GB700071A - Improvements in or relating to air pilot's controls - Google Patents
Improvements in or relating to air pilot's controlsInfo
- Publication number
- GB700071A GB700071A GB13033/52A GB1303352A GB700071A GB 700071 A GB700071 A GB 700071A GB 13033/52 A GB13033/52 A GB 13033/52A GB 1303352 A GB1303352 A GB 1303352A GB 700071 A GB700071 A GB 700071A
- Authority
- GB
- United Kingdom
- Prior art keywords
- switches
- arm
- movement
- opposite directions
- relating
- 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
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Light Control Or Optical Switches (AREA)
Abstract
700,071. Retractive switches. BLACKBURN & GENERAL AIRCRAFT, Ltd., and WOODWARD, S. C. May 22, 1952. No. 13033/52. Class 38(5) [Also in Group XXXIII] In a control column head is mounted a rotatable member 8 so that its fluted surface protrudes from the arm 3. Member 10 is eccentrically pivoted to member 8, so that rotation of the latter in opposite directions results in movement of member 10 in the direction of its length, in opposite directions, causing actuation of one of the switches 6 and 7, according to the direction of movement. A double acting spring box is connected between member 10 and the arm 3 to provide centering bias, rendering both switches off unless member 8 is held in a rotated position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13033/52A GB700071A (en) | 1952-05-22 | 1952-05-22 | Improvements in or relating to air pilot's controls |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13033/52A GB700071A (en) | 1952-05-22 | 1952-05-22 | Improvements in or relating to air pilot's controls |
Publications (1)
Publication Number | Publication Date |
---|---|
GB700071A true GB700071A (en) | 1953-11-25 |
Family
ID=10015573
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13033/52A Expired GB700071A (en) | 1952-05-22 | 1952-05-22 | Improvements in or relating to air pilot's controls |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB700071A (en) |
-
1952
- 1952-05-22 GB GB13033/52A patent/GB700071A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1368347A (en) | Control flap arrangement for aircraft | |
GB700071A (en) | Improvements in or relating to air pilot's controls | |
CA499417A (en) | Motor control systems | |
GB516720A (en) | Improvements relating to the control and operation of wing flaps of aircraft | |
GB655089A (en) | Improvements in or relating to the control of aircraft at low speeds | |
GB803576A (en) | Control systems for aircraft | |
GB1034959A (en) | Improvements in or relating to controllers for effecting through control elements movement of hydraulically or pneumatically operated devices in vehicles | |
GB803577A (en) | Control systems for aircraft | |
CA495605A (en) | Motor control systems | |
GB682483A (en) | Improvements relating to automatic air-flow control means, particularly for use on aircraft | |
GB587993A (en) | Improvements in aircraft control systems | |
GB727754A (en) | An improved butterfly valve | |
CA469420A (en) | Air-operated rotating devices and air supply and control mechanism therefor | |
CA464362A (en) | Valve control mechanism | |
CA469311A (en) | Pilot fuel flow controls | |
CA463165A (en) | Steering arm joint assembly unit | |
CA465987A (en) | Speed control mechanism | |
GB526388A (en) | Improvements in control gear, particularly for aircraft | |
GB557464A (en) | Improvements in aircraft controls | |
GB656217A (en) | Improvements in aircraft control mechanism | |
AU151003B2 (en) | Overspeed control means for rotary motion | |
CA465814A (en) | Fluid pressure control mechanism | |
CA465106A (en) | Fluid pressure control mechanism | |
GB707626A (en) | Improvements in or relating to control linkages | |
FR936260A (en) | Compressed air control device actuating the aircraft controls by compressed air position regulator |