US4398667A
Expired / Lapsed
US
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Apparatus and method for jet noise suppression
Assignee: National Aeronautics and Space Administration
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Filing: 1981-02-27
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Granted: 1983-08-16
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Expires: 2001-02-27
Abstract
Abstract A method and apparatus for jet noise suppression through control of the static pressure of the jet and control of the rate of entrainment of ambient fluid into the jet downstream of the exhaust nozzle is disclosed and serving to regulate the momentum flux over an extended region of the jet, affecting Reynolds stresses in the jet and the spreading angle of the jet. Static pressure is controlled through a long hollow, porous nozzle plug centerbody which may be selectively vented to ambient conditions, connected to a vacuum source, or supplied with fluids of various densities for injection into the stream. Additionally, sound in the jet may be channeled along the nozzle plug centerbody by injecting coolant such as a cryogenic fluid through the center-body into the jet.
Inventors
- 👤 Lucio Maestrello
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 18:20
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/28; F02K1/34
Claims Analysis
Total Claims: 25
Claim 1
Independent Claim
96 words
A method of directing the sound in a jet comprising the steps of: (a) providing a jet exhaust nozzle; (b) providing a porous centerbody internally along the entire nozzle length with a portion thereof extending rearward from the exhaust nozzle and downstream in the jet; (c) injecting a cryogenic fluid coolant through the porous centerbody into the jet thereby; (d) creating a heat sink along the jet extending downstream of the exhaust nozzle whereby the heat sink will attract acoustical energy in the jet and channel the jet noise in the direction of the heat sink.
Claim 2
Independent Claim
96 words
A method of directing the sound in a jet comprising the steps of: (a) providing a jet exhaust nozzle; (b) providing a porous centerbody internally along the entire nozzle length with a portion thereof extending rearward from the exhaust nozzle and downstream in the jet; (c) injecting a cryogenic fluid coolant through the porous centerbody into the jet thereby; (d) creating a heat sink along the jet extending downstream of the exhaust nozzle whereby the heat sink will attract acoustical energy in the jet and channel the jet noise in the direction of the heat sink.
Claim 3
Dependent Claim
35 words
The method of claim 1 including the further step of controllably directing the centerbody portion extending rearward from the exhaust nozzle angularly relative to the nozzle to channel the jet noise in a desired direction.
Claim 4
Independent Claim
75 words
A device for directing the sound in a jet comprising: a jet exhaust nozzle; means for creating a heat sink along the jet emanating from and extending downstream of said exhaust nozzle whereby acoustical energy in the jet will be attracted to the heat sink and channeled in the direction of said heat sink and, means for controllably directing the heat sink angularly relative to said nozzle to channel the noise in a desired direction.
Claim 5
Independent Claim
75 words
A device for directing the sound in a jet comprising: a jet exhaust nozzle; means for creating a heat sink along the jet emanating from and extending downstream of said exhaust nozzle whereby acoustical energy in the jet will be attracted to the heat sink and channeled in the direction of said heat sink and, means for controllably directing the heat sink angularly relative to said nozzle to channel the noise in a desired direction.
Claim 6
Independent Claim
99 words
A method of suppressing noise in a jet comprising the steps of: (a) providing a jet exhaust nozzle from which the jet exits; (b) providing an elongated porous member fixed within said nozzle and having a portion thereof projecting rearward from the center of said jet exhaust nozzle and downstream in the jet; thereby, (c) creating a pressure difference between the jet and the interior of the porous member to affect the static pressure in the jet downstream of the exhaust nozzle and influence the rate of entrainment of ambient fluid into the jet downstream of the exhaust nozzle.
Claim 7
Independent Claim
99 words
A method of suppressing noise in a jet comprising the steps of: (a) providing a jet exhaust nozzle from which the jet exits; (b) providing an elongated porous member fixed within said nozzle and having a portion thereof projecting rearward from the center of said jet exhaust nozzle and downstream in the jet; thereby, (c) creating a pressure difference between the jet and the interior of the porous member to affect the static pressure in the jet downstream of the exhaust nozzle and influence the rate of entrainment of ambient fluid into the jet downstream of the exhaust nozzle.
Claim 8
Dependent Claim
39 words
The method of claim 4 including the further step of controllably inducing a curvature in the porous member downstream of the exhaust nozzle whereby the jet may be controllably directed away from a course normal to the exhaust nozzle.
Claim 9
Dependent Claim
47 words
The method of claim 4 including the further steps of telescopically extending the porous member downstream of the exhaust nozzle when maximum noise suppression is desired and retracting the porous member toward the interior of the exhaust nozzle when maximum propulsive efficiency and fuel economy is desired.
Claim 10
Dependent Claim
76 words
The method of claim 4 wherein the porous member is projected along the jet to a distance downstream from the jet exit equal to at least 10D, D being the average distance from the outer surface of the porous member fixed portion to the exhaust nozzle wall measured at the jet exit and wherein the step of creating a pressure difference is accomplished along the length of the porous member portion downstream of the jet exit.
Claim 11
Independent Claim
129 words
A method of suppressing noise in a jet comprising the steps of: (a) providing a jet exhaust nozzle from which the jet exits; (b) providing an elongated substantially equal diameter hollow nozzle plug centerbody; (c) extending the hollow nozzle plug centerbody rearward from the jet equal to at least 10D, D being the average distance from the outer surface of the centerbody to the exhaust nozzle wall measured at the jet exit; (d) providing a pressure source for producing a pressure differential between the jet and the interior of the hollow centerbody along the length of the centerbody downstream of the jet exit to affect the static pressure in the jet stream and influence the rate of entrainment of ambient fluid into the jet downstream of the exhaust nozzle.
Claim 12
Independent Claim
129 words
A method of suppressing noise in a jet comprising the steps of: (a) providing a jet exhaust nozzle from which the jet exits; (b) providing an elongated substantially equal diameter hollow nozzle plug centerbody; (c) extending the hollow nozzle plug centerbody rearward from the jet equal to at least 10D, D being the average distance from the outer surface of the centerbody to the exhaust nozzle wall measured at the jet exit; (d) providing a pressure source for producing a pressure differential between the jet and the interior of the hollow centerbody along the length of the centerbody downstream of the jet exit to affect the static pressure in the jet stream and influence the rate of entrainment of ambient fluid into the jet downstream of the exhaust nozzle.
Claim 13
Dependent Claim
70 words
The method of claim 8 including the further steps of: (a) telescopically extending the centerbody downstream of the exhaust nozzle when maximum noise suppression is desired; (b) retracting the centerbody toward the interior of the exhaust nozzle when maximum propulsive efficiency and fuel economy is desired; and (c) controllably inducing a curvature in the centerbody downstream of the exhaust nozzle whereby the jet may be directed in a desired course.
Claim 14
Independent Claim
166 words
A method of suppressing noise in a jet operating in an ambient fluid comprising the steps of: (a) providing a jet exhaust nozzle from which the jet exits; (b) providing an elongated hollow nozzle plug centerbody supplied with perforations about the exterior surface thereof, the number and size of the perforations being related to the length of the centerbody and the maximum mass flow of the jet; (c) extending a portion of the centerbody rearward from the exhaust nozzle to a distance downstream equal to at least 10D, D being the average distance from the outer surface of the centerbody portion within the exhaust nozzle to the exhaust nozzle wall measured at the jet exit; (d) providing a pressure source for producing a pressure differential between the jet and the interior of the centerbody downstream of the jet; and (e) regulating the pressure differential along the centerbody length to influence the rate of entrainment of the ambient fluid into the jet downstream of the exhaust nozzle.
Claim 15
Independent Claim
166 words
A method of suppressing noise in a jet operating in an ambient fluid comprising the steps of: (a) providing a jet exhaust nozzle from which the jet exits; (b) providing an elongated hollow nozzle plug centerbody supplied with perforations about the exterior surface thereof, the number and size of the perforations being related to the length of the centerbody and the maximum mass flow of the jet; (c) extending a portion of the centerbody rearward from the exhaust nozzle to a distance downstream equal to at least 10D, D being the average distance from the outer surface of the centerbody portion within the exhaust nozzle to the exhaust nozzle wall measured at the jet exit; (d) providing a pressure source for producing a pressure differential between the jet and the interior of the centerbody downstream of the jet; and (e) regulating the pressure differential along the centerbody length to influence the rate of entrainment of the ambient fluid into the jet downstream of the exhaust nozzle.
Claim 16
Dependent Claim
66 words
The method of claim 10 including the further steps of: (a) extending the centerbody downstream of the exhaust nozzle when maximum noise suppression is desired; (b) retracting the centerbody toward the interior of the exhaust nozzle when maximum propulsive efficiency and fuel economy is desired; and, (c) controllably inducing a curvature in the centerbody downstream of the exhaust nozzle whereby the jet may be controllably directed.
Claim 17
Dependent Claim
23 words
The method of claim 10 wherein the perforations through said centerbody permit flow therethrough equivalent to 10-15% of the jet mass flow rate.
Claim 18
Dependent Claim
116 words
A jet noise suppression device comprising: a jet exhaust nozzle; an elongated hollow member having a portion thereof fixed within said nozzle and a portion centrally extending in the jet downstream of said nozzle; said hollow member being of a substantially constant diameter along the length thereof; a porous wall serving as the exterior surface of said elongated hollow member on at least the portion thereof extending in the jet downstream of said nozzle; and, pressure means connected to said elongated hollow member, said pressure means serving to affect the static pressure in the jet through said porous wall to influence the rate of entrainment of ambient fluid into the jet downstream of said exhaust nozzle.
Claim 19
Dependent Claim
116 words
A jet noise suppression device comprising: a jet exhaust nozzle; an elongated hollow member having a portion thereof fixed within said nozzle and a portion centrally extending in the jet downstream of said nozzle; said hollow member being of a substantially constant diameter along the length thereof; a porous wall serving as the exterior surface of said elongated hollow member on at least the portion thereof extending in the jet downstream of said nozzle; and, pressure means connected to said elongated hollow member, said pressure means serving to affect the static pressure in the jet through said porous wall to influence the rate of entrainment of ambient fluid into the jet downstream of said exhaust nozzle.
Claim 20
Dependent Claim
77 words
A noise suppression device for a jet operating in an ambient fluid comprising: a jet exhaust nozzle; means for influencing the rate of entrainment of ambient fluid into the jet emanating from said nozzle; said means including an elongated hollow porous nozzle plug centerbody member having a length thereof fixed within said nozzle and a length thereof extending downstream in the jet emanating from said jet exhaust nozzle; and pressure means connected to said porous centerbody member.
Claim 21
Dependent Claim
77 words
A noise suppression device for a jet operating in an ambient fluid comprising: a jet exhaust nozzle; means for influencing the rate of entrainment of ambient fluid into the jet emanating from said nozzle; said means including an elongated hollow porous nozzle plug centerbody member having a length thereof fixed within said nozzle and a length thereof extending downstream in the jet emanating from said jet exhaust nozzle; and pressure means connected to said porous centerbody member.
Claim 22
Dependent Claim
35 words
A noise suppression device for a jet as in claim 14 wherein said pressure means is selected from the group consisting of, (a) a pressurized fluid source; (b) a vacuum; and (c) the ambient fluid.
Claim 23
Dependent Claim
46 words
The jet noise suppressor of claim 15 including means for selectively telescopically extending and retracting a length of said nozzle plug centerbody relative to said exhaust nozzle; and means for deflecting a length of said nozzle plug centerbody to direct the jet in a desired path.
Claim 24
Independent Claim
111 words
A device for suppressing noise in a jet flow containing at least one shock wave comprising: a jet exhaust nozzle; an elongated hollow porous member having a first length portion thereof fixed relative to the nozzle and a second length portion disposed within the jet flow extending downstream of said exhaust nozzle; and, pressure means connected to said porous member to provide a pressure differential between the jet flow and porous member, said pressure means serving to affect the static pressure in the jet downstrream of said exhaust nozzle by homogenous mixing of the differential pressures through said porous member to dissipate any shock waves emanating from within said exhaust nozzle.
Claim 25
Independent Claim
111 words
A device for suppressing noise in a jet flow containing at least one shock wave comprising: a jet exhaust nozzle; an elongated hollow porous member having a first length portion thereof fixed relative to the nozzle and a second length portion disposed within the jet flow extending downstream of said exhaust nozzle; and, pressure means connected to said porous member to provide a pressure differential between the jet flow and porous member, said pressure means serving to affect the static pressure in the jet downstrream of said exhaust nozzle by homogenous mixing of the differential pressures through said porous member to dissipate any shock waves emanating from within said exhaust nozzle.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-08-15 | 1987-02-14 | 1987-08-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-08-15 | 1991-02-14 | 1991-08-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-08-15 | 1995-02-14 | 1995-08-16 | $7700.00 | Window Closed / Lapsed |