Aircraft landing gear and pitch trimmer assembly

1. An aircraft landing gear assembly comprising:

a bogie beam pivotally coupled to a support member, the bogie beam having a predetermined neutral position relative to the support member; and

a pitch trimmer assembly including a pitch trimmer actuator configured to exert a biasing force in a first direction and a bias force transmission assembly configured to receive the biasing force, wherein the bias force transmission assembly comprises a bias force transmission head at the free end of the pitch trimmer actuator and a pair of contact points on the bogie beam either side of the pivot axis of the bogie beam, the contact points being configured to receive the biasing force from the bias force transmission head and to define the predetermined neutral position of the bogie beam, wherein both contact points are in contact with the bias force transmission head when the bogie beam is in the predetermined neutral position.

2. The aircraft landing gear assembly according to claim 1 , wherein the contact points are asymmetrically shaped.

3. The aircraft landing gear assembly according to claim 1 , wherein the bias force transmission assembly comprises a toothed pinion gear configured to transmit a rotational force to the bogie beam and at least one toothed rack in engagement with the pinion gear, the toothed rack having a contact point configured to engage with the force transmission head of the pitch trimmer actuator.

4. The aircraft landing gear assembly according to claim 1 , wherein the support member comprises an oleo-pneumatic shock absorber having at least one fluid chamber, wherein the pitch trimmer actuator is integrally formed with the oleo-pneumatic shock absorber and is in fluid communication with the fluid chamber.

5. The aircraft landing gear assembly according to claim 1 , wherein the contact point of the bias force transmission assembly comprises a cam profile, the bias force transmission head being configured to contact the cam profile and transmit the bias force thereto, the cam profile defining the predetermined neutral position of the bogie beam.

6. The aircraft landing gear assembly according to claim 5 , wherein the bias force transmission head is rotatable relative to the cam profile.

7. The aircraft landing gear assembly according to claim 1 , wherein the pitch trimmer actuator comprises a single gland linear actuator.

8. The aircraft landing gear assembly according to claim 7 , wherein the pitch trimmer actuator comprises a hydraulic actuator.

9. The aircraft landing gear assembly according to claim 8 , wherein the pitch trimmer assembly includes a hydraulic accumulator.

10. An aircraft landing gear assembly comprising:

a bogie beam pivotally coupled to a support member;

a pitch trimmer assembly including a pitch trimmer actuator configured to exert a biasing force in a first direction to bias the bogie beam towards a predetermined neutral position relative to the support member;

a mounting bracket located on the support member to which a first end of the pitch trimmer actuator is pivotally coupled at a first pivot point; and

an attachment point located on the bogie beam to which a second end of the pitch trimmer actuator is pivotally coupled at a second pivot point,

wherein the first pivot point, second pivot point and a third pivot point about which the bogie beam is pivotally coupled to the support member are configured such that they are substantially aligned such that rotation of the bogie beam away from the neutral position results in compression of the pitch trimmer actuator in an opposite direction to the biasing force.