GB352035A - Automatic sighting and directing devices for torpedoes, guns and other apparatus - Google Patents
Automatic sighting and directing devices for torpedoes, guns and other apparatusInfo
- Publication number
- GB352035A GB352035A GB39195/29A GB3919529A GB352035A GB 352035 A GB352035 A GB 352035A GB 39195/29 A GB39195/29 A GB 39195/29A GB 3919529 A GB3919529 A GB 3919529A GB 352035 A GB352035 A GB 352035A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cells
- target
- image
- steering
- currents
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/2273—Homing guidance systems characterised by the type of waves
- F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/10—Missiles having a trajectory only in the air
- F42B15/105—Air torpedoes, e.g. projectiles with or without propulsion, provided with supporting air foil surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/01—Steering control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
352,035. Optical apparatus. TIHANYI, K., 324, Juranies telep D.l.Úp, Budapest. Dec. 21, 1929, No. 39195. Convention date, Dec. 16. [Class 97 (i).] Relates to devices for automatically directing telescopes, range-finders, &c., in which an image of the target is distributed on one or more light or heat sensitive cells connected in a balanced circuit, the movement of the target producing out of balance currents which actuate steering mechanism. The invention consists in providing means for automatically varying the angle of vision in accordance with the size of the image of the target. Varying the angle of vision. Two cells 93, 94, Fig. 17, are connected, or feed valves 96, 97, connected in a balanced circuit such as a Wheatstone bridge. One cell 93 is illuminated by an image 98 of the target and the other cell is illuminated by an image of an empty portion of the field of the target. Should the size of the image of the target increase, the balance of the bridge is disturbed and the resulting out of balance current, after amplification at 95, actuates a variable diaphragm such as in Fig. 15 by rotating one or both of the apertured discs 88, 89. Steering in one plane. In the complete device of Fig. 12 an image of the target 2 is reflected from a mirror 67 through a biprism 9 on to cells 59, 60, 61 of which the cells 59, 60 control the diaphragm 57 as described above. The cells 60, 61 are connected in a balanced circuit and out of balance currents produced by the movements of the target and amplified at 68 may steer the torpedo &c. or may actuate a mirror 67 which distributes light from a source 51 on to two cells 65, 69. The cells 65, 69 are balanced and out of balance currents after amplification at 64 may control the steering mechanism. The relay comprising mirror 67 and cells 65, 69 may be duplicated to add sensitivity and need not be an optical system. Short-wave electromagnetic radiation may be used and controlled by the currents from amplifier 62. This device steers in one plane only. The biprism 9 may be replaced by mirrors or an internally reflecting prism. The cells 60, 61 may comprise bolometer threads 34, 35, Fig. 8, rotating in the plane of the image and connected by commutators into the arms of a Wheatstone bridge. Spatial steering. By distributing the image over four cells 30 .. 33, Fig. 7, connected in pairs in two balanced circuits such as Wheatstone bridges, movements of the target produce two out of balance currents which are used to control the steering in two planes at right-angles. The photo-electric cells 30 .. 33 are enclosed in a common vacuum and have a common cathode 19. A slotted shutter may rotate before the cells, exposing each cell in turn to the image. Circuit arrangements. The cells for producing steering currents and those for controlling the diaphragm may be combined as in Fig. 18 in which the cells 60, 61 control the diaphragm and the cells 59, 61 control the steering. Details. The device may be enclosed in heat or magnetic protective casings and may have electrical instruments mounted on it or contacts for such instruments. The device may be fitted to be controlled by radiation from the sending station for at least part of the time. The target may be irradiated with energy to which the device is particularly sensitive.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HU352035X | 1929-12-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB352035A true GB352035A (en) | 1931-06-22 |
Family
ID=10978904
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB39195/29A Expired GB352035A (en) | 1929-12-16 | 1929-12-21 | Automatic sighting and directing devices for torpedoes, guns and other apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB352035A (en) |
Cited By (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2418137A (en) * | 1943-06-03 | 1947-04-01 | Milton J Noell | Means for guiding projectiles toward predetermined destinations and for ascertaining the positions of the destinations |
US2421012A (en) * | 1945-12-10 | 1947-05-27 | Thornton W Chew | Homing system |
US2421085A (en) * | 1943-07-12 | 1947-05-27 | Bendix Aviat Corp | Target seeking aerial bomb |
US2424193A (en) * | 1939-08-16 | 1947-07-15 | Rost Helge Fabian | Self-steering device |
US2425956A (en) * | 1944-01-27 | 1947-08-19 | Farnsworth Television & Radio | Target seeking device with phototube multiplier |
US2428713A (en) * | 1942-05-18 | 1947-10-07 | Jr John E Lindberg | Signalling system |
US2432920A (en) * | 1942-04-29 | 1947-12-16 | Mckay Herbert Couchman | Radiation-controlled release for aerial bombs or other loads |
US2433843A (en) * | 1942-10-17 | 1948-01-06 | Sperry Gyroscope Co Inc | Fixed gun interaircraft fire control system |
US2439294A (en) * | 1943-11-27 | 1948-04-06 | Hammond Instr Co | Steering control apparatus |
US2454651A (en) * | 1940-08-03 | 1948-11-23 | John H Homrighous | Synchronizing system |
US2457393A (en) * | 1942-01-14 | 1948-12-28 | Muffly Glenn | Apparatus for causation and prevention of collisions |
US2462925A (en) * | 1946-12-07 | 1949-03-01 | Sperry Corp | Radiant energy directional apparatus |
US2513367A (en) * | 1948-05-26 | 1950-07-04 | Sperry Corp | Radiant energy tracking apparatus |
US2680578A (en) * | 1945-02-17 | 1954-06-08 | Katz Leonhard | Glide bomb |
US2704513A (en) * | 1955-03-22 | Eye bias device for homing bomb | ||
US2764698A (en) * | 1942-11-23 | 1956-09-25 | Arthur R Knight | Control system |
US2823612A (en) * | 1953-08-20 | 1958-02-18 | Cox Arthur | Target seeker head for guided missiles |
US2828930A (en) * | 1952-06-21 | 1958-04-01 | Lafayette M Hughes | Electronic apparatus for stabilizing the attitude of moving craft and instruments carried thereby |
US2882823A (en) * | 1952-06-06 | 1959-04-21 | Brinro Ltd Soc | Improvements in proximity fuzes and similar apparatus |
US2911167A (en) * | 1952-04-08 | 1959-11-03 | Fay E Null | Heat seeker |
US2917967A (en) * | 1955-10-01 | 1959-12-22 | Askania Werke Ag | Photoelectric device, mainly for geodetical and astronomical instruments |
US2964265A (en) * | 1948-03-26 | 1960-12-13 | Bell Telephone Labor Inc | Steering system utilizing thermalenergy radiations |
US2966591A (en) * | 1956-05-09 | 1960-12-27 | Sperry Rand Corp | Object detection and tracking system |
US2966823A (en) * | 1948-08-21 | 1961-01-03 | Northrop Corp | Tracking telescope with dual field optical system |
US2972924A (en) * | 1958-02-26 | 1961-02-28 | John E Clemens | Optical comparator and range finder |
US2994270A (en) * | 1942-01-08 | 1961-08-01 | Maury I Hull | Anti-aircraft defense systems |
DE1113637B (en) * | 1958-03-11 | 1961-09-07 | Optische Ind Iade Oude Delftia | Seeker head for flying bodies |
US3000307A (en) * | 1953-08-04 | 1961-09-19 | Jr Herbert Trotter | Device for correcting the course of a missile |
US3015249A (en) * | 1949-03-14 | 1962-01-02 | Northrop Corp | Tracking telescope |
US3025023A (en) * | 1954-09-14 | 1962-03-13 | John W B Barghausen | Missile guidance system |
US3041011A (en) * | 1951-03-12 | 1962-06-26 | Rand Corp | Method and apparatus for vernier map matching and flight control therewith |
US3064924A (en) * | 1956-02-27 | 1962-11-20 | North American Aviation Inc | Infrared terminal guidance tracking system |
US3112399A (en) * | 1945-08-11 | 1963-11-26 | Thornton W Chew | Device for automatic homing of movable objects |
DE1159771B (en) * | 1960-06-11 | 1963-12-19 | Boelkow Entwicklungen Kg | Target seeker in flight bodies |
US3128061A (en) * | 1945-08-11 | 1964-04-07 | Thornton W Chew | Automatic self-guidance system for movable objects |
US3226057A (en) * | 1951-05-21 | 1965-12-28 | Robert G Wilson | Automatic control system for navigating a vehicle toward an isolated reference point |
DE1214094B (en) * | 1958-07-01 | 1966-04-07 | Dehavilland Aircraft | Shielding device in target search heads of unmanned aerial vehicles |
DE1217632B (en) * | 1958-01-16 | 1966-05-26 | Continental Elektro Ind Ag | Device, in particular for electro-optical distance measurement |
DE1294687B (en) * | 1963-10-29 | 1969-05-08 | Kern & Co Ag | Electro-optical distance measuring device |
DE977911C (en) * | 1957-11-06 | 1972-11-23 | Josef F Dipl-Ing Menke | Procedure for determining the location of heat targets |
US3724783A (en) * | 1952-07-01 | 1973-04-03 | Us Navy | Discriminatory missile guidance system |
US4519707A (en) * | 1983-01-31 | 1985-05-28 | General Dynamics, Pomona Division | Multi-spectral target detection system with common collecting means |
-
1929
- 1929-12-21 GB GB39195/29A patent/GB352035A/en not_active Expired
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2704513A (en) * | 1955-03-22 | Eye bias device for homing bomb | ||
US2424193A (en) * | 1939-08-16 | 1947-07-15 | Rost Helge Fabian | Self-steering device |
US2454651A (en) * | 1940-08-03 | 1948-11-23 | John H Homrighous | Synchronizing system |
US2994270A (en) * | 1942-01-08 | 1961-08-01 | Maury I Hull | Anti-aircraft defense systems |
US2457393A (en) * | 1942-01-14 | 1948-12-28 | Muffly Glenn | Apparatus for causation and prevention of collisions |
US2432920A (en) * | 1942-04-29 | 1947-12-16 | Mckay Herbert Couchman | Radiation-controlled release for aerial bombs or other loads |
US2428713A (en) * | 1942-05-18 | 1947-10-07 | Jr John E Lindberg | Signalling system |
US2433843A (en) * | 1942-10-17 | 1948-01-06 | Sperry Gyroscope Co Inc | Fixed gun interaircraft fire control system |
US2764698A (en) * | 1942-11-23 | 1956-09-25 | Arthur R Knight | Control system |
US2418137A (en) * | 1943-06-03 | 1947-04-01 | Milton J Noell | Means for guiding projectiles toward predetermined destinations and for ascertaining the positions of the destinations |
US2421085A (en) * | 1943-07-12 | 1947-05-27 | Bendix Aviat Corp | Target seeking aerial bomb |
US2439294A (en) * | 1943-11-27 | 1948-04-06 | Hammond Instr Co | Steering control apparatus |
US2425956A (en) * | 1944-01-27 | 1947-08-19 | Farnsworth Television & Radio | Target seeking device with phototube multiplier |
US2680578A (en) * | 1945-02-17 | 1954-06-08 | Katz Leonhard | Glide bomb |
US3128061A (en) * | 1945-08-11 | 1964-04-07 | Thornton W Chew | Automatic self-guidance system for movable objects |
US3112399A (en) * | 1945-08-11 | 1963-11-26 | Thornton W Chew | Device for automatic homing of movable objects |
US2421012A (en) * | 1945-12-10 | 1947-05-27 | Thornton W Chew | Homing system |
US2462925A (en) * | 1946-12-07 | 1949-03-01 | Sperry Corp | Radiant energy directional apparatus |
US2964265A (en) * | 1948-03-26 | 1960-12-13 | Bell Telephone Labor Inc | Steering system utilizing thermalenergy radiations |
US2513367A (en) * | 1948-05-26 | 1950-07-04 | Sperry Corp | Radiant energy tracking apparatus |
US2966823A (en) * | 1948-08-21 | 1961-01-03 | Northrop Corp | Tracking telescope with dual field optical system |
US3015249A (en) * | 1949-03-14 | 1962-01-02 | Northrop Corp | Tracking telescope |
US3041011A (en) * | 1951-03-12 | 1962-06-26 | Rand Corp | Method and apparatus for vernier map matching and flight control therewith |
US3226057A (en) * | 1951-05-21 | 1965-12-28 | Robert G Wilson | Automatic control system for navigating a vehicle toward an isolated reference point |
US2911167A (en) * | 1952-04-08 | 1959-11-03 | Fay E Null | Heat seeker |
US2882823A (en) * | 1952-06-06 | 1959-04-21 | Brinro Ltd Soc | Improvements in proximity fuzes and similar apparatus |
US2828930A (en) * | 1952-06-21 | 1958-04-01 | Lafayette M Hughes | Electronic apparatus for stabilizing the attitude of moving craft and instruments carried thereby |
US3724783A (en) * | 1952-07-01 | 1973-04-03 | Us Navy | Discriminatory missile guidance system |
US3000307A (en) * | 1953-08-04 | 1961-09-19 | Jr Herbert Trotter | Device for correcting the course of a missile |
US2823612A (en) * | 1953-08-20 | 1958-02-18 | Cox Arthur | Target seeker head for guided missiles |
US3025023A (en) * | 1954-09-14 | 1962-03-13 | John W B Barghausen | Missile guidance system |
US2917967A (en) * | 1955-10-01 | 1959-12-22 | Askania Werke Ag | Photoelectric device, mainly for geodetical and astronomical instruments |
US3064924A (en) * | 1956-02-27 | 1962-11-20 | North American Aviation Inc | Infrared terminal guidance tracking system |
US2966591A (en) * | 1956-05-09 | 1960-12-27 | Sperry Rand Corp | Object detection and tracking system |
DE977911C (en) * | 1957-11-06 | 1972-11-23 | Josef F Dipl-Ing Menke | Procedure for determining the location of heat targets |
DE1217632B (en) * | 1958-01-16 | 1966-05-26 | Continental Elektro Ind Ag | Device, in particular for electro-optical distance measurement |
DE1217632C2 (en) * | 1958-01-16 | 1973-07-19 | Continental Elektro Ind Ag | Device, in particular for electro-optical distance measurement |
US2972924A (en) * | 1958-02-26 | 1961-02-28 | John E Clemens | Optical comparator and range finder |
DE1113637B (en) * | 1958-03-11 | 1961-09-07 | Optische Ind Iade Oude Delftia | Seeker head for flying bodies |
DE1214094B (en) * | 1958-07-01 | 1966-04-07 | Dehavilland Aircraft | Shielding device in target search heads of unmanned aerial vehicles |
DE1159771B (en) * | 1960-06-11 | 1963-12-19 | Boelkow Entwicklungen Kg | Target seeker in flight bodies |
DE1294687B (en) * | 1963-10-29 | 1969-05-08 | Kern & Co Ag | Electro-optical distance measuring device |
US4519707A (en) * | 1983-01-31 | 1985-05-28 | General Dynamics, Pomona Division | Multi-spectral target detection system with common collecting means |
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