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US3113636A Expired / Lapsed US ⏱️ 0.0 years remaining

Jet noise silencing appartus for an aircraft

Assignee: Rolls Royce PLC
•
Filing: 1960-10-07
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Granted: 1963-12-10
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Expires: 1980-10-07
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Abstract

No abstract record available.

Inventors

  • 👤 Brown David Morris
  • 👤 Spooner Hubert

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 09:01
CPC Classifications
B; B64; B64D; B64D27/00; B64D27/02; B64D27/16; B64D27/20; F; F02; F02K; F02K1/00; F02K1/40

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 127 words
AN AIRCRAFT HAVING A FUSELAGE, AT LEAST ONE GAS TURBINE ENGINE, JET NOISE SILENCING APPARATUS DISPOSED AT THE REAR END OF THE FUSELAGE, SAID JET NOISE SILENCING APPARATUS DISCHARGING EXHAUST GASES FROM SAID AT LEAST ONE ENGINE AND COMPRISING AT LEAST ONE PAIR OF HORIZONTALLY SPACED SILENCERS, EACH OF SAID SILENCERS COMPRISING A ROW OF VERTICALLY ALIGNED JET NOZZLES, A DUCT DISPOSED BETWEEN SAID SILENCERS AND HAVING AIR INTAKE MEANS OPENING ON SAID FUSELAGE ADJACENT THE REAR END THEREOF FOR RECEIVING BOUNDARY AIR PROGRESSING ALONG THE SAME, SAID DUCT AND SAID NOZZLES TERMINATING IN SUBSTANTIALLY THE SAME TRANSVERSE PLANE OF THE FUSELAGE SO THAT JETS ISSUING FROM THE ROWS OF VERTICAL NOZZLES ARE SEPARATED BY A RELATIVELY DENSE AND SLOW MOVING STREAM OF FUSELAGE BOUNDARY LAYER AIR.
Claim 2
Dependent Claim 127 words
AN AIRCRAFT HAVING A FUSELAGE, AT LEAST ONE GAS TURBINE ENGINE, JET NOISE SILENCING APPARATUS DISPOSED AT THE REAR END OF THE FUSELAGE, SAID JET NOISE SILENCING APPARATUS DISCHARGING EXHAUST GASES FROM SAID AT LEAST ONE ENGINE AND COMPRISING AT LEAST ONE PAIR OF HORIZONTALLY SPACED SILENCERS, EACH OF SAID SILENCERS COMPRISING A ROW OF VERTICALLY ALIGNED JET NOZZLES, A DUCT DISPOSED BETWEEN SAID SILENCERS AND HAVING AIR INTAKE MEANS OPENING ON SAID FUSELAGE ADJACENT THE REAR END THEREOF FOR RECEIVING BOUNDARY AIR PROGRESSING ALONG THE SAME, SAID DUCT AND SAID NOZZLES TERMINATING IN SUBSTANTIALLY THE SAME TRANSVERSE PLANE OF THE FUSELAGE SO THAT JETS ISSUING FROM THE ROWS OF VERTICAL NOZZLES ARE SEPARATED BY A RELATIVELY DENSE AND SLOW MOVING STREAM OF FUSELAGE BOUNDARY LAYER AIR.

References Cited (Backward Citations)

US2335134A Cited
US2395919A Cited
US2633703A Cited
US2650752A Cited
US2840325A Cited
GB744196A Cited
US2973825A Cited
US3025667A Cited
US2988302A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1966-12-09 1967-06-10 1967-12-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1970-12-09 1971-06-10 1971-12-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1974-12-09 1975-06-10 1975-12-10 $7700.00 Window Closed / Lapsed

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