Method of managing a turning movement of an aircraft taxiing on the ground
US-9134730-B2 · Sep 15, 2015 · US
US11304262B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11304262-B2 |
| Application number | US-201716343801-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 8, 2017 |
| Priority date | Nov 11, 2016 |
| Publication date | Apr 12, 2022 |
| Grant date | Apr 12, 2022 |
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An apparatus for dissipating braking energy generated by the operation of a vehicle brake. The apparatus includes a heating element configured to receive electric current generated by operation of the vehicle brake, the heating element arranged in a chamber for containing liquid. The apparatus is configured such that liquid contained in the chamber is heated in response to operation of the vehicle brake.
Opening claim text (preview).
The invention claimed is: 1. An apparatus for dissipating braking energy generated by the operation of a vehicle brake, the apparatus comprising: a heating element configured to receive electric current generated by operation of the vehicle brake, a chamber configured to contain a fluid and the heating element immersed in a liquid phase of the fluid, wherein the chamber includes a liquid inlet for the liquid phase of the fluid and a vapor outlet for a vapor phase of the fluid, and wherein the chamber is configured to release the fluid from the chamber only in the vapor phase during a braking event of the vehicle brake, wherein the apparatus is configured such that the fluid in the liquid phase contained in the chamber is boiled to convert the fluid to the vapor phase in response to operation of the vehicle brake. 2. The apparatus according to claim 1 , comprising a pressure regulator configured to prevent vapor pressure in the chamber from exceeding a predetermined pressure during operation of the apparatus. 3. The apparatus according to claim 1 , comprising a liquid sensor configured to measure an amount of the liquid phase in the chamber, wherein a flow of the liquid phase through the liquid inlet is controlled based on a measured amount of the liquid phase in the chamber. 4. The apparatus according to claim 1 , comprising a temperature sensor configured to sense temperature of the fluid in the chamber, wherein the apparatus is configured to control a flow of the liquid phase through the liquid inlet in dependence on the temperature of the fluid in the chamber. 5. The apparatus according to claim 1 , wherein the apparatus is configured to control a flow of the liquid phase through the liquid inlet in dependence on a level of the electric current received by the heating element. 6. The apparatus according to claim 1 , further comprising a pump configured to control a flow of the liquid phase to the liquid inlet. 7. The apparatus according to claim 1 , wherein the vehicle brake is an electromagnetic brake. 8. An aircraft comprising an apparatus according to claim 1 . 9. An aircraft according to claim 8 , further comprising an electronic braking system. 10. A method of dissipating braking energy generated by the operation of a vehicle brake, the method comprising: converting braking energy generated by operation of a vehicle brake into an electric current; supplying the electric current to a heating element arranged in a chamber containing a liquid, wherein the chamber configured to contain a fluid and the heating element immersed in a liquid phase of the fluid, wherein the chamber includes a liquid inlet for receiving the liquid phase of the liquid and a vapor outlet for releasing a vapor phase of the liquid, and wherein the chamber is configured to release the fluid from the chamber only in the vapor phase during a braking event of the vehicle brake; and; boiling the liquid to generate vapor; and releasing the generated vapor from the chamber. 11. The method according to claim 10 , comprising: supplying a flow of liquid to the chamber; and regulating the flow of liquid to the chamber based on one or more of: a liquid volume in the chamber; a temperature in the chamber; and a level of the electric current supplied to the heating element. 12. An apparatus for dissipating braking energy generated by the operation of a vehicle brake, the apparatus comprising: a heating element configured to receive electric current generated by operation of the vehicle brake; a chamber configured to contain a fluid and the heating element immersed in a liquid phase of the fluid, wherein the chamber includes a liquid inlet for the liquid phase of the fluid and a vapor outlet for a vapor phase of the fluid, and wherein the chamber is configured to release the fluid from the chamber only in the vapor phase during a braking event of the vehicle brake, and a pressure regulator configured to prevent pressure in the chamber from exceeding a predetermined pressure during operation of the apparatus, wherein the predetermined pressure is in a range of 2 bar to 10 bar. 13. An apparatus for dissipating braking energy generated by the operation of a vehicle brake, the apparatus comprising: a heating element configured to receive electric current generated by operation of the vehicle brake; a chamber configured to contain a liquid and the heating element immersed in the liquid, wherein the chamber includes a liquid inlet for receiving the liquid and a vapor outlet for releasing a vapor phase of the liquid, and wherein the chamber is configured to release the fluid from the chamber only in the vapor phase during a braking event of the vehicle brake; and a controller configured to receive a signal and to control a flow of the liquid through the liquid inlet and into the chamber based on the received signal. 14. The apparatus according to claim 13 , wherein the controller is configured to alter the flow of the liquid phase in to the chamber if the received signal meets a predetermined criterion. 15. The apparatus according to claim 14 , wherein the received signal indicates an amount of the liquid phase in the chamber measured by the liquid sensor; the predetermined criterion is defined such that the predetermined criterion is met if a measured amount of the liquid phase in the chamber is less than a predetermined minimum amount; and the controller is configured to increase the flow of the liquid phase through the liquid inlet and into the chamber if the received signal meets the predetermined criterion. 16. The apparatus according to claim 14 : wherein the received signal indicates a temperature in the chamber measured by the temperature sensor; and the predetermined criterion is defined such that the predetermined criterion is met if a temperature in the chamber is outside of a predetermined temperature range. 17. The apparatus according to claim 16 , wherein the controller is configured to decrease the flow of the liquid phase into the chamber if the received signal indicates that the temperature in the chamber is less than a lower limit of the predetermined temperature range, and to increase the flow of the liquid phase into the chamber if the received signal indicates that the temperature in the chamber is greater than an upper limit of the predetermined temperature range. 18. The apparatus according to claim 14 , wherein the received signal indicates a pressure of the vapor phase in the chamber measured by a pressure sensor; and the predetermined criterion is defined such that the predetermined criterion is met if a pressure of the vapor phase in the chamber is outside of a predetermined pressure range. 19. The apparatus according to claim 18 , wherein the controller is configured to increase the flow of liquid into the chamber if the received signal indicates that the pressure in the chamber is less than a lower limit of the predetermined pressure range, and to decrease the flow of liquid into the chamber if the received signal indicates that the pressure in the chamber is greater than an upper limit of the predetermined pressure range. 20. The apparatus according to claim 13 , wherein the received signal comprises one or more of: data received from a user interface; and information relating to an operational parameter of the vehicle brake. 21. An aircraft comprising the apparatus according to claim 13 , wherein the controller is in an avionics system of the aircraft.
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