GB1378943A - Jet discharge nozzle device - Google Patents
Jet discharge nozzle deviceInfo
- Publication number
- GB1378943A GB1378943A GB673872A GB673872A GB1378943A GB 1378943 A GB1378943 A GB 1378943A GB 673872 A GB673872 A GB 673872A GB 673872 A GB673872 A GB 673872A GB 1378943 A GB1378943 A GB 1378943A
- Authority
- GB
- United Kingdom
- Prior art keywords
- orifices
- jet
- flow
- mach
- trailing edge
- 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
Abstract
1378943 Jet propulsion nozzles TEXTRON Inc 14 Feb 1972 [14 June 1971] 6738/72 Heading F1J The invention relates to a jet propulsion nozzle which is adapted to be silenced in operation. The nozzle comprises an externally aerofoil-shaped plenum chamber 10 which is formed at its trailing edge 18 with a plurality of discharge orifices 12 through which jet gases from the pressurized fluid conduit 14 discharge in the form of jets 22, the arrangement being such that a flow of ambient air is induced to flow in the form of a sheath 20 around each jet stream whereby the noise of the jet is attenuated. In a second embodiment two parallel rows of orifices are provided adjacent the trailing edge, the orifices being in staggered relation and being inclined at a small angle whereby the jet streams diverge. In a third embodiment three rows of orifices are provided. The fluid-pressure may be up to 10 p.s.i. and the diameter of the Orifices 0À040 inch; the rate of flow through the orifices must be greater than Mach 0À5 but not greater than Mach 1.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15269671A | 1971-06-14 | 1971-06-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1378943A true GB1378943A (en) | 1975-01-02 |
Family
ID=22544018
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB673872A Expired GB1378943A (en) | 1971-06-14 | 1972-02-14 | Jet discharge nozzle device |
Country Status (4)
Country | Link |
---|---|
US (1) | US3695388A (en) |
CA (1) | CA953755A (en) |
FR (1) | FR2141913B1 (en) |
GB (1) | GB1378943A (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4090583A (en) * | 1976-02-02 | 1978-05-23 | Leonard James L | Streamlined monolithic internal combustion engine muffler |
US5156353A (en) * | 1987-04-13 | 1992-10-20 | General Electric Company | Aircraft pylon |
US4966338A (en) * | 1987-08-05 | 1990-10-30 | General Electric Company | Aircraft pylon |
US5929396A (en) * | 1997-07-29 | 1999-07-27 | Awad; Elias A. | Noise reducing diffuser |
US7703573B2 (en) * | 2005-08-05 | 2010-04-27 | Paccar Inc | Ported aerodynamic exhaust tailpipe |
US20090014235A1 (en) * | 2007-07-13 | 2009-01-15 | Paccar Inc | Flow diffuser for exhaust pipe |
US7971432B2 (en) * | 2007-07-13 | 2011-07-05 | Paccar Inc | Flow diffuser for exhaust pipe |
JP4860773B1 (en) * | 2011-02-18 | 2012-01-25 | サンヨー食品株式会社 | Instant noodle manufacturing method |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB514913A (en) * | 1937-05-24 | 1939-11-21 | Bronzavia Sa | Improvements in or relating to the exhaust pipes of internal combustion engines |
FR859272A (en) * | 1939-04-26 | 1940-12-14 | Apyr | Improvements to manifolds pipes and exhaust pipes for air-cooled or liquid-cooled aircraft engines |
US2845775A (en) * | 1956-06-01 | 1958-08-05 | United Aircraft Corp | Noise suppressors for jet engines |
-
1971
- 1971-06-14 US US152696A patent/US3695388A/en not_active Expired - Lifetime
- 1971-12-17 CA CA130,421A patent/CA953755A/en not_active Expired
-
1972
- 1972-02-14 GB GB673872A patent/GB1378943A/en not_active Expired
- 1972-06-14 FR FR7221394A patent/FR2141913B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3695388A (en) | 1972-10-03 |
CA953755A (en) | 1974-08-27 |
FR2141913A1 (en) | 1973-01-26 |
FR2141913B1 (en) | 1977-12-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |