GB831776A - Jet engine noise attenuator - Google Patents
Jet engine noise attenuatorInfo
- Publication number
- GB831776A GB831776A GB9078/58A GB907858A GB831776A GB 831776 A GB831776 A GB 831776A GB 9078/58 A GB9078/58 A GB 9078/58A GB 907858 A GB907858 A GB 907858A GB 831776 A GB831776 A GB 831776A
- Authority
- GB
- United Kingdom
- Prior art keywords
- diffuser
- supported
- ribs
- wire mesh
- tail pipe
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/26—Ground or aircraft-carrier-deck installations for reducing engine or jet noise; Protecting airports from jet erosion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Exhaust Silencers (AREA)
Abstract
831,776. Exhaust-silencers. LEMMERMAN Inc., C. W. March 21, 1958 [July 29, 1957], No. 9078/58. Class 7(2) A portable or fixed ground silencer for jet engines comprises a sheet metal casing 10, Fig. 2, with an upturned exit 14, a sound-absorbing lining 18 constructed as in U.S.A. Specification 2,674,336, and a diffuser 23 supported by vanes 22 and having a gas entry 26 for connection to or reception of a jet engine tail pipe and gas exit perforations 32 increasing in size and spacing towards its downstream end and having a total area at least equal to that of the tail pipe. The upstream perforations 32 are small enough to prevent passage therethrough of cooling air drawn in between the members 10 and 23. The diffuser 23 may be wholly conical and of wire mesh and supported at its front and rear only, the lining 18 being optionally omitted or disposed only in the area of the diffuser. Figs. 5 and 6 show a diffuser formed of axially spaced notched rings 239 with flanges 241 interconnected by ribs 243; such a diffuser may be used with a wire mesh diffuser formed as above covering it. In Fig. 8 a diffuser is formed by a perforated cylinder 424 and rings 447 supported by ribs 448. A core 449 and an annular air guide 446 are provided, together with supporting vanes 449<SP>1</SP>, 422<SP>1</SP> and 422.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US831776XA | 1957-07-29 | 1957-07-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB831776A true GB831776A (en) | 1960-03-30 |
Family
ID=22176675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9078/58A Expired GB831776A (en) | 1957-07-29 | 1958-03-21 | Jet engine noise attenuator |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB831776A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174581A (en) * | 1960-09-30 | 1965-03-23 | Bertin & Cie | Removable silencer device for jet engines |
US3195678A (en) * | 1962-02-23 | 1965-07-20 | Industrial Acoustics Co | Aerodynamic coupling for jet noise suppressors |
US3196977A (en) * | 1960-04-27 | 1965-07-27 | Industrial Acoustics Co | Sound attenuation control means including diffuser for high velocity streams |
US3215172A (en) * | 1962-12-24 | 1965-11-02 | Nilsson Robbins & Anderson | Jet engine noise suppressor with shroud for aspiration of air into exhaust stream |
US3286787A (en) * | 1963-08-26 | 1966-11-22 | Garrett Corp | Turbine exhaust silencer |
DE1231957B (en) * | 1964-01-04 | 1967-01-05 | Gruenzweig & Hartmann | Silencer for the gas jet emerging from a mouth at high speed |
DE1248372B (en) * | 1962-02-23 | 1967-08-24 | Industrial Acoustics Co | Exhaust silencer for the ground operation of jet engines |
GB2139696A (en) * | 1983-05-11 | 1984-11-14 | Industry The Secretary Of Stat | Absorptive exhaust gas silencer |
-
1958
- 1958-03-21 GB GB9078/58A patent/GB831776A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3196977A (en) * | 1960-04-27 | 1965-07-27 | Industrial Acoustics Co | Sound attenuation control means including diffuser for high velocity streams |
US3174581A (en) * | 1960-09-30 | 1965-03-23 | Bertin & Cie | Removable silencer device for jet engines |
US3195678A (en) * | 1962-02-23 | 1965-07-20 | Industrial Acoustics Co | Aerodynamic coupling for jet noise suppressors |
DE1248372B (en) * | 1962-02-23 | 1967-08-24 | Industrial Acoustics Co | Exhaust silencer for the ground operation of jet engines |
US3215172A (en) * | 1962-12-24 | 1965-11-02 | Nilsson Robbins & Anderson | Jet engine noise suppressor with shroud for aspiration of air into exhaust stream |
US3286787A (en) * | 1963-08-26 | 1966-11-22 | Garrett Corp | Turbine exhaust silencer |
DE1231957B (en) * | 1964-01-04 | 1967-01-05 | Gruenzweig & Hartmann | Silencer for the gas jet emerging from a mouth at high speed |
GB2139696A (en) * | 1983-05-11 | 1984-11-14 | Industry The Secretary Of Stat | Absorptive exhaust gas silencer |
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