Bogie beam angle sensor
A bogie beam sensor may include a bracket and a target arm pivotably coupled to the bracket. The bracket may be coupled to a bogie beam. A sensor may be coupled to the bracket, and a target may be coupled to the target arm. A drive link may be coupled to the target arm and a piston. In response to the bogie beam pivoting with respect to the piston, the drive link may cause the target arm to rotate with respect to the bogie beam. The sensor may detect movement of the target on the target arm, and an angular position of the bogie beam may be determined based on the position of the target.
1. A bogie beam sensor comprising:
a bracket non-rotatably coupled to a bogie beam;
a sensor coupled to the bracket, wherein the sensor is configured to detect an angular position of the bogie beam relative to a piston;
a target arm coupled to the bracket;
a target coupled to the target arm; and
a drive link, wherein the drive link is coupled to the target arm and wherein the drive link is coupled to the piston.
2. The bogie beam sensor of claim 1 , wherein the target arm is configured to pivot relative to the bracket.
3. The bogie beam sensor of claim 1 , wherein the sensor comprises a proximity sensor.
4. The bogie beam sensor of claim 1 , wherein the bracket is coupled to the bogie beam via a forward lug and an aft lug.
5. The bogie beam sensor of claim 4 , wherein the aft lug comprises a sliding joint.
6. The bogie beam sensor of claim 1 , wherein the drive link comprises a spherical bearing.
7. The bogie beam sensor of claim 1 , wherein the target comprises a nose up target and a nose down target.
8. The bogie beam sensor of claim 7 , wherein the nose up target and the nose down target are non-parallel.
9. The bogie beam sensor of claim 1 , wherein the target is offset relative to the sensor in a neutral position.
10. The bogie beam sensor of claim 1 , wherein the bogie beam sensor in configured to detect a change in a bogie beam position of less than or equal to +/− 1.1 degrees.
11. An aircraft landing gear comprising;
a piston;
a bogie beam coupled to the piston, wherein the bogie beam is configured to pivot relative to the piston;
a target arm pivotably coupled to a bracket, wherein the bracket is non-rotatably coupled to the bogie beam;
a sensor coupled to the bogie beam, wherein the sensor is configured to detect an angular position of the bogie beam relative to a piston; and
a drive link coupled to the piston and the target arm.
12. The aircraft landing gear of claim 11 , wherein the drive link is configured to pivot the target arm with respect to the bogie beam in response to the bogie beam pivoting relative to the piston.
13. The aircraft landing gear of claim 11 , further comprising a target coupled to the target arm.
14. The aircraft landing gear of claim 11 , wherein the sensor is configured to detect a rotation of the bogie beam. of less than or equal to 1.1 degrees.
15. The aircraft landing gear of claim 11 , wherein the drive link is coupled to the target arm via a spherical bearing.