GB447573A - A new braking system for aeroplanes - Google Patents
A new braking system for aeroplanesInfo
- Publication number
- GB447573A GB447573A GB14200/35A GB1420035A GB447573A GB 447573 A GB447573 A GB 447573A GB 14200/35 A GB14200/35 A GB 14200/35A GB 1420035 A GB1420035 A GB 1420035A GB 447573 A GB447573 A GB 447573A
- Authority
- GB
- United Kingdom
- Prior art keywords
- braking device
- chain
- pulleys
- pulley
- tail
- 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
- B64C25/44—Actuating mechanisms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Braking Arrangements (AREA)
Abstract
447,573. Braking device for aircraft. OROPESA, J. M. C. DE, 113, Calle de San Bernardo, Madrid. May 15, 1935, No. 14200. Convention date, Dec. 20, 1934. [Class 4] A braking device for use on aeroplanes comprises one or more endless chain or bands of material containing rubber which are normally nested in the tail end of the fuselage, Fig. 1, but which may be lowered to a groundcontacting position, Fig. 2, and which are adapted to be driven in reverse sense of rotation to that of the front landing wheels. As shown, a chain 1 is mounted on a pulley 3 with a fixed axle and on pulleys 2 having movable axles. Axles of pulleys 2 are vertically slidable in guides 7, under the control of means such as pneumatic jacks, but manual means may be provided for the raising operation which is effected when the craft is at rest. Pulley 3 constitutes the driving wheel of the chain 1 its axle being formed with cranks engaged by the connecting rods of a compressed air motor. Means are provided for raising a tail skid or tail wheel prior to bringing the braking device into operation.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES447573X | 1934-12-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB447573A true GB447573A (en) | 1936-05-21 |
Family
ID=8245350
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB14200/35A Expired GB447573A (en) | 1934-12-20 | 1935-05-15 | A new braking system for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB447573A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2502802A (en) * | 1948-12-06 | 1950-04-04 | Sievers George | Automatic leveling retractable elongated landing gear for aircraft |
-
1935
- 1935-05-15 GB GB14200/35A patent/GB447573A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2502802A (en) * | 1948-12-06 | 1950-04-04 | Sievers George | Automatic leveling retractable elongated landing gear for aircraft |
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