GB821557A - Improvements in or relating to indicating instruments - Google Patents
Improvements in or relating to indicating instrumentsInfo
- Publication number
- GB821557A GB821557A GB28297/56A GB2829756A GB821557A GB 821557 A GB821557 A GB 821557A GB 28297/56 A GB28297/56 A GB 28297/56A GB 2829756 A GB2829756 A GB 2829756A GB 821557 A GB821557 A GB 821557A
- Authority
- GB
- United Kingdom
- Prior art keywords
- screen
- image
- screens
- indicator
- vertical
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
Abstract
821,557. Final indicators for measuring systems. DEUTA-WERKE (VORM. DEUTSCHE TACHOMETER-WERKE) G.m.b.H. Sept. 17, 1956 [Nov. 23, 1955], No. 28297/56. Class 40 (1). [Also in Groups XXXIII and XL (c)] A cathode-ray tube indicator comprises a cathode-ray tube with a substantially flat rectangular screen and a planar electron beam producing a line image on the screen which is deflected transversely to itself or orientated in accordance with the magnitude of a quantity to be measured. Fig. 1 illustrates an aircraft instrument panel comprising a plurality of such indicators, scalar quantities such as engine speed and altitude being displayed as vertical displacements of the line images on the vertical screens 2 .. 6 and angular quantities such as heading and artificial horizon being displayed by orientation of the line images on the horizontal screens 7, 8, 9. The controls for each vertical indicator are arranged so that the central position of the image corresponds to the desired value of the input quantity, these datum positions being in horizontal alignment. The images may be blanked out when in their datum positions to prevent screen burn and the image focus may be varied in accordance with the deviation of the image from its datum position. The calibration scales may be adjacent the screens as shown or they may be in the form of self-luminous lines on the screen. Each indicator tube 33, Fig. 4, may be mounted in a rectangular metal screening case 34 which can be plugged into the instrument panel, the front edge 39 of the case 34 having an inwardlysloping flange against which the flat screen of the tube abuts; the scale 41 may be applied to the side flanges; cut-outs or projections 40 in the top and bottom flanges facilitate removal of the case. If the image is displaced to either end of the screen, the electron beam impinges on an electrode 38 to actuate an indicating or safety relay device.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE821557X | 1955-11-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB821557A true GB821557A (en) | 1959-10-07 |
Family
ID=6740564
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28297/56A Expired GB821557A (en) | 1955-11-23 | 1956-09-17 | Improvements in or relating to indicating instruments |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB821557A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2137848A (en) * | 1983-03-11 | 1984-10-10 | Sony Corp | Television receivers |
WO2012025695A1 (en) * | 2010-08-24 | 2012-03-01 | Airbus Operations | Bracket for display devices for an aircraft cockpit |
-
1956
- 1956-09-17 GB GB28297/56A patent/GB821557A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2137848A (en) * | 1983-03-11 | 1984-10-10 | Sony Corp | Television receivers |
WO2012025695A1 (en) * | 2010-08-24 | 2012-03-01 | Airbus Operations | Bracket for display devices for an aircraft cockpit |
FR2964084A1 (en) * | 2010-08-24 | 2012-03-02 | Airbus Operations Sas | SUPPORT OF DISPLAY DEVICES FOR AN AIRCRAFT DRIVING UNIT |
CN103068680A (en) * | 2010-08-24 | 2013-04-24 | 空中客车运营简化股份公司 | Bracket for display devices for an aircraft cockpit |
US9643731B2 (en) | 2010-08-24 | 2017-05-09 | Airbus Operations (S.A.S.) | Bracket for display devices for an aircraft cockpit |
CN103068680B (en) * | 2010-08-24 | 2017-07-28 | 空中客车运营简化股份公司 | Supporting member for the display device of aircraft cockpit |
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