GB426439A - Improvements in automatic course redresser for aircraft - Google Patents
Improvements in automatic course redresser for aircraftInfo
- Publication number
- GB426439A GB426439A GB3961/34A GB396134A GB426439A GB 426439 A GB426439 A GB 426439A GB 3961/34 A GB3961/34 A GB 3961/34A GB 396134 A GB396134 A GB 396134A GB 426439 A GB426439 A GB 426439A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pulley
- pawl
- electromagnets
- aircraft
- pawls
- 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
- NCEXYHBECQHGNR-UHFFFAOYSA-N chembl421 Chemical compound C1=C(O)C(C(=O)O)=CC(N=NC=2C=CC(=CC=2)S(=O)(=O)NC=2N=CC=CC=2)=C1 NCEXYHBECQHGNR-UHFFFAOYSA-N 0.000 abstract 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 239000011435 rock Substances 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
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)
- Magnetic Treatment Devices (AREA)
Abstract
426,439. Controlling aircraft. SOC. ANON. SVILUPPI AERONAUTICI (S.A.S.A.), 184, Corso Umberto I, Rome. Feb. 7, 1934, No. 3961. Convention date, Feb. 8, 1933. [Class 4] Automatic steering - gear for aircraft, in which indications of the course are transmitted from the compass to the rudder by means of electric contacts, photoelectric cells, or gyroscopic devices, through two electric circuits controlling the servometer through a system of lever and pawl devices, comprises two wheels 21, 2<11> continuously rotated in opposite directions by the aircraft engine or an electric motor through pinions 7 and endless screws 5<1>, 5<11> and a central grooved-pulley 1 loose on a shaft 4, and to which is secured by a pin 9 a ruddercontrol rope and two electromagnets 13<1> 13<11> mounted on the pulley 1 for controlling in clockwise or anticlockwise direction one or other of two pawls 16<1>. Movement of an indicator 42 closes a circuit through one or other of two adjustable contacts 43<1> 43<11> to energize respectively either one of electromagnets 44<1>, 44<11> and move a core causing a contact 35 to close a circuit to energize one or other of the electromagnets 13<1>, 13<11>. Energization of the magnet 13<1>, e.g. moves its core 121 to the left locking a lever 10<1> against the action of a spring 14<1> to release one end of a rocking pawl 16<1> mounted on the pulley and allow a spring 15<1> to rock the pawl to cause engagement with teeth 6<1> on the wheel 21 thus causing the wheel 2<1> and pulley 1 to rotate together until the pawl engages a stop 191 to disengage the pawl and allow the pulley to be brought to its initial position by springs. The pulley carries three electrically insulated brushes, one of which contacts continuously whilst the other two only contact until the pawls are unlocked. Simultaneous engagement of the pawls is prevented by means of two levers mounted one on each end of a spindle passing through the pulley and provided at their free ends with rollers bearing against and actuated by the levers 10<1>, 10<11>. A hand lever may be provided, which, when placed in one or other of two extreme positions closes a circuit through one or other of the electromagnets to effect steering of the craft.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT426439X | 1933-02-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB426439A true GB426439A (en) | 1935-04-03 |
Family
ID=11254415
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3961/34A Expired GB426439A (en) | 1933-02-08 | 1934-02-07 | Improvements in automatic course redresser for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB426439A (en) |
-
1934
- 1934-02-07 GB GB3961/34A patent/GB426439A/en not_active Expired
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