OVER-SPEED, ROUGH LOADS AND HARD LANDING DETECTION SYSTEM

• US 20100281967A1
• Filed: 05/05/2009
• Published: 11/11/2010
• Est. Priority Date: 05/05/2009
• Status: Active Grant

• Current Assignee: Goodrich Corporation (Rtx Corporation)
• Original Assignee: Goodrich Corporation (Rtx Corporation)
• Inventors: Cahill, Eric D.
• Granted Patent: US 7,946,165 B2
• Time in Patent Office: Days
• US Class Current: 73/146
• CPC Class Codes: B64C 25/00 Alighting gear air-cushion alighting gear B60V3/08
• CPC Class Codes: B64D 2045/008 Devices for detecting or indicating hard landing
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00

Abstract

A system, apparatus and method provide a means for indicating an overload condition has occurred during aircraft operation. The occurrence of an overload condition is automatically determined and an indication output thereof. Based on the indication received by the cockpit, avionics, maintenance, etc., further action may be taken to correct the effects of the overload condition on the tires and/or landing gear.

Claims

1. A controller for indicating an overload condition has occurred during aircraft operation for at least one aircraft tire, wheel and/or at least one aircraft landing gear, said controller configured to:

receive at least one input indicative of at least one of a load placed on the at least one tire and/or at least one landing gear or an angular velocity of the at least one tire;

determine, based on the at least one input, if the at least one tire or landing gear corresponding to the at least one tire has exceeded a prespecified threshold; and

based on the determination, provide an output indicative an overload condition of the at least one tire or the landing gear corresponding to the at least one tire.

2. The controller according to claim 1, wherein the output corresponds to at least one of a tire overspeed condition, a tire overload condition, or a landing gear overload condition.

3. The controller according to claim 1, wherein the threshold is a velocity threshold, and the controller in order to determine if the at least one tire has exceeded the prespecified threshold, is configured to:

compare the angular velocity of the at least one tire to the prespecified threshold; and

conclude a tire overspeed condition has occurred if the angular velocity of the at least one tire exceeds the prespecified threshold.

4. The controller according to claim 1, wherein the controller is further configured to:

determine a first angular velocity of the at least one tire during a first time period after aircraft touchdown;

determine a second angular velocity of the at least one tire during a second time period after aircraft touchdown, the second time period occurring subsequent to the first time period; and

calculate a radius of the at least one tire during the first time period based on the first angular velocity and the second angular velocity.

5. The controller according to claim 4, wherein the controller, in order to determine the load placed on the at least one tire, is configured to use the calculated tire radius and a deflection to load curve corresponding to the at least one tire to approximate the load on the at least one tire.

6. The controller according to claim 5, wherein the threshold is a load threshold, and wherein the controller in order to determine if the at least one tire or landing gear has exceeded the prespecified threshold, is configured to:

compare the determined load placed on the at least one tire to the prespecified threshold; and

conclude an overload condition has occurred for the at least one tire and/or landing gear corresponding to the at least one tire if the load on the at least one tire exceeds the prespecified threshold.

7. The controller according to claim 1, wherein the controller is further configured to calculate the rate of wheel spinup based on the velocity data and using the calculated wheel spinup and wheel inertia, the controller is further configured to determine a coefficient of friction of a runaway surface.

8. The controller according to claim 7, wherein the controller is further configured to use the determined coefficient of friction to determine runway conditions.

9. The controller according to claim 1, wherein the threshold is a velocity threshold, and wherein the controller, to determine if the at least one tire or landing gear has exceeded the prespecified threshold, is configured to:

use an accelerometer to determine a rate of vertical descent of an aircraft at a time of aircraft touchdown;

compare the determined rate of vertical descent to the prespecified threshold; and

conclude a hard landing condition has occurred for the at least one tire and/or landing gear corresponding to the at least one tire if the rate of vertical descent of the aircraft exceeds the prespecified threshold.

10. An aircraft landing gear system for indicating an overload condition comprising:

the controller according to claim 1, the controller having a plurality of inputs;

at least one aircraft landing gear and at least one tire associated with the at least one landing gear; and

a wheel speed sensor operatively coupled to one of the plurality of inputs, wherein the at least one aircraft tire comprises a wheel speed sensor configured to provide data indicative of a velocity of the at least one tire.

11. The aircraft landing gear system of claim 10, further comprising an accelerometer operatively coupled to one of the plurality of inputs, wherein the accelerometer is used to determine a hard landing.

12. A method of indicating an overload condition has occurred for at during aircraft operation for at least one aircraft tire, wheel and/or at least one aircraft landing gear, comprising:

determining at least one of a load placed on the at least one tire or an angular velocity of the at least one tire;

determining, based on at least one of the load or the angular velocity, if the at least one tire or landing gear corresponding to the at least one tire has exceeded a prespecified threshold; and

based on the determination, providing an output indicative of an overload condition of the at least one tire or the landing gear corresponding to the at least one tire.

13. The method according to claim 12, wherein the output corresponds to at least one of a tire overspeed condition, a tire overload condition, or a landing gear overload condition.

14. The method according to claim 12, wherein the threshold is a velocity threshold, and determining if the at least one tire has exceeded the prespecified threshold includes:

comparing the angular velocity of the at least one tire to the prespecified threshold; and

concluding a tire overspeed condition has occurred if the angular velocity of the at least one tire exceeds the prespecified threshold.

15. The method according to claim 12, further comprising:

determining a first angular velocity of the at least one tire during a first time period after aircraft touchdown;

determining a second angular velocity of the at least one tire during a second time period after aircraft touchdown, the second time period occurring subsequent to the first time period; and

calculating a radius of the at least one tire during the first time period based on the first angular velocity and the second angular velocity.

16. The method according to claim 15, wherein determining the load placed on the at least one tire comprises using the calculated tire radius and a deflection to load curve corresponding to the at least one tire to approximate the load on the at least one tire.

17. The method according to claim 16, wherein the threshold is a load threshold, and determining if the at least one tire or landing gear has exceeded the prespecified threshold includes:

comparing the determined load placed on the at least one tire to the prespecified threshold; and

concluding an overload condition has occurred for the at least one tire and/or landing gear corresponding to the at least one tire if the load on the at least one tire exceeds the prespecified threshold.

18. The method according to claim 12, further comprising:

calculating the rate of wheel spinup based on the velocity data; and

using the calculated wheel spinup and wheel inertia to determine a coefficient of friction of a runaway surface.

19. The method according to claim 18, further comprising using the determined coefficient of friction to determine runway conditions.

20. The method according to claim 12, wherein the threshold is a velocity threshold, and determining if the at least one tire or landing gear has exceeded the prespecified threshold includes:

using an accelerometer to determine a rate of vertical descent of an aircraft at a time of aircraft touchdown;

comparing the determined rate of vertical descent to the prespecified threshold; and

concluding a hard landing condition has occurred for the at least one tire and/or landing gear corresponding to the at least one tire if the rate of vertical descent of the aircraft exceeds the prespecified threshold.