US4404633A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Process and device for braking an aircraft by seeking an optimal sliding of the braked wheels
Assignee: Airbus Group SAS
•
Filing: 1981-01-07
•
Granted: 1983-09-13
•
Expires: 2001-01-07
Abstract
Abstract The present invention relates to a process and device for braking an aircraft taxiing on the ground after landing and comprising a plurality of braked wheels, by seeking a maximum coefficient of adherence between said braked wheels and the ground on which they roll, wherein said braking is subdivided into a plurality of successive braking periods and each of these periods is itself divided into a first phase during which a reference sliding value is imposed on each braked wheel and the optimal sliding value of the period is determined, and into a second phase during which said optimal sliding value is imposed on all said braked wheels. The invention is applicable to the automatic braking of aircraft.
Inventors
- 👤 Jose R. Goicoechea
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 02:26
CPC Classifications
B; B64; B64C; B64C25/00; B64C25/32; B64C25/42; B64C25/426; B60; B60T; B60T8/00; B60T8/17; B60T8/1701; B60T8/1703
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
145 words
Process for braking an aircraft taxiing on the ground after landing, said aircraft comprising a plurality of braked wheels, comprising the steps of: dividing said braking into a plurality of successive braking periods; sub-dividing each of said braking periods into a first relatively short interval and a second substantially longer interval; imposing on each of said wheels a predetermined different reference sliding value during said first interval; determining for each wheel a coefficient of adherence corresponding to the sliding value imposed thereon; establishing from said imposed sliding values and corresponding coefficients of adherence a relationship expressing the coefficient of adherence of said wheels as a function of the sliding value imposed thereon; determining from said relationship an optimal sliding value resulting in the maximum value of the coefficient of adherence; and imposing said optimal sliding value on all of said wheels during said second interval.
Claim 2
Dependent Claim
145 words
Process for braking an aircraft taxiing on the ground after landing, said aircraft comprising a plurality of braked wheels, comprising the steps of: dividing said braking into a plurality of successive braking periods; sub-dividing each of said braking periods into a first relatively short interval and a second substantially longer interval; imposing on each of said wheels a predetermined different reference sliding value during said first interval; determining for each wheel a coefficient of adherence corresponding to the sliding value imposed thereon; establishing from said imposed sliding values and corresponding coefficients of adherence a relationship expressing the coefficient of adherence of said wheels as a function of the sliding value imposed thereon; determining from said relationship an optimal sliding value resulting in the maximum value of the coefficient of adherence; and imposing said optimal sliding value on all of said wheels during said second interval.
Claim 3
Dependent Claim
29 words
The process of claim 1, wherein, in a braking period, the first interval lasts a few tenths of second, whilst the second interval lasts a few tens of seconds.
Claim 4
Dependent Claim
25 words
The process of claim 1, wherein the coefficients of adherence of the braked wheels are represented by the drag force or the drag torque thereof.
Claim 5
Dependent Claim
32 words
The process of claim 1 applied to wheels provided with hydraulic brakes wherein the sliding of the braked wheels is controlled by controlling the pressure of the fluid in the associated brakes.
Claim 6
Dependent Claim
53 words
The process of claim 1, wherein the different reference sliding values applied to the different braked wheels during the first interval of each braking period are deduced from the optimal sliding value of the preceding braking period, one being equal to this optimal value whilst the others differ therefrom by a few tenths.
Claim 7
Dependent Claim
26 words
The process of claim 1, wherein the beginning and end of a braking period are determined by predetermined values of the taxiing speed of the aircraft.
Claim 8
Dependent Claim
20 words
The process of claim 3, wherein the drag force or the drag torque are measured by means of strain gauges.
Claim 9
Dependent Claim
19 words
The process of claim 1, applied to all the braked wheels of all the bogies of a landing gear.
Claim 10
Dependent Claim
38 words
A process in accordance with claim 1 further including a preliminary phase prior to the first of said successive braking periods, during which preliminary phase a constant predetermined sliding value is imposed on all of said braked wheels.
Claim 11
Independent Claim
137 words
A device for braking an aircraft comprising a plurality of braked wheels and at least one non-braked wheel, said device comprising: means including braking means for imposing on each of said braked wheels a different predetermined sliding value, means including a tachometer generator associated with each of said braked wheels and said non-braked wheel for determining a coefficient of adherence of each braked wheel corresponding to the sliding value imposed thereon; means for establishing from said sliding values and corresponding coefficients of adherence a relationship expressing the coefficient of adherence of said braked wheels as a function of the sliding value imposed thereon; means for determining from said relationship an optimal sliding value resulting in the maximum value of the coefficient of adherence; and means for imposing said optimal sliding value on all of said braked wheels.
Claim 12
Independent Claim
137 words
A device for braking an aircraft comprising a plurality of braked wheels and at least one non-braked wheel, said device comprising: means including braking means for imposing on each of said braked wheels a different predetermined sliding value, means including a tachometer generator associated with each of said braked wheels and said non-braked wheel for determining a coefficient of adherence of each braked wheel corresponding to the sliding value imposed thereon; means for establishing from said sliding values and corresponding coefficients of adherence a relationship expressing the coefficient of adherence of said braked wheels as a function of the sliding value imposed thereon; means for determining from said relationship an optimal sliding value resulting in the maximum value of the coefficient of adherence; and means for imposing said optimal sliding value on all of said braked wheels.
Claim 13
Dependent Claim
29 words
A device in accordance with claim 10 wherein each of said braking means comprises: a hydraulic brake, and a servovalve associated with each brake and controlling the operation thereof.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-09-12 | 1987-03-14 | 1987-09-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-09-12 | 1991-03-14 | 1991-09-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-09-12 | 1995-03-14 | 1995-09-13 | $7700.00 | Window Closed / Lapsed |