising a retraction actuator connected between the side brace and the aircraft fuselage.
6. An aircraft landing gear assembly according to claim 1 further comprising a folding stay assembly pivotably attached to the main arm and the aircraft fuselage and arranged to brace the landing gear assembly when the assembly is in the deployed position.
7. An aircraft landing gear assembly according to claim 1 , wherein the assembly is arranged to be pivotably attached to the aircraft fuselage by one or more revolute joints.
8. In combination, an aircraft and a landing gear assembly, wherein said landing gear assembly further comprises
a landing gear leg,
a main arm pivotably attached at a first end to the landing gear leg and arranged to be pivotably attached at a second end to an aircraft fuselage,
a side brace pivotably attached at a first end to the landing gear leg and arranged to be pivotably attached at a second end to the aircraft fuselage, wherein the landing gear leg, the main arm, the side brace, and the aircraft fuselage form a four bar linkage pivotably attached to the aircraft fuselage and movable between a deployed position and a retracted position, wherein at least a first portion of said landing gear assembly is housed within a wing of said aircraft when in the retracted position.