GB886201A - Jet noise silencer for an aircraft - Google Patents
Jet noise silencer for an aircraftInfo
- Publication number
- GB886201A GB886201A GB1857959A GB1857959A GB886201A GB 886201 A GB886201 A GB 886201A GB 1857959 A GB1857959 A GB 1857959A GB 1857959 A GB1857959 A GB 1857959A GB 886201 A GB886201 A GB 886201A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- jet
- rows
- nozzles
- noise silencer
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
Abstract
886,201. Jet propelled aircraft. ROLLSROYCE Ltd. May 25, 1960 [June 1, 1959], No. 18579/59. Class 4. [Also in Group XXVI] A silenced jet propulsion installation comprises one or more rows of jet nozzles arranged at the outlet end of a jet pipe. The engine is arranged on the aircraft with the rows of nozzles extending vertically. The aircraft 10, Fig. 5, has two pairs of engines arranged on each side of the rear end of the fuselage. The rows 21, 22, 23 of jet nozzles of each engine are arranged in the vertical plane when the aircraft is in its normal flight attitude.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1857959A GB886201A (en) | 1959-06-01 | 1959-06-01 | Jet noise silencer for an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1857959A GB886201A (en) | 1959-06-01 | 1959-06-01 | Jet noise silencer for an aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB886201A true GB886201A (en) | 1962-01-03 |
Family
ID=10114879
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1857959A Expired GB886201A (en) | 1959-06-01 | 1959-06-01 | Jet noise silencer for an aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB886201A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3212700A (en) * | 1962-01-12 | 1965-10-19 | Bertin & Cie | Ejector devices having slot-like inducing nozzles, especially for sustentation |
US3612212A (en) * | 1969-08-11 | 1971-10-12 | Rohr Corp | Method and apparatus for suppressing the noise of a jet engine |
US3648800A (en) * | 1970-04-27 | 1972-03-14 | Gen Electric | Coanda expansion exhaust nozzle suppressor |
US3968853A (en) * | 1973-08-31 | 1976-07-13 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Notch attenuation device |
-
1959
- 1959-06-01 GB GB1857959A patent/GB886201A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3212700A (en) * | 1962-01-12 | 1965-10-19 | Bertin & Cie | Ejector devices having slot-like inducing nozzles, especially for sustentation |
US3612212A (en) * | 1969-08-11 | 1971-10-12 | Rohr Corp | Method and apparatus for suppressing the noise of a jet engine |
US3648800A (en) * | 1970-04-27 | 1972-03-14 | Gen Electric | Coanda expansion exhaust nozzle suppressor |
US3968853A (en) * | 1973-08-31 | 1976-07-13 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Notch attenuation device |
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