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US3568694A Expired / Lapsed US ⏱️ 0.0 years remaining

Jet engine installation for noise control

Assignee: Lockheed Martin Corp
•
Filing: 1968-05-08
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Granted: 1971-03-09
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Expires: 1988-05-08
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Abstract

Abstract A jet or fan-jet engine installation wherein inlet noise is reduced on takeoff and landing by changing the direction of the noise radiated from the inlet and by using an inlet duct having soundproofing. Exhaust noise is reduced by use of tertiary air bleed (or quaternary bleed) to reduce the shearing velocity of the final jet.

Inventors

  • 👤 Clarence L Johnson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 22:43
CPC Classifications
B; B64; B64D; B64D33/00; B64D33/02; F; F02; F02C; F02C7/00; F02C7/04; F02C7/045; F02K; F02K1/00; F02K1/38; B64D2033/0206; B64D2033/0266; B64D2033/0286; Y; Y10; Y10T; Y10T137/00; Y10T137/0536

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 82 words
The combination comprising a nacelle, an engine mounted in said nacelle, an inlet on the forward end of the nacelle, an upwardly opening inlet, a deflector at the rear of the last mentioned inlet for deflecting air into the nacelle, and a vane positioned in the first mentioned inlet and rotatable about a horizontal axis in the center of the inlet and transverse to the longitudinal axis of the inlet, said vane when closed sloping down toward the rear of the inlet.
Claim 2
Dependent Claim 82 words
The combination comprising a nacelle, an engine mounted in said nacelle, an inlet on the forward end of the nacelle, an upwardly opening inlet, a deflector at the rear of the last mentioned inlet for deflecting air into the nacelle, and a vane positioned in the first mentioned inlet and rotatable about a horizontal axis in the center of the inlet and transverse to the longitudinal axis of the inlet, said vane when closed sloping down toward the rear of the inlet.

References Cited (Backward Citations)

US2869670A Cited
US3347496A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-03-08 1974-09-07 1975-03-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-03-08 1978-09-07 1979-03-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-03-08 1982-09-07 1983-03-09 $7700.00 Window Closed / Lapsed

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