GB145459A - Improvements in indicators for the turning of aircraft about a vertical axis - Google Patents

Improvements in indicators for the turning of aircraft about a vertical axis

Info

Publication number
GB145459A
GB145459A GB16579/20A GB1657920A GB145459A GB 145459 A GB145459 A GB 145459A GB 16579/20 A GB16579/20 A GB 16579/20A GB 1657920 A GB1657920 A GB 1657920A GB 145459 A GB145459 A GB 145459A
Authority
GB
United Kingdom
Prior art keywords
pendulum
aircraft
turning
gyroscopic
deflexion
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
GB16579/20A
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.)
Raytheon Anschuetz GmbH
Original Assignee
Anschuetz and Co GmbH
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 Anschuetz and Co GmbH filed Critical Anschuetz and Co GmbH
Publication of GB145459A publication Critical patent/GB145459A/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/42—Rotary gyroscopes for indicating rate of turn; for integrating rate of turn

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)

Abstract

145,459. Ansch³tz & Co. March 24, 1917, [Convention date]. Gyroscopic apparatus.- A turn-indicator for aircraft comprises a simple pendulum 6 and a gyroscopic pendulum 10, mounted in co-linear bearings 4, 5 and 7, 8 respectively, the line of these bearings lying in the direction of flight. The axis of rotation of the rotor 12 is parallel to the transverse axis of the aircraft. The pendulums carry pointers 13, 14 moving over a common scale 15, turning of the aircraft about the vertical being indicated by relative movement between the pointers. The dimensions and speed of rotation of the gyroscope are preferably so adjusted that the gyroscopic deflexion on turning is approximately equal and opposite to the deflexion of the pendulum due to centrifugal force, so that the pendulum 10 remains approximately in the true vertical. The pendulum 6 may be replaced by a liquid level.
GB16579/20A 1917-03-24 1920-06-18 Improvements in indicators for the turning of aircraft about a vertical axis Expired GB145459A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE145459X 1917-03-24

Publications (1)

Publication Number Publication Date
GB145459A true GB145459A (en) 1921-04-21

Family

ID=5670759

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16579/20A Expired GB145459A (en) 1917-03-24 1920-06-18 Improvements in indicators for the turning of aircraft about a vertical axis

Country Status (1)

Country Link
GB (1) GB145459A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437175A (en) * 1942-12-08 1948-03-02 Jr Thomas O Summers Gyroscopic flight indicating instrument
AT386197B (en) * 1986-01-08 1988-07-11 Glaxo Group Ltd METHOD FOR PRODUCING NEW INDOLDER DERIVATIVES

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437175A (en) * 1942-12-08 1948-03-02 Jr Thomas O Summers Gyroscopic flight indicating instrument
AT386197B (en) * 1986-01-08 1988-07-11 Glaxo Group Ltd METHOD FOR PRODUCING NEW INDOLDER DERIVATIVES

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