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US4089215A Expired / Lapsed US ⏱️ 0.0 years remaining

Air flow transducer

Assignee: Autotronic Controls Corp
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Filing: 1977-04-01
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Granted: 1978-05-16
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Expires: 1997-04-01
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Abstract

Abstract An air flow transducer for measuring rate of air flow into an engine having a propensity to backfire includes a rotor with vanes disposed to intercept the air flow. The vanes are formed of low density plastic and affixed to a rotor. The trailing edges of the vanes are shaped to direct forces occasioned by backfire pressure waves to hold the vanes to the hub.

Inventors

  • 👤 Leonard Lee Chapin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 03:29
CPC Classifications
G; G01; G01F; G01F1/00; G01F1/05; G01F1/10; F; F02; F02M; F02M69/00; F02M69/46; F02M69/48; F02M9/00; F02M9/08; F02B; F02B1/00; F02B1/02; F02B1/04

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 223 words
An air flow transducer for measuring the rate of air flow into the intake manifold of an internal combustion engine having a propensity to backfire on occasion, said transducer comprising a flow tube forming a passageway, means for mounting said flow tube to pass the air flowing to said intake manifold through said passageway, a rotor having a shaft with a hub mounted thereon for rotation therewith and a plurality of vanes extending outwardly from said hub, means for mounting said shaft for rotation of said rotor within said passageway, and signal means for providing an electrical signal systematically related to the rate of rotation of said rotor, said vanes being equally spaced around the periphery of said hub and shaped to intercept air flowing through said passageway for movement by said air, said vanes being formed of low density plastic, each of said vanes having a thickened root at which it joins said hub, and each of said vanes having a trailing edge that slopes from said hub in the upstream direction at a substantial angle to the plane normal to said shaft to provide a reaction surface to any backfire pressure wave that forces said trailing edge in the direction of said hub in counteraction to forces created by said backfire pressure wave directed to tearing said vane from said hub.
Claim 2
Dependent Claim 223 words
An air flow transducer for measuring the rate of air flow into the intake manifold of an internal combustion engine having a propensity to backfire on occasion, said transducer comprising a flow tube forming a passageway, means for mounting said flow tube to pass the air flowing to said intake manifold through said passageway, a rotor having a shaft with a hub mounted thereon for rotation therewith and a plurality of vanes extending outwardly from said hub, means for mounting said shaft for rotation of said rotor within said passageway, and signal means for providing an electrical signal systematically related to the rate of rotation of said rotor, said vanes being equally spaced around the periphery of said hub and shaped to intercept air flowing through said passageway for movement by said air, said vanes being formed of low density plastic, each of said vanes having a thickened root at which it joins said hub, and each of said vanes having a trailing edge that slopes from said hub in the upstream direction at a substantial angle to the plane normal to said shaft to provide a reaction surface to any backfire pressure wave that forces said trailing edge in the direction of said hub in counteraction to forces created by said backfire pressure wave directed to tearing said vane from said hub.
Claim 3
Dependent Claim 15 words
A transducer according to claim 1 wherein said vanes are formed integrally with said hub.
Claim 4
Dependent Claim 16 words
A transducer according to claim 2 wherein said low density plastic is fiber reinforced foamed plastic.
Claim 5
Dependent Claim 20 words
A transducer according to claim 3 wherein said low density plastic is foamed polyurethane reinforced by glass and/or carbon fibers.
Claim 6
Dependent Claim 20 words
A transducer according to claim 2 wherein said vanes number two disposed at respective diametrically opposite locations on said hub.
Claim 7
Dependent Claim 27 words
A transducer according to claim 1 including means for deflecting and diffusing at least a portion of said backfire pressure wave from direct impingement on said vanes.
Claim 8
Dependent Claim 42 words
A transducer according to claim 1 wherein said means for mounting said shaft comprises an enlarged section at the manifold end of said shaft for deflecting and diffusing at least part of said backfire pressure waves from direct impingement on said vanes.

References Cited (Backward Citations)

US3788285A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-05-15 1981-11-14 1982-05-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-05-15 1985-11-14 1986-05-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-05-15 1989-11-14 1990-05-16 $7700.00 Window Closed / Lapsed

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