GB524017A - Improvements in bearings for gyroscopic instruments - Google Patents

Improvements in bearings for gyroscopic instruments

Info

Publication number
GB524017A
GB524017A GB3731938A GB3731938A GB524017A GB 524017 A GB524017 A GB 524017A GB 3731938 A GB3731938 A GB 3731938A GB 3731938 A GB3731938 A GB 3731938A GB 524017 A GB524017 A GB 524017A
Authority
GB
United Kingdom
Prior art keywords
rotor case
sensitive element
ball
blades
blade
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
GB3731938A
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.)
WILLIAM GEORGE HARDING
Sperry Gyroscope Co Ltd
Original Assignee
WILLIAM GEORGE HARDING
Sperry Gyroscope Co Ltd
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 WILLIAM GEORGE HARDING, Sperry Gyroscope Co Ltd filed Critical WILLIAM GEORGE HARDING
Priority to GB3731938A priority Critical patent/GB524017A/en
Publication of GB524017A publication Critical patent/GB524017A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/34Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
    • G01C19/38Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation

Landscapes

  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Toys (AREA)

Abstract

524,017. Gyroscopic apparatus ; pivots. SPERRY GYROSCOPE CO., Ltd., MURTAGH, H., and HARDING, W. G. Dec. 22, 1938, No. 37319. [Class 97 (iii)] [Also in Group XXV] In a gyroscopic instrument the sensitive element is supported, for limited angular movement about a substantially horizontal axis, by vertical filaments or blades which connect with the sensitive element substantially on the horizontal axis, lateral movements of the sensitive element being prevented by low-friction guides. In Fig. 2 is shown the suspension means at one side of the rotor case 1 of a directional gyroscope of the type described in Specification 504,726. A spring steel blade 7 is secured at its upper end to the cardan or vertical ring 2 and is clamped between two blocks 9<SP>1</SP> bolted to the rotor case. A pivot 11 extending from the rotor case is received in a ball-bearing 12 which may slide vertically in a slot to accommodate vertical movement as the blade 7 shortens during bending. An eccentric shaft 14 may be adjusted to raise the ball-bearing and relieve the blade spring of weight, for example, during transport. In a modification, Fig. 5, the pivot shafts 18, 18<SP>1</SP> at each side of the rotor case project eccentrically as shown and are suspended by flexible steel blades 16, 16<SP>1</SP>, and instead of employing ball-bearings, lateral movement is prevented by stretched horizontal wires. The rotor case is tested for balance, top-heaviness and bottom-heaviness by suspending the rotor case solely by the spring blades and observing any tendency to rotate when displaced, and by observing its sensitivity to the transference of a very small weight from one side of the rotor case to the other.
GB3731938A 1938-12-22 1938-12-22 Improvements in bearings for gyroscopic instruments Expired GB524017A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3731938A GB524017A (en) 1938-12-22 1938-12-22 Improvements in bearings for gyroscopic instruments

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3731938A GB524017A (en) 1938-12-22 1938-12-22 Improvements in bearings for gyroscopic instruments

Publications (1)

Publication Number Publication Date
GB524017A true GB524017A (en) 1940-07-29

Family

ID=10395545

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3731938A Expired GB524017A (en) 1938-12-22 1938-12-22 Improvements in bearings for gyroscopic instruments

Country Status (1)

Country Link
GB (1) GB524017A (en)

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