GB880361A - Dual string force transducer - Google Patents

Dual string force transducer

Info

Publication number
GB880361A
GB880361A GB1522058A GB1522058A GB880361A GB 880361 A GB880361 A GB 880361A GB 1522058 A GB1522058 A GB 1522058A GB 1522058 A GB1522058 A GB 1522058A GB 880361 A GB880361 A GB 880361A
Authority
GB
United Kingdom
Prior art keywords
wire
wires
mass
force
difference
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
GB1522058A
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.)
Borg Warner Corp
Original Assignee
Borg Warner Corp
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 Borg Warner Corp filed Critical Borg Warner Corp
Publication of GB880361A publication Critical patent/GB880361A/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
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P15/097Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by vibratory elements
    • G01P15/10Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by vibratory elements by vibratory strings

Landscapes

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

Abstract

880,361. Force transducers; accelerometers; pressure gauges. BORG-WARNER CORPORATION. May 12, 1958 [May 17, 1957], No. 15220/58. Class 40 (1). [Also in Groups XIX and XL (c)] A force-measuring apparatus comprises a force-responsive mass with two non-magnetic wires extending from opposite sides of it, each wire being maintained in oscillation at its resonant frequency under tension in a magnetic field, means for suspending the mass so that it can move axially relative to the wires and thus differentially alter the tensions in the wires, an electronic amplifier having feedback to sustain the oscillations in the wires at a constant amplitude, and means to heterodyne the outputs of the two amplifiers and measure the difference frequency which is a measure of the axial force applied to the mass. Such a system is substantially unaffected by forces at right angles to the wires or by changes in ambient temperature. The force to be measured may for example be due to acceleration or fluid pressure. Accelerometer (Fig. 1).-A mass 16 is supported in a housing by an annular flexible diaphragm 18 so that it can move axially as far as stops 20. On each side of the housing is a cylindrical shell 24 carrying a cap 25 in which is mounted an insulated terminal post 26. A wire 28 is stretched between this post and a tab 27 on the mass 16 and passes through a semicircular magnet 29. Each wire is non-magnetic and is preferably made of tungsten. Axial displacement of the mass will produce an increase of tension in one wire and a decrease in the other so that the difference between their resonant frequencies (originally equal) is a measure of the force exerted on the mass. Pressure gauge (Fig. 4).-The mass 16 of the accelerometer is here replaced by a pin 102 which is attached to the centre portion of a diaphragm 94 and to hubs 98, 100 which are connected by thin webs 99 to mounting plates 92, 93. The centre portion of the diaphragm can move sideways by virtue of a thin portion 97. A cavity 95 on one side of the diaphragm communicates with a pressure source via a port 103, and a similar cavity 96 on the other side communicates with another pressure source via a port 104, so that axial movement of the pin 102 is a measure of the difference between the two pressures. One pressure source can be omitted if the absolute pressure of the other is to be determined. Modifications.-The two wires 28 can be unequal in length, density, cross-sectional area or modulus of elasticity if it is intended that the difference between their resonant frequencies shall be finite for zero applied force. The wires can be circular, ribbon-like or polygonal in cross-section. Conductively-coated strings can be used instead of wires. Circuitry (Fig. 3).-Each wire 28 is connected to a separate amplifier of the type shown here and is joined in a Wheatstone bridge with a similar wire 36 which is not in a magnetic field. This wire is preferably in the same housing as the wire 28 so that both are at the same temperature. Any change in the impedance of the wire 28, due to a change in the back E.M.F. induced in it by the magnetic field, alters the signal applied to three cascaded amplifier valves 37, 50, 62. A voltage is fed back from the anode of valve 50 to maintain oscillations in the wire 28, the amplitude being kept constant by an A.G.C. circuit fed from the output of valve 62 via a rectifier bridge 75. The output signal at terminal 72 is mixed with a similar signal from the other amplifier in a conventional heterodyning circuit, and the difference signal is selected by a low-pass filter and displayed on a meter.
GB1522058A 1957-05-17 1958-05-12 Dual string force transducer Expired GB880361A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US66000957A 1957-05-17 1957-05-17

Publications (1)

Publication Number Publication Date
GB880361A true GB880361A (en) 1961-10-18

Family

ID=24647753

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1522058A Expired GB880361A (en) 1957-05-17 1958-05-12 Dual string force transducer

Country Status (4)

Country Link
CH (1) CH364641A (en)
DE (1) DE1097718B (en)
FR (1) FR1206800A (en)
GB (1) GB880361A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541866A (en) * 1967-02-24 1970-11-24 Csf Vibrating string accelerometers
CN115655453A (en) * 2022-10-26 2023-01-31 西南交通大学 Novel broadband and impact-resistant tension vibration acceleration sensor and use method thereof

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1202025B (en) * 1961-04-10 1965-09-30 Borg Warner Device for measuring mechanical forces, in particular accelerometers responsive to inertial forces
DE1220170B (en) * 1962-03-29 1966-06-30 Gen Precision Inc Height measuring arrangement
FR1344358A (en) * 1962-10-05 1963-11-29 Csf Improvements to vibrating string accelerometers
DE3166254D1 (en) * 1980-04-03 1984-10-31 Giers Fluid-pressure responsive apparatus
CN115165267A (en) * 2022-08-17 2022-10-11 重庆大学 Method for rapidly detecting weak side end of bridge bearing based on vehicle vibration signal

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE729894C (en) * 1936-05-09 1942-12-19 Deutsches Reich Vertreten Durc Arrangement for measuring the speed over the ground of a watercraft or aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541866A (en) * 1967-02-24 1970-11-24 Csf Vibrating string accelerometers
CN115655453A (en) * 2022-10-26 2023-01-31 西南交通大学 Novel broadband and impact-resistant tension vibration acceleration sensor and use method thereof
CN115655453B (en) * 2022-10-26 2023-07-18 西南交通大学 Broadband, impact-resistant stretching vibration acceleration sensor and use method thereof

Also Published As

Publication number Publication date
CH364641A (en) 1962-09-30
DE1097718B (en) 1961-01-19
FR1206800A (en) 1960-02-11

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