Braking system having electromechanical braking function and method for controlling the same
US-2016325724-A1 · Nov 10, 2016 · US
US10093291B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10093291-B2 |
| Application number | US-201715423174-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 2, 2017 |
| Priority date | Feb 2, 2017 |
| Publication date | Oct 9, 2018 |
| Grant date | Oct 9, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A hydraulic park brake system for an aircraft may include a hydraulic park brake controller having a processor and a tangible, non-transitory memory configured to communicate with the processor. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the processor, cause the hydraulic park brake system to perform various operations. Such operations may include receiving, by the processor, a hydraulic park brake condition, comparing, by the processor, the hydraulic park brake condition with a predetermined condition to yield comparison data, and determining, by the processor and based on the comparison data, a hydraulic park brake adjustment status. Such operations may further include generating, by the processor and based on the hydraulic park brake adjustment status, an adjustment command and transmitting, by the processor, the adjustment command to a hydraulic park brake of the aircraft.
Opening claim text (preview).
What is claimed is: 1. A hydraulic park brake system for an aircraft, the hydraulic park brake system comprising: a hydraulic park brake; a sensor coupled to the hydraulic park brake; a hydraulic park brake controller having a processor; and a tangible, non-transitory memory configured to communicate with the processor, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the hydraulic park brake system to perform operations comprising: receiving, by the processor, a hydraulic park brake condition, wherein receiving the hydraulic park brake condition comprises detecting, by the processor and via the sensor, the hydraulic park brake condition; comparing, by the processor, the hydraulic park brake condition with a predetermined condition to yield comparison data; and determining, by the processor and based on the comparison data, a hydraulic park brake adjustment status. 2. The hydraulic park brake system of claim 1 , wherein the sensor comprises a temperature sensor and the hydraulic park brake condition is a temperature of the hydraulic park brake. 3. The hydraulic park brake system of claim 1 , wherein the sensor comprises a pressure sensor and the hydraulic park brake condition is a hydraulic pressure of the hydraulic park brake. 4. The hydraulic park brake system of claim 1 , wherein the sensor comprises a force sensor and the hydraulic park brake condition is a magnitude of parking brake force of the hydraulic park brake. 5. The hydraulic park brake system of claim 1 , wherein the receiving the hydraulic park brake condition is performed in response to a passage of time of the aircraft being parked. 6. The hydraulic park brake system of claim 1 , wherein the receiving the hydraulic park brake condition is performed intermittently. 7. The hydraulic park brake system of claim 1 , wherein the determining the hydraulic park brake adjustment status is performed in response to a passage of time of the aircraft being parked. 8. The hydraulic park brake system of claim 1 , wherein the determining the hydraulic park brake adjustment status is performed intermittently. 9. The hydraulic park brake system of claim 1 , wherein the determining the hydraulic park brake adjustment status is performed in response to the comparison data comprising a threshold difference between the hydraulic park brake condition and the predetermined condition. 10. The hydraulic park brake system of claim 1 , wherein the operations further comprise transmitting the hydraulic park brake adjustment status to at least one of a brake control unit, a full authority digital engine control, and an engine-indicating and crew-alerting system. 11. The hydraulic park brake system of claim 1 , wherein the operations further comprise: generating, by the processor and based on the hydraulic park brake adjustment status, an adjustment command; and transmitting, by the processor, the adjustment command to a hydraulic park brake of the aircraft. 12. The hydraulic park brake system of claim 11 , wherein the adjustment command comprises instructions to increase a parking brake force of the hydraulic park brake. 13. The hydraulic park brake system of claim 11 , wherein the adjustment command comprises instructions to decrease a parking brake force of the hydraulic park brake. 14. A hydraulic park brake system for an aircraft, the hydraulic park brake system comprising: a hydraulic park brake; a sensor coupled to the hydraulic park brake; a hydraulic park brake controller having a processor; and a tangible, non-transitory memory configured to communicate with the processor, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the hydraulic park brake system to perform operations comprising: detecting, by the processor and via the sensor, a hydraulic park brake condition; comparing, by the processor, the hydraulic park brake condition with a predetermined condition to yield comparison data; and determining, by the processor and based on the comparison data, a hydraulic park brake adjustment status. 15. A method of controlling a hydraulic park brake system of an aircraft, the method comprising: receiving, by a hydraulic park brake controller, a hydraulic park brake condition; comparing, by the hydraulic park brake controller, the hydraulic park brake condition with a predetermined condition to yield comparison data; determining, by the hydraulic park brake controller and based on the comparison data, a hydraulic park brake adjustment status; generating, by the hydraulic park brake controller and based on the hydraulic park brake adjustment status, an adjustment command; and transmitting, by the hydraulic park brake controller, the adjustment command to a hydraulic park brake of the aircraft; wherein the adjustment command comprises instructions to at least one of increase a parking brake force of the hydraulic park brake and decrease the parking brake force of the hydraulic park brake. 16. The method of claim 15 , wherein the receiving the hydraulic park brake condition comprises detecting, by the hydraulic park brake controller and via a sensor, the hydraulic park brake condition.
Pressure measurement in brake systems · CPC title
Procedure or apparatus for checking or keeping in a correct functioning condition of brake systems (hydraulic pressure systems in general F15B19/00, F15B21/04; testing structures or apparatus G01M) · CPC title
Actuating mechanisms · CPC title
controlling auxiliary pressure brakes, e.g. parking or emergency brakes (B60T15/048 takes precedence) · CPC title
Complex systems; Conjoint control of two or more vehicle active control systems · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.