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US3905445A Expired / Lapsed US ⏱️ 0.0 years remaining

Vortex turbulence noise generation suppressor

Assignee: RTX BBN Technologies Corp
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Filing: 1973-07-20
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Granted: 1975-09-16
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Expires: 1993-07-20
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Abstract

Abstract This disclosure deals with structures for suppressing a substantial percentage of noise that normally is attendant upon vortex generation from jet engines, blown flaps, turbine outlets and the like, involving successive tubular sections of successively reduced width disposed longitudinally, preferably along a common axis.

Inventors

  • 👤 Terry D Scharton

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 04:14
CPC Classifications
F; F01; F01N; F01N13/00; F01N13/08; F01N13/082; F02; F02K; F02K1/00; F02K1/40

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 114 words
A noise generation suppresSor for breaking up the exhaust of a jet outlet into a plurality of streams while minimizing flowdividing drag, having, in combination, means including a plurality of successive longitudinally extending passages of successively smaller cross-dimension for dividing said exhaust into a plurality of streams and for breaking up the vortex pattern of said exhaust, each of said passages having an inlet at one end and an outlet at the opposite end, each inlet being located adjacent the outlet of the preceding passage and remote from the inlet of the preceding passage, and each passage being substantially freely open and devoid of transverse sub-division along said cross-dimension throughout most of its length.
Claim 2
Dependent Claim 114 words
A noise generation suppresSor for breaking up the exhaust of a jet outlet into a plurality of streams while minimizing flowdividing drag, having, in combination, means including a plurality of successive longitudinally extending passages of successively smaller cross-dimension for dividing said exhaust into a plurality of streams and for breaking up the vortex pattern of said exhaust, each of said passages having an inlet at one end and an outlet at the opposite end, each inlet being located adjacent the outlet of the preceding passage and remote from the inlet of the preceding passage, and each passage being substantially freely open and devoid of transverse sub-division along said cross-dimension throughout most of its length.
Claim 3
Dependent Claim 19 words
A noise generation suppressor as claimed in claim 1 and in which said passages are of about equal length.
Claim 4
Dependent Claim 24 words
A noise generation suppressor as claimed in claim 1 and in which each of said passages overlaps only a portion of the preceding passage.
Claim 5
Dependent Claim 18 words
A noise generation suppressor as claimed in claim 1 and in which said passages have substantially cylindrical cross-section.
Claim 6
Dependent Claim 18 words
A noise generation suppressor as claimed in claim 1 and in which said passages have substantially rectangular cross-section.
Claim 7
Dependent Claim 17 words
A noise generation suppressor as claimed in claim 1 and in which said passages comprise plate members.
Claim 8
Dependent Claim 18 words
A noise generation suppressor as claimed in claim 1 and in which said passage outlets are rectangular slits.
Claim 9
Dependent Claim 34 words
A noise generation suppressor as claimed in claim 1 and in which said jet outlet has associated therewith a converging potential core and in which said passages are located within the converging potential core.

References Cited (Backward Citations)

US2995200A Cited
US3528336A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-09-15 1979-03-17 1979-09-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-09-15 1983-03-17 1983-09-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-09-15 1987-03-17 1987-09-16 $7700.00 Window Closed / Lapsed

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