GB924765A - Improvements in or relating to fluid pressure responsive instruments - Google Patents

Improvements in or relating to fluid pressure responsive instruments

Info

Publication number
GB924765A
GB924765A GB882761A GB882761A GB924765A GB 924765 A GB924765 A GB 924765A GB 882761 A GB882761 A GB 882761A GB 882761 A GB882761 A GB 882761A GB 924765 A GB924765 A GB 924765A
Authority
GB
United Kingdom
Prior art keywords
pressure
instrument
responsive
accelerated
closed end
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
GB882761A
Inventor
Walter Leonard Oliver
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.)
SECR AVIATION
Minister of Aviation
Original Assignee
SECR AVIATION
Minister of Aviation
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 SECR AVIATION, Minister of Aviation filed Critical SECR AVIATION
Priority to GB882761A priority Critical patent/GB924765A/en
Publication of GB924765A publication Critical patent/GB924765A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L13/00Devices or apparatus for measuring differences of two or more fluid pressure values
    • G01L13/02Devices or apparatus for measuring differences of two or more fluid pressure values using elastically-deformable members or pistons as sensing elements

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

924,765. Measuring pressure electrically. MINISTER OF AVIATION. Feb. 22, 1962 [March 10, 1961], No. 8827/61. Class 40 (1). Inertial forces acting on a pressure-responsive member 20 of relatively low density, are substantially cancelled when the body 11 of a pressure-responsive instrument is accelerated in either sense in the direction of member movement, the annular responsive member 20 being supported in a liquid 17 of relatively high density by the common closed end 14 of two extensible tubular members 18, 19, or two parts of a single such member. Gas or liquid pressure applied through connection 22 acts on the closed end 14 of the chamber 18 and thus causes slider 26 insulatedly mounted on the end member 14 to move relatively to a potentiometer resistor 23 mounted on the instrument case 11. Alternatively, the chambers 18, 19 may be differentially connected to separate pressure sources. The open ends 15, 16 of members 18, 19 are sealed on to the casing 11, so that when the instrument is accelerated in the direction movement of member 14, then the body 20 and member 14 tend to move in opposite directions so that the effect of acceleration on the composite component is substantially eliminated. Specification 899,494 is referred to.
GB882761A 1961-03-10 1961-03-10 Improvements in or relating to fluid pressure responsive instruments Expired GB924765A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB882761A GB924765A (en) 1961-03-10 1961-03-10 Improvements in or relating to fluid pressure responsive instruments

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB882761A GB924765A (en) 1961-03-10 1961-03-10 Improvements in or relating to fluid pressure responsive instruments

Publications (1)

Publication Number Publication Date
GB924765A true GB924765A (en) 1963-05-01

Family

ID=9859983

Family Applications (1)

Application Number Title Priority Date Filing Date
GB882761A Expired GB924765A (en) 1961-03-10 1961-03-10 Improvements in or relating to fluid pressure responsive instruments

Country Status (1)

Country Link
GB (1) GB924765A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5367944A (en) * 1991-10-04 1994-11-29 Fanuc Robotics North America, Inc. Sensor for use in a fluid transfer system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5367944A (en) * 1991-10-04 1994-11-29 Fanuc Robotics North America, Inc. Sensor for use in a fluid transfer system

Similar Documents

Publication Publication Date Title
GB927075A (en) Improvements relating to pressure sensing devices and methods of manufacture of suchdevices
GB924765A (en) Improvements in or relating to fluid pressure responsive instruments
GB1512895A (en) Differential-pressure overflow valve assembly
GB934465A (en) Fluid pressure sensitive electrical signal generating device with flexural pivot
USD187351S (en) Aircraft
GB924665A (en) Improvements in or relating to fluid pressure responsive instruments
GB938081A (en) Improvements in or relating to pilot static pressure sensing devices
USD193357S (en) Aircraft flight instrument
USD187352S (en) Amcraft
GB759802A (en) Improvements in or relating to respirator
GB900578A (en) Rapid response pressure instrument
GB903186A (en) Improvements in and relating to aircraft instruments operated by air pressure
US3566693A (en) Fluidic altitude sensor
Bueckner Remarks on the Germain-Liger family of approximations to the equation of state of an ideal gas
USD187353S (en) Aircraft
GB1204010A (en) Open-loop fluidic analog accelerometer
USD189138S (en) Oscillograph
Essers Max Valier: A pioneer of space travel
SU611154A1 (en) Acceleration sensor
USD190763S (en) Aircraft flight instrument
NAZAROV et al. An analytic solution of a system of equations for the axisymmetric flow of an incompressible fluid(Strict general solution of velocity potential and stream function of partial differential equation system for incompressible axisymmetric ideal fluid flow)
USD187350S (en) Aircraft
GB1079839A (en) Improvements in or relating to restriction indicators for fluid filters
WILLIAMS A fluidic linear accelerometer for ship motion sensing(Fluidic linear nozzle-flapper valve accelerometer for ship motion sensing, describing circuit configuration and performance tests)
MOSELEY Static longitudinal stability characteristics of various Mercury escape configurations and of a proposed alternate escape configuration for Mach numbers of 0. 05 to 9. 60(Static longitudinal stability characteristics of Mercury escape configurations and alternate escape configuration for Mach numbers 0. 05 to 9. 60)