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GB516987A - An indicating instrument for use in aircraft - Google Patents

An indicating instrument for use in aircraft

Info

Publication number
GB516987A
GB516987A GB21065/38A GB2106538A GB516987A GB 516987 A GB516987 A GB 516987A GB 21065/38 A GB21065/38 A GB 21065/38A GB 2106538 A GB2106538 A GB 2106538A GB 516987 A GB516987 A GB 516987A
Authority
GB
United Kingdom
Prior art keywords
pointer
air
climb
rate
speed
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
GB21065/38A
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.)
Askania Werke AG
Original Assignee
Askania Werke AG
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 Askania Werke AG filed Critical Askania Werke AG
Publication of GB516987A publication Critical patent/GB516987A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P1/00Details of instruments
    • G01P1/07Indicating devices, e.g. for remote indication
    • G01P1/08Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)

Abstract

516,987. Indicating-instruments. ASKANIAWERKE AKT.-GES. July 15, 1938, No. 21065. Convention date, July 23, 1937. Class 106 (ii)] On an aircraft the air-speed indicator and the rate-of-climb indicator are combined in a common casing, the first instrument being mounted to be rotatably adjustable. The pointers of the instrument are either arranged on a common axis or to avoid friction on two axes lying near one another as in the form illustrated. The air-speed pointer a pivoted at c moves over the dial plate h of the speedometer which is rotatable by turning the knob k, while the rate of climb pointer b pivoted at d moves over a fixed dial plate i slits corresponding to the size of the attaching means allow movement of the dial of the air-speed indicator. The pivots c, d are joined by a phospherescent bar f. When on a long distance flight the rate of climb pointer is at zero, the air speed pointer is adjusted to the Horizontal line formed by pointer a, bar f, and pointer b to secure uniformity of flight with respect to these factors.
GB21065/38A 1937-07-23 1938-07-15 An indicating instrument for use in aircraft Expired GB516987A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE516987X 1937-07-23

Publications (1)

Publication Number Publication Date
GB516987A true GB516987A (en) 1940-01-17

Family

ID=6549431

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21065/38A Expired GB516987A (en) 1937-07-23 1938-07-15 An indicating instrument for use in aircraft

Country Status (1)

Country Link
GB (1) GB516987A (en)

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