GB1054973A - - Google Patents

Info

Publication number
GB1054973A
GB1054973A GB1054973DA GB1054973A GB 1054973 A GB1054973 A GB 1054973A GB 1054973D A GB1054973D A GB 1054973DA GB 1054973 A GB1054973 A GB 1054973A
Authority
GB
United Kingdom
Prior art keywords
link
diaphragm
aneroid
static
drives
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
Other languages
English (en)
Publication of GB1054973A publication Critical patent/GB1054973A/en
Active legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L7/00—Measuring the steady or quasi-steady pressure of a fluid or a fluent solid material by mechanical or fluid pressure-sensitive elements
GB1054973D Active GB1054973A (de)

Publications (1)

Publication Number Publication Date
GB1054973A true GB1054973A (de)

Family

ID=1758439

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1054973D Active GB1054973A (de)

Country Status (1)

Country Link
GB (1) GB1054973A (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3817617A1 (de) * 1988-05-25 1989-07-20 Daimler Benz Ag Abgasturbolader fuer eine brennkraftmaschine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3817617A1 (de) * 1988-05-25 1989-07-20 Daimler Benz Ag Abgasturbolader fuer eine brennkraftmaschine

Similar Documents

Publication Publication Date Title
US3318146A (en) Pressure sensing instrument for aircraft
US2424511A (en) Aircraft flight instrument
EP0167585A4 (de) Druckempfindliches fühlerinstrument für luftfahrzeug.
GB935728A (en) A device for calibrating pressure sensitive instruments
Richardson Wind-Tunnel Calibrations of a Combined Pitot-Static Tube, Vane-Type Flow-Direction Transmitter, and Stagnation-Temperature Element at Mach Numbers From 0.60 to 2.87
GB1054973A (de)
Larson et al. Calibrations and comparisons of pressure-type airspeed-altitude systems of the X-15 airplane from subsonic to high supersonic speeds
US2927460A (en) Speed indicator for airplanes
US2265045A (en) Pressure gauge, and more particularly a barograph
CN112504547A (zh) 一种长期稳定性的高精度动压测量方法及系统
Brunn et al. Mach Number Measurements and Calibrations During Flight at High Speeds and at High Altitudes Including Data for the D-558-II Research Airplane
US2807958A (en) Means for indicating equivalent airspeed
US3942376A (en) Diaphragm type angle of attack indicator
US2223705A (en) Pressure gauge with barometric correction
US2606444A (en) Air-speed indicator with altitude correction
US3222932A (en) Pressure responsive instrument
Luu et al. Correction of error perception of static pressure in the air data computer
US2271142A (en) Fluid-speed meter
US3739638A (en) Airspeed and altitude measuring device
GB1053985A (de)
US3738167A (en) Airspeed and altitude measuring device
US2363143A (en) Air-speed indicator
US2402618A (en) Gross weight indicator for airplanes
Armistead et al. Flight calibration tests of a nose-boom-mounted fixed hemispherical flow-direction sensor
SU313091A1 (ru) Расходомер пыли