DE316167C - - Google Patents

Info

Publication number
DE316167C
DE316167C DENDAT316167D DE316167DA DE316167C DE 316167 C DE316167 C DE 316167C DE NDAT316167 D DENDAT316167 D DE NDAT316167D DE 316167D A DE316167D A DE 316167DA DE 316167 C DE316167 C DE 316167C
Authority
DE
Germany
Prior art keywords
pendulum
inclination
aircraft
dial
pivot point
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.)
Active
Application number
DENDAT316167D
Other languages
German (de)
English (en)
Publication of DE316167C publication Critical patent/DE316167C/de
Active legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C9/00—Measuring inclination, e.g. by clinometers, by levels
    • G01C9/02—Details
    • G01C9/08—Means for compensating acceleration forces due to movement of instrument

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • A Measuring Device Byusing Mechanical Method (AREA)
DENDAT316167D Active DE316167C (cs)

Publications (1)

Publication Number Publication Date
DE316167C true DE316167C (cs)

Family

ID=568891

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT316167D Active DE316167C (cs)

Country Status (1)

Country Link
DE (1) DE316167C (cs)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2480867A (en) * 1943-07-24 1949-09-06 Us Navy Aircraft instrument
US3497962A (en) * 1967-11-06 1970-03-03 Us Navy Method and means for minimizing horizontal accelerations in shipboard vertical pendula
US4303164A (en) * 1974-09-02 1981-12-01 Linden-Alimak Ab Structure for damping the oscillation of building cranes

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2480867A (en) * 1943-07-24 1949-09-06 Us Navy Aircraft instrument
US3497962A (en) * 1967-11-06 1970-03-03 Us Navy Method and means for minimizing horizontal accelerations in shipboard vertical pendula
US4303164A (en) * 1974-09-02 1981-12-01 Linden-Alimak Ab Structure for damping the oscillation of building cranes

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