GB598383A - Improvements in the braking of aeroplane wheels - Google Patents
Improvements in the braking of aeroplane wheelsInfo
- Publication number
- GB598383A GB598383A GB17090/45A GB1709045A GB598383A GB 598383 A GB598383 A GB 598383A GB 17090/45 A GB17090/45 A GB 17090/45A GB 1709045 A GB1709045 A GB 1709045A GB 598383 A GB598383 A GB 598383A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- wheels
- aeroplane
- vane
- incidence
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
- Braking Systems And Boosters (AREA)
- Transmission Of Braking Force In Braking Systems (AREA)
Abstract
598,383. Aircraft wheel brakes. OLAER PATENT CO., and COMPAGNIE GENERALE POUR L'EQUIPEMENT AERONAUTIQUE. July 4, 1945, No. 17090. Convention date, April 7, 1944. [Class 4] A brake system for the landing wheels of an aircraft comprises an aerodynamic device acting on control means such as a regulating valve to limit the maximum applicable braking force in accordance with the lift acting on the aircraft or the speed of the aircraft. As shown applied to a hydraulic brake system, the wheel brakes 5, 6 are operated from a pressure accumulator 13 through valves 9, 10 controlled by pedals 11, 12. A pressure-regulating valve 18 is interposed between the accumulator and the valves 9, 10 and is controlled by a vane 2. mounted on a parallelogram linkage 20, 21, 22 The loading per unit area and incidence of the vane are arranged to be the same as the wing loading and incidence of the aeroplane so that the position of the control member 19 of the valve corresponds to the nett weight on the wheels (weight minus lift) and the maximum braking force which may be applied to the wheels is limited accordingly. The member 19 may, alternatively, be operated by a device, such as a Pitot tube, responsive to the speed of the aeroplane.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR598383X | 1944-04-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB598383A true GB598383A (en) | 1948-02-17 |
Family
ID=8968861
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB17090/45A Expired GB598383A (en) | 1944-04-07 | 1945-07-04 | Improvements in the braking of aeroplane wheels |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB598383A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103204240A (en) * | 2012-01-10 | 2013-07-17 | 霍尼韦尔国际公司 | Brake assembly including independently activatable brake actuators |
| EP4159617A3 (en) * | 2021-09-30 | 2023-07-05 | Airbus Operations Limited | Aircraft hydraulic braking system and method of controlling same |
-
1945
- 1945-07-04 GB GB17090/45A patent/GB598383A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103204240A (en) * | 2012-01-10 | 2013-07-17 | 霍尼韦尔国际公司 | Brake assembly including independently activatable brake actuators |
| EP4159617A3 (en) * | 2021-09-30 | 2023-07-05 | Airbus Operations Limited | Aircraft hydraulic braking system and method of controlling same |
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