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US3724477A Expired / Lapsed US ⏱️ 0.0 years remaining

Laminar rate sensor

Assignee: General Electric Co
•
Filing: 1972-01-10
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Granted: 1973-04-03
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Expires: 1992-01-10
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Abstract

Abstract A laminar fluidic angular rate sensor for sensing the rate of angular rotation of the sensor which includes a supply passageway; at least two receiver passageways; vents, at least one of which is located between the two receiver passageways and is aligned with the supply passageways; and a cavity which are of a configuration and location such that fluid flowing through the supply passageway forms a laminar fluid stream which is capable of being received by the receiver passageways in the laminar state. The Reynolds number of the fluid forming the laminar fluid stream is preferably within the rante of 200-1500.

Inventors

  • 👤 D Rexford

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 20:20
CPC Classifications
F; F15; F15C; F15C1/00; F15C1/08; F15C1/005; F15C1/14; Y; Y10; Y10T; Y10T137/00; Y10T137/206; Y10T137/2229; Y10T137/2251; Y10T137/2256

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 231 words
A laminar fluidic angular rate sensing device for sensing the rate of angular rotation of the device in a plane for use with a fluid having a Reynolds number less than 1,500 comprising: a. a substantially linear supply passageway having at its downstream end a nozzle portion for forming a laminar fluid stream, the length of said supply passageway being at least 10 times the smallest cross-sectional dimension of said nozzle portion; b. two substantially linear receiver passageways capable of receiving a portion of said laminar fluid stream from said supply passageway, the cross-sectional area of each of said receiver passageways being no less than the cross-sectional area of said nozzle portion; c. a substantially closed cavity located between said supply and receiver passageways and through which said laminar fluid stream flows; and d. venting means in communication with said cavity a portion of which is located between said receiver passageways for helping to maintain said fluid stream flowing through said cavity in the laminar state by presenting substantially no impedance to fluid flow therethrough; whereby rotation of said device in a plane which includes the exit of said supply passageway and the entrances of said receiver passageways causes deflection of said laminar fluid stream to produce a pressure differential between and within said receiver passageways which is proportional to the angular rate of rotation of said device within the plane.
Claim 2
Dependent Claim 231 words
A laminar fluidic angular rate sensing device for sensing the rate of angular rotation of the device in a plane for use with a fluid having a Reynolds number less than 1,500 comprising: a. a substantially linear supply passageway having at its downstream end a nozzle portion for forming a laminar fluid stream, the length of said supply passageway being at least 10 times the smallest cross-sectional dimension of said nozzle portion; b. two substantially linear receiver passageways capable of receiving a portion of said laminar fluid stream from said supply passageway, the cross-sectional area of each of said receiver passageways being no less than the cross-sectional area of said nozzle portion; c. a substantially closed cavity located between said supply and receiver passageways and through which said laminar fluid stream flows; and d. venting means in communication with said cavity a portion of which is located between said receiver passageways for helping to maintain said fluid stream flowing through said cavity in the laminar state by presenting substantially no impedance to fluid flow therethrough; whereby rotation of said device in a plane which includes the exit of said supply passageway and the entrances of said receiver passageways causes deflection of said laminar fluid stream to produce a pressure differential between and within said receiver passageways which is proportional to the angular rate of rotation of said device within the plane.
Claim 3
Dependent Claim 23 words
A device as in claim 1 wherein the height of said cavity is substantially the same as the height of said nozzle portion.
Claim 4
Dependent Claim 26 words
A device as in claim 1 wherein the height of said cavity is at least ten times a great as the height of said nozzle portion.
Claim 5
Dependent Claim 26 words
A device as in claim 1 wherein the length of said cavity is no greater than 50 times the smallest cross-sectional dimension of said nozzle portion.

References Cited (Backward Citations)

US3362421A Cited
US3310985A Cited
US3429323A Cited
US3469593A Cited
US3450145A Cited
US3457934A Cited
US3574309A Cited
US3636964A Cited
US3670755A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-04-02 1976-10-02 1977-04-03 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-04-02 1980-10-02 1981-04-03 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-04-02 1984-10-02 1985-04-03 $7700.00 Window Closed / Lapsed

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