GB621836A - Improvements in or relating to radio gun control systems - Google Patents

Improvements in or relating to radio gun control systems

Info

Publication number
GB621836A
GB621836A GB2516/44A GB251644A GB621836A GB 621836 A GB621836 A GB 621836A GB 2516/44 A GB2516/44 A GB 2516/44A GB 251644 A GB251644 A GB 251644A GB 621836 A GB621836 A GB 621836A
Authority
GB
United Kingdom
Prior art keywords
axis
gyro
follow
target
housing
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
Application number
GB2516/44A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sperry Gyroscope Co Inc
Original Assignee
Sperry Gyroscope Co Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sperry Gyroscope Co Inc filed Critical Sperry Gyroscope Co Inc
Publication of GB621836A publication Critical patent/GB621836A/en
Expired legal-status Critical Current

Links

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Abstract

621,836. Gyroscopic apparatus. SPERRY GYROSCOPE CO., Inc. Feb. 10, 1944, No. 2516. Convention date, Feb. 15, 1943. [Class 97 (iii)] [Also in Groups XXI, XXXV and XXXVIII] A stabilized radio tracking system, for use in gun-fire control apparatus, comprises a gyro element, a follow-up member positioned by said element, and means for receiving radiant energy from a target, such means being,posi. tioned in accordance with the position of the follow-up member, automatic means being provided which is responsive to the reception of the received energy and which is adapted to direct the gyro element towards the target. When an azimuth torque motor amplifier 46 is actuated as the result of a radio scanner being out of line with the target it operates torque motor 23 mounted about axis C-C on a housing or follow-up member 18. Housing 18 is supported by trunnions in a bracket 33 movable about axis B-B and within the housing is a gimbal ring 26 movable about axis C-C. The gyro 16, which spins about axis A-A, is carried by a frame 25 movable in ring 26 about axis B-B. Actuation of motor 23 causes the gyro to precess about axis B-B and the gyro carries with it, by means of a shaft 39 coincident with its spin axis, a second gimbal ring 35 carrying the armature 55 of an E-transformer type pick-off device 19. The output voltage thereby induced across the conductors 53, 54 actuates an amplifier 21 which causes a servomotor to actuate, through gearing as shown, the housing 18 until armature 51 is restored to its neutral position. Similar means are employed for applying torque to the gyro about axis B-B and for causing the frame 18 to follow the resulting movements of the gyro when the scanner is out of line with the target in elevation.
GB2516/44A 1943-02-15 1944-02-10 Improvements in or relating to radio gun control systems Expired GB621836A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US621836XA 1943-02-15 1943-02-15

Publications (1)

Publication Number Publication Date
GB621836A true GB621836A (en) 1949-04-21

Family

ID=22040740

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2516/44A Expired GB621836A (en) 1943-02-15 1944-02-10 Improvements in or relating to radio gun control systems

Country Status (1)

Country Link
GB (1) GB621836A (en)

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