GB302137A - Improvements relating to rudder-bars for aircraft - Google Patents
Improvements relating to rudder-bars for aircraftInfo
- Publication number
- GB302137A GB302137A GB26551/28A GB2655128A GB302137A GB 302137 A GB302137 A GB 302137A GB 26551/28 A GB26551/28 A GB 26551/28A GB 2655128 A GB2655128 A GB 2655128A GB 302137 A GB302137 A GB 302137A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pivoted
- post
- pilot
- fitting
- bar
- 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
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/06—Initiating means actuated personally adjustable to suit individual persons
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Bridges Or Land Bridges (AREA)
Abstract
302,137. Saunders, S. E., Knowler, H., and Richards, L. J. H. Sept. 15, 1928. Steering.-A rudder-bar a for an aeroplane is adjustable with regard to a fitting h about the pivoted lower end of a vertically-movable pivotpost c by a foot-manipulation of the pilot. The bar a is pivoted at d to the upper bearing f of the pivot post, trunnions g on which engage slots i in the fitting h. The lower bearing l for the post c is pivoted at n, to a link m, which is itself pivoted at o. The cable-arms j on the post c have the cable connections in line with the pivot n. By means of the toe straps b the pilot can raise the bar and post bodily about the pivot o and adjust the trunnions g to a suitable position on the fitting h. The slots i preferably slope towards the pilot, and may be closed by means such as pivoted bars. Rollers e on the rudderbar engage runways on the cock-pit floor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB26551/28A GB302137A (en) | 1928-09-15 | 1928-09-15 | Improvements relating to rudder-bars for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB26551/28A GB302137A (en) | 1928-09-15 | 1928-09-15 | Improvements relating to rudder-bars for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB302137A true GB302137A (en) | 1928-12-13 |
Family
ID=10245408
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB26551/28A Expired GB302137A (en) | 1928-09-15 | 1928-09-15 | Improvements relating to rudder-bars for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB302137A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3124378A1 (en) | 2015-07-27 | 2017-02-01 | Airbus Helicopters | An adjustable and rotary rudder bar for a rotary wing aircraft |
-
1928
- 1928-09-15 GB GB26551/28A patent/GB302137A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3124378A1 (en) | 2015-07-27 | 2017-02-01 | Airbus Helicopters | An adjustable and rotary rudder bar for a rotary wing aircraft |
| FR3039505A1 (en) * | 2015-07-27 | 2017-02-03 | Airbus Helicopters | ADJUSTABLE AND ROTARY ROTARY FOR A ROTATING AIRCRAFT |
| US10196130B2 (en) | 2015-07-27 | 2019-02-05 | Airbus Helicopters | Adjustable and rotary rudder bar for a rotary wing aircraft |
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