FR2087076A5 - - Google Patents
Info
- Publication number
- FR2087076A5 FR2087076A5 FR7016227A FR7016227A FR2087076A5 FR 2087076 A5 FR2087076 A5 FR 2087076A5 FR 7016227 A FR7016227 A FR 7016227A FR 7016227 A FR7016227 A FR 7016227A FR 2087076 A5 FR2087076 A5 FR 2087076A5
- Authority
- FR
- France
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/20—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00 having flared outlets, e.g. of fish-tail shape
-
- 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
- F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
-
- 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)
- Exhaust Silencers (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7016227A FR2087076A5 (de) | 1970-05-04 | 1970-05-04 | |
DE19712121485 DE2121485A1 (de) | 1970-05-04 | 1971-04-30 | Schalldämpfende Vorrichtung zur Bildung eines Gasstrahles |
US139402A US3685612A (en) | 1970-05-04 | 1971-05-03 | Gas ejection device with a silencer feature |
CA112026A CA927614A (en) | 1970-05-04 | 1971-05-03 | Gas ejection device with a silencer feature |
GB1275671*[A GB1345786A (en) | 1970-05-04 | 1971-05-03 | Gas ejection device with a silencer feature |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7016227A FR2087076A5 (de) | 1970-05-04 | 1970-05-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2087076A5 true FR2087076A5 (de) | 1971-12-31 |
Family
ID=9055032
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7016227A Expired FR2087076A5 (de) | 1970-05-04 | 1970-05-04 |
Country Status (5)
Country | Link |
---|---|
US (1) | US3685612A (de) |
CA (1) | CA927614A (de) |
DE (1) | DE2121485A1 (de) |
FR (1) | FR2087076A5 (de) |
GB (1) | GB1345786A (de) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2945439A1 (de) * | 1978-11-13 | 1980-05-22 | Gen Electric | Vorrichtung zum unterdruecken von infrarotstrahlung eines gasturbinentriebwerkes |
EP0244336A3 (en) * | 1986-04-30 | 1989-04-26 | United Technologies Corporation | Fluid dynamic pump |
FR2740832A1 (fr) * | 1995-11-02 | 1997-05-09 | Onera (Off Nat Aerospatiale) | Arriere-corps de turboreacteur a double flux |
WO1998059162A1 (en) * | 1997-06-24 | 1998-12-30 | Sikorsky Aircraft Corporation | Multi-stage mixer/ejector for suppressing infrared radiation |
WO1998059163A1 (en) * | 1997-06-24 | 1998-12-30 | Sikorsky Aircraft Corporation | Exhaust nozzle for suppressing infrared radiation |
WO1999005407A1 (en) * | 1997-07-23 | 1999-02-04 | Sikorsky Aircraft Corporation | Turning vane arrangement for ir suppressors |
WO2009138068A1 (de) * | 2008-05-15 | 2009-11-19 | Mtu Aero Engines Gmbh | Mischdüsenaufbau |
EP2226486A1 (de) * | 2009-03-03 | 2010-09-08 | Rolls-Royce Deutschland Ltd & Co KG | Verfahren zur Herstellung eines Ejektor-Düsen-Rohrs |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4128769A (en) * | 1976-09-27 | 1978-12-05 | The Garrett Corporation | Eductor muffler |
GB2185718B (en) * | 1986-01-23 | 1989-11-01 | Rolls Royce | Exhaust nozzle for a gas turbine engine |
US5699965A (en) * | 1989-06-30 | 1997-12-23 | Sikorsky Aircraft Corporation | Infrared suppressor for a gas turbine engine |
GB2240364B (en) * | 1990-01-27 | 1994-09-28 | S & C Thermofluids Ltd | Combustion engines improvements |
GB2249140B (en) * | 1990-08-30 | 1994-12-07 | S & C Thermofluids Ltd | Aircraft engine noise suppression |
US5717172A (en) * | 1996-10-18 | 1998-02-10 | Northrop Grumman Corporation | Sound suppressor exhaust structure |
US6122907A (en) * | 1998-05-11 | 2000-09-26 | Sikorsky Aircraft Corporation | IR suppressor |
US6354538B1 (en) * | 1999-10-25 | 2002-03-12 | Rohr, Inc. | Passive control of hot air injection for swirling rotational type anti-icing system |
US7836682B2 (en) * | 2006-02-13 | 2010-11-23 | General Electric Company | Methods and apparatus for operating a pulse detonation engine |
US7882696B2 (en) * | 2007-06-28 | 2011-02-08 | Honeywell International Inc. | Integrated support and mixer for turbo machinery |
US20130327417A1 (en) * | 2012-06-07 | 2013-12-12 | Jeffrey L. Gardner | Self aligning venturi pipe assembly |
US10150438B2 (en) * | 2017-05-03 | 2018-12-11 | Nissan North America, Inc. | Rear exhaust finisher assembly |
US20230112668A1 (en) * | 2021-10-11 | 2023-04-13 | Boom Technology, Inc. | Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methods |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1357079A (en) * | 1919-06-19 | 1920-10-26 | Harry M Patch | Muffler |
DE441932C (de) * | 1925-09-13 | 1927-03-16 | Hans Erich Koch | Vakuum-Auspufftopf und Schalldaempfer fuer Brennkraftmaschinen |
FR657569A (fr) * | 1927-11-28 | 1929-05-24 | Perfectionnements aux pots d'échappement | |
FR725510A (fr) * | 1931-10-31 | 1932-05-13 | Silencieux particulièrement destiné aux moteurs d'aviation et formant à la fois radiateur et pare-flammes | |
FR859758A (fr) * | 1939-05-27 | 1940-12-28 | Perfectionnements aux pare-flammes | |
FR865279A (fr) * | 1940-04-29 | 1941-05-17 | Perfectionnement aux pare-flammes silencieux | |
US2396208A (en) * | 1943-03-08 | 1946-03-05 | Anemostat Corp | Method of and means for treating gases |
FR1588852A (de) * | 1968-07-31 | 1970-03-16 |
-
1970
- 1970-05-04 FR FR7016227A patent/FR2087076A5/fr not_active Expired
-
1971
- 1971-04-30 DE DE19712121485 patent/DE2121485A1/de active Pending
- 1971-05-03 CA CA112026A patent/CA927614A/en not_active Expired
- 1971-05-03 GB GB1275671*[A patent/GB1345786A/en not_active Expired
- 1971-05-03 US US139402A patent/US3685612A/en not_active Expired - Lifetime
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2945439A1 (de) * | 1978-11-13 | 1980-05-22 | Gen Electric | Vorrichtung zum unterdruecken von infrarotstrahlung eines gasturbinentriebwerkes |
EP0244336A3 (en) * | 1986-04-30 | 1989-04-26 | United Technologies Corporation | Fluid dynamic pump |
FR2740832A1 (fr) * | 1995-11-02 | 1997-05-09 | Onera (Off Nat Aerospatiale) | Arriere-corps de turboreacteur a double flux |
WO1998059162A1 (en) * | 1997-06-24 | 1998-12-30 | Sikorsky Aircraft Corporation | Multi-stage mixer/ejector for suppressing infrared radiation |
WO1998059163A1 (en) * | 1997-06-24 | 1998-12-30 | Sikorsky Aircraft Corporation | Exhaust nozzle for suppressing infrared radiation |
US6016651A (en) * | 1997-06-24 | 2000-01-25 | Sikorsky Aircraft Corporation | Multi-stage mixer/ejector for suppressing infrared radiation |
WO1999005407A1 (en) * | 1997-07-23 | 1999-02-04 | Sikorsky Aircraft Corporation | Turning vane arrangement for ir suppressors |
US6055804A (en) * | 1997-07-23 | 2000-05-02 | Sikorsky Aircraft Corporation | Turning vane arrangement for IR suppressors |
WO2009138068A1 (de) * | 2008-05-15 | 2009-11-19 | Mtu Aero Engines Gmbh | Mischdüsenaufbau |
EP2226486A1 (de) * | 2009-03-03 | 2010-09-08 | Rolls-Royce Deutschland Ltd & Co KG | Verfahren zur Herstellung eines Ejektor-Düsen-Rohrs |
US8782896B2 (en) | 2009-03-03 | 2014-07-22 | Rolls-Royce Deutschland Ltd & Co Kg | Method for the manufacture of an ejector nozzle tube |
Also Published As
Publication number | Publication date |
---|---|
GB1345786A (en) | 1974-02-06 |
DE2121485A1 (de) | 1971-11-25 |
US3685612A (en) | 1972-08-22 |
CA927614A (en) | 1973-06-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |