GB449702A - Improvements relating to brake control mechanism for aircraft - Google Patents
Improvements relating to brake control mechanism for aircraftInfo
- Publication number
- GB449702A GB449702A GB540635A GB540635A GB449702A GB 449702 A GB449702 A GB 449702A GB 540635 A GB540635 A GB 540635A GB 540635 A GB540635 A GB 540635A GB 449702 A GB449702 A GB 449702A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plunger
- instructor
- cable
- aircraft
- seat
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hydraulic Control Valves For Brake Systems (AREA)
Abstract
449,702. Dual - control for aircraft. BENDIX, Ltd., and LAMBERT, A. W., King's Road, Tyseley, Birmingham. Feb. 20, 1935, No. 5406. [Class 4] Aircraft landing- wheel brakes can be applied from the instructor's seat through a movable member with which is associated a relatively movable part operable from the pupil's seat and normally locked to the movable member by a catch or detent which can be disengaged at will by a control operated from the instructor's seat. As shown, the landing-wheel brakes are applied by the instructor through a cable g, a plunger b and a cable c. The cable g is connected to the plunger by means of a nipple kslidable in a bore in the plunger. Cables h,j, lead to the pupil's brake lever and rudder bar and are releasably connected to the plunger b by rollers r and plungers n which are connected to the cables h, j by slidable nipples m. Springs p urge the barrel b to its inoperative position. The plungers n are freed from the plunger on actuation, by the instructor, of a plunger u by a cable w against the action of a spring v.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB540635A GB449702A (en) | 1935-02-20 | 1935-02-20 | Improvements relating to brake control mechanism for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB540635A GB449702A (en) | 1935-02-20 | 1935-02-20 | Improvements relating to brake control mechanism for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB449702A true GB449702A (en) | 1936-07-02 |
Family
ID=9795562
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB540635A Expired GB449702A (en) | 1935-02-20 | 1935-02-20 | Improvements relating to brake control mechanism for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB449702A (en) |
-
1935
- 1935-02-20 GB GB540635A patent/GB449702A/en not_active Expired
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