Apparatus and method for lowering and raising a trailer
A landing gear assembly includes a leg assembly, a gear assembly configured to telescopingly move a second leg portion with respect to a first leg portion, and a drive assembly including a gear arrangement configured to drive the drive shaft of the gear assembly at a high speed and low torque configuration and at a low speed and high torque configuration, an electric motor configured to drive the gear arrangement, and a controller configured to switch the gear arrangement from the high speed and low torque configuration to the low speed and high torque configuration in response to an increase in current draw by the electric motor as the second leg portion moves from a retracted to an extended position, and configured to maintain the gear arrangement in the high speed and low torque configuration as the second portion moves from the extended position toward the retracted position.
1. A landing gear assembly, comprising:
a leg assembly including a first leg portion and a second leg portion telescopingly engaging one another;
a gear assembly operably coupled to the first and second leg portions and configured to telescopingly move the second leg portion between fully retracted and fully extended positions with respect to the first leg portion, the gear assembly including an input shaft; and
a drive assembly coupled to the gear assembly and comprising:
a gear arrangement configured to drive the drive shaft of the gear assembly at a high speed and low torque configuration and at a low speed and high torque configuration where the high speed is greater than the low speed and the low torque is less than the high torque;
an electric motor configured to drive the gear arrangement; and
a controller configured to switch the gear arrangement from the high speed and low torque configuration to the low speed and high torque configuration in response to an increase in current draw by the electric motor as the second leg portion moves from the fully retracted position toward the fully extended position, and configured to maintain the gear arrangement in the high speed and low torque configuration as the second portion moves from an extended position toward the fully retracted position.
2. The landing gear assembly of claim 1 , further comprising:
a battery configured to provide power to the motor.
3. The landing gear assembly of claim 2 , wherein the battery includes a lithium battery.
4. The landing gear assembly of claim 1 , further comprising:
a sensor in communication with the controller and configured to sense relative movement of the second leg member with respect to the first leg member.
5. The landing gear assembly of claim 4 , further comprising:
a spindle operably coupling the second leg portion to the first leg portion such the second portion moves with respect the first leg portion as the spindle rotates, and wherein the sensor is configured to directly sense a rotation of the spindle.
6. The landing gear assembly of claim 1 , wherein the gear arrangement comprises a planetary gear arrangement.
7. The landing gear assembly of claim 1 , wherein the gear assembly is a single speed gear assembly.
8. The landing gear assembly of claim 1 , further comprising:
a spindle operably coupling the second leg portion to the first leg portion such the second portion moves with respect the first leg portion as the spindle rotates;
a first stop member attached to the second leg portion and configured to abut a lifting nut at the fully extended position of the second leg member with respect to the first leg member where the lifting nut is configured to travel along a length of the spindle; and
a second stop member attached to the second leg portion and configured to abut a bearing wall at the fully retracted position of the second leg member with respect to the first leg member.
9. A landing gear assembly, comprising:
a leg assembly including a first leg portion and a second leg portion, wherein the first and second leg portions of the leg assembly are telescopingly coupled with one another;
a gear assembly operably coupled to the first and second leg portions and configured to telescopingly move the second leg portion between a fully retracted position and a fully extended position with respect to the first leg portion; and
a drive assembly coupled to the gear assembly and comprising:
an electric motor configured operably coupled to the gear assembly;
a sensor configured to sense movement of an element of the leg assembly as the first leg member moves with respect to the second leg member; and
a controller operably coupled to the sensor and configured to calculate the relative position of the first leg member with respect to the second leg member based a signal received from the sensor, and configured to control the electric motor and limit movement of the first leg member to the fully extended and/or the fully retracted position.
10. The landing gear assembly of claim 9 , wherein the element of the leg assembly includes a spindle operably coupling the second leg portion to the first leg portion such the second portion moves with respect the first leg portion as the spindle rotates, and wherein the sensor is configured to sense a rotation of the spindle.
11. The landing gear assembly of claim 10 , wherein the drive assembly further includes a gear arrangement configured to drive the gear assembly at a high speed and low torque configuration and at a low speed and high torque configuration where the high speed is greater than the low speed and the low torque is less than the high torque.
12. The landing gear assembly of claim 11 , wherein the gear arrangement comprises a planetary gear arrangement.
13. The landing gear assembly of claim 9 , wherein the controller is configured to change the configuration of the gear arrangement between the high speed and low torque configuration and the low speed and high torque configuration in response to an increase and/or decrease in current draw by the electric motor as the second leg portion moves from the fully retracted position to the fully extended position, and configured to maintain the gear arrangement in the high speed and low torque configuration as the second portion moves from an extended position to the fully retracted position.
14. The landing gear assembly of claim 9 , further comprising:
a battery configured to provide power to the motor.
15. The landing gear assembly of claim 14 , wherein the battery includes a lithium battery.
16. The landing gear assembly of claim 9 , wherein the gear assembly is a single speed gear assembly.
17. A landing gear assembly, comprising:
a leg assembly including a first leg portion and a second leg portion, wherein the first and second leg portions of the leg assembly telescopingly engage one another;
a gear assembly operably coupled to the first and second leg portions and configured to telescopingly move the second leg portion between retracted and extended positions with respect to the first leg portion; and
a drive assembly coupled to the gear assembly and comprising:
an electric motor configured to drive the gear arrangement; and
a controller configured to operate the motor in a first direction such that the second leg portion moves from the retracted position to the extended position and in a second direction such that the second leg portion moves from the extended position to the retracted position, wherein the controller limits movement of the motor in the first direction based on an increase in current draw from a first current amount to a second current amount and the controller limits movement of the motor in the first direction based on an increase in current draw from a third current amount to a fourth current amount, and wherein the fourth current amount is different than the second current amount.
18. The landing gear assembly of claim 17 , wherein the second current amount is greater than the first current amount, and the fourth current amount is greater than the third current amount.
19. The landing gear assembly of claim 17 , wherein the drive assembly further includes a gear arrangement configured to drive the gear assembly at a high speed and low torque configuration and at a low speed and high torque configuration where the high speed is greater than the low speed and the low torque is less than the high torque.
20. The landing gear assembly of claim 17 , further comprising:
a battery configured to provide power to the motor.