Patent US3019583A successfully refreshed from Google Patents.
Patent US3762223A successfully refreshed from Google Patents.
← Back to Patent Explorer
US3762223A Expired / Lapsed US ⏱️ 0.0 years remaining

Digital pressure transducer

Assignee: CONRAC AVIONIC SYSTEMS Corp A CORP OF
•
Filing: 1971-09-10
•
Granted: 1973-10-02
•
Expires: 1991-09-10
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract Fluid pressure is sensed by applying it differentially to a diaphragm, causing the diaphragm to vibrate at a natural frequency, and sensing the stressing of the diaphragm in terms of the resulting change in the natural frequency. The frequency of vibration is measured essentially by counting cycles and offsetting the count to introduce a reference pressure. Improved accuracy is obtained by forming the diaphragm of preferred magnetic materials having low temperature dependence of elasticity.

Inventors

  • 👤 R Feuer
  • 👤 D Ball

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 11:56
CPC Classifications
G; G01; G01L; G01L9/00; G01L9/0001; G01L9/0008; G01L9/0016

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 101 words
A pressure transducer, comprising in combination a resilient diaphragm formed of an alloy having substantially zero thermoelastic coefficient for oscillation frequencies higher than a predetermined threshold value, the form of the diaphragm being such that its natural frequency of oscillation is higher than said threshold value, structure for applying a fluid pressure differentially to the diaphragm to stress the same transversely, means for driving the so stressed diaphragm to oscillate at its natural frequency, sensing means responsive to the diaphragm movement, and means for deriving from the frequency of the sensed movement an indication of the magnitude of the applied pressure.
Claim 2
Dependent Claim 101 words
A pressure transducer, comprising in combination a resilient diaphragm formed of an alloy having substantially zero thermoelastic coefficient for oscillation frequencies higher than a predetermined threshold value, the form of the diaphragm being such that its natural frequency of oscillation is higher than said threshold value, structure for applying a fluid pressure differentially to the diaphragm to stress the same transversely, means for driving the so stressed diaphragm to oscillate at its natural frequency, sensing means responsive to the diaphragm movement, and means for deriving from the frequency of the sensed movement an indication of the magnitude of the applied pressure.
Claim 3
Dependent Claim 69 words
A pressure transducer according to claim 1, and in which said diaphragm consists essentially of about 48 percent iron, 42 percent nickel, 5 percent chromium and 2.5 percent titanium and has substantially zero thermoelastic coefficient for oscillation frequencies higher than a threshold value of about 800 cycles per second, and the form of the diaphragm is such that its natural frequency of oscillation is higher than said threshold value.
Claim 4
Dependent Claim 44 words
A pressure transducer according to claim 2, and in which said diapHragm driving means comprise an electrical winding magnetically coupled to the diaphragm, and circuit means for producing in the winding a current that varies periodically in definite phase relation to the diaphragm oscillation.
Claim 5
Dependent Claim 125 words
A pressure transducer, comprising in combination a resilient diaphragm, structure for applying a fluid pressure differentially to the diaphragm to stress the same transversely, means for driving the so stressed diaphragm to oscillate at its natural frequency, sensing means responsive to the diaphragm movement, means for developing clock pulses at a constant frequency higher than the frequency of diaphragm oscillation, means controlled by said sensing means for counting the clock pulses during a predetermined number of diaphragm oscillations and for offsetting the pulse count by the number of clock pulses that would occur during the same number of diaphragm oscillations at a predetermined reference pressure, and means responsive to the offset pulse count for indicating the excess of the applied pressure over the reference pressure.
Claim 6
Dependent Claim 125 words
A pressure transducer, comprising in combination a resilient diaphragm, structure for applying a fluid pressure differentially to the diaphragm to stress the same transversely, means for driving the so stressed diaphragm to oscillate at its natural frequency, sensing means responsive to the diaphragm movement, means for developing clock pulses at a constant frequency higher than the frequency of diaphragm oscillation, means controlled by said sensing means for counting the clock pulses during a predetermined number of diaphragm oscillations and for offsetting the pulse count by the number of clock pulses that would occur during the same number of diaphragm oscillations at a predetermined reference pressure, and means responsive to the offset pulse count for indicating the excess of the applied pressure over the reference pressure.

References Cited (Backward Citations)

US2796863A Cited
US3071725A Cited
US3425281A Cited
US3295360A Cited
US3503263A Cited
US3595069A Cited
US3668930A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-10-01 1977-04-02 1977-10-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-10-01 1981-04-02 1981-10-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-10-01 1985-04-02 1985-10-02 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag