GB402225A - Apparatus for the automatic operation of the vertical and transverse stabilising of aircraft - Google Patents
Apparatus for the automatic operation of the vertical and transverse stabilising of aircraftInfo
- Publication number
- GB402225A GB402225A GB28769/32A GB2876932A GB402225A GB 402225 A GB402225 A GB 402225A GB 28769/32 A GB28769/32 A GB 28769/32A GB 2876932 A GB2876932 A GB 2876932A GB 402225 A GB402225 A GB 402225A
- Authority
- GB
- United Kingdom
- Prior art keywords
- disc
- pointer
- plane
- magnet
- 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
- G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Transmission And Conversion Of Sensor Element Output (AREA)
Abstract
402,225. Clinometers. MESSGERATE BOYKOW GES., Goerz Allee, Zehlendorf, Berlin. - (Assignees of Boykow, J. M. ; 2A, Fontanestrasse, West Lichterfelde, Berlin.) Oct. 14, 1932, No. 28769. Convention date, Oct. 14, 1931. [Class 97 (ii).] An aircraft is provided with two bodies each containing two symmetrically disposed nozzles, one pair being in a vertical plane and directed upwards and downwards and the other pair being in a horizontal plane, these nozzles through differential manometers automatically controlling the elevator and ailerons or adjusting an indicator on the dashboard. Two streamlined bodies having symmetrically disposed nozzle openings d<1>, d<11> are arranged on the wings, one with its plane ofsymmetry parallel to a horizontal plane and the other with its plane parallel to a vertical longitudinal plane. The nozzle throats are connected to capsules m<1>, m<2> which normally hold a pointer z in mid position between contact strips c, Fig. 3, carried by a spindle b which is constrained by a spring f, levers g, and a crank n to assume a normal position. Any movement of the pointer z energizes magnets e<1>, e<2> to move the spindle b in a direction to follow up the pointer, this motion being damped by a fluid friction device p, this friction device also resisting the return motion produced by the spring f. Simultaneously, rotary magnets control air-valves of cylinders acting upon the elevator or aileron controls. As applied to an indicating instrument, the pointers z act through devices similar to that shown in Fig. 3 upon rotary magnets T', T', Fig. 5. The magnet T' rotates a semicircular disc S, the top edge of which represents the horizon, by means of links r<1>, r<2>, r<3> in front of a disc representing the sky. The magnet T<1> raises and lowers the disc S by means of a lever u<3> link u<2> and angle lever u<1> centred on the axis of the magnet T2. In front of the disc S is a transparent disc having an outline of the bonnet g of the machine. The disc S may bear a photographic representation of the ground. A pointer may be moved transversely across the instrument in response to a turn indicator.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE402225X | 1931-10-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB402225A true GB402225A (en) | 1933-11-30 |
Family
ID=6410180
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28769/32A Expired GB402225A (en) | 1931-10-14 | 1932-10-14 | Apparatus for the automatic operation of the vertical and transverse stabilising of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB402225A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2420932A (en) * | 1943-08-11 | 1947-05-20 | E H Johnson | Control system for airplanes |
US2621873A (en) * | 1947-03-31 | 1952-12-16 | North American Aviation Inc | Aircraft control |
US2626115A (en) * | 1951-06-07 | 1953-01-20 | North American Aviation Inc | Aircraft controls |
-
1932
- 1932-10-14 GB GB28769/32A patent/GB402225A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2420932A (en) * | 1943-08-11 | 1947-05-20 | E H Johnson | Control system for airplanes |
US2621873A (en) * | 1947-03-31 | 1952-12-16 | North American Aviation Inc | Aircraft control |
US2626115A (en) * | 1951-06-07 | 1953-01-20 | North American Aviation Inc | Aircraft controls |
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