FR1401425A - Dispositif de tuyère d'éjection pour avions à réaction - Google Patents
Dispositif de tuyère d'éjection pour avions à réactionInfo
- Publication number
- FR1401425A FR1401425A FR972170A FR972170A FR1401425A FR 1401425 A FR1401425 A FR 1401425A FR 972170 A FR972170 A FR 972170A FR 972170 A FR972170 A FR 972170A FR 1401425 A FR1401425 A FR 1401425A
- Authority
- FR
- France
- Prior art keywords
- jet
- nozzle device
- jet nozzle
- jet jet
- nozzle
- 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
- F02K1/36—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
- F02K1/42—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet the means being movable into an inoperative position
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Exhaust Silencers (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR972170A FR1401425A (fr) | 1964-04-24 | 1964-04-24 | Dispositif de tuyère d'éjection pour avions à réaction |
GB11346/65A GB1057265A (en) | 1964-04-24 | 1965-03-17 | Discharge nozzle apparatus for jet aircraft |
US443974A US3333772A (en) | 1964-04-24 | 1965-03-30 | Discharge nozzle apparatus for jet aircraft |
DE19651476597 DE1476597B1 (de) | 1964-04-24 | 1965-04-23 | Austrittsduesenvorrichtung fuer Luftfahrzeuge mit Strahlantrieb |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR972170A FR1401425A (fr) | 1964-04-24 | 1964-04-24 | Dispositif de tuyère d'éjection pour avions à réaction |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1401425A true FR1401425A (fr) | 1965-06-04 |
Family
ID=8828586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR972170A Expired FR1401425A (fr) | 1964-04-24 | 1964-04-24 | Dispositif de tuyère d'éjection pour avions à réaction |
Country Status (4)
Country | Link |
---|---|
US (1) | US3333772A (fr) |
DE (1) | DE1476597B1 (fr) |
FR (1) | FR1401425A (fr) |
GB (1) | GB1057265A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2126922A1 (fr) * | 1971-01-20 | 1972-10-13 | Snecma |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3392529A (en) * | 1965-07-23 | 1968-07-16 | Rolls Royce | Aircraft provided with a gas turbine vertical lift engine |
FR1547756A (fr) * | 1967-10-19 | 1968-11-29 | Snecma | Silencieux pour réacteurs aéronautiques |
FR1588852A (fr) * | 1968-07-31 | 1970-03-16 | ||
US3566989A (en) * | 1969-12-01 | 1971-03-02 | Rohr Corp | Sound suppression nozzle structure for fan jet aircraft engine |
US3667680A (en) * | 1970-04-24 | 1972-06-06 | Boeing Co | Jet engine exhaust nozzle system |
US3685293A (en) * | 1970-05-13 | 1972-08-22 | Herbert C Shipman | Exhaust control for engines |
US3726091A (en) * | 1971-02-16 | 1973-04-10 | Rohr Corp | Sound suppressing apparatus |
GB1473543A (en) * | 1974-09-07 | 1977-05-11 | Rolls Royce | Gas turbine powerplants |
US3990530A (en) * | 1975-05-19 | 1976-11-09 | United Technologies Corporation | Noise suppressor for turbine type power plant |
US4291782A (en) * | 1979-10-30 | 1981-09-29 | The Boeing Company | Simplified method and apparatus for hot-shield jet noise suppression |
EP0102953A4 (fr) * | 1982-03-17 | 1984-08-10 | Boeing Co | Attenuateur de bruit ventile interieurement avec diffuseur a large tampon. |
US5154052A (en) * | 1990-05-07 | 1992-10-13 | General Electric Company | Exhaust assembly for a high speed civil transport aircraft engine |
US5761899A (en) * | 1995-05-11 | 1998-06-09 | The Boeing Company | Supersonic engine apparatus and method with ejector/suppressor |
US5655360A (en) * | 1995-05-31 | 1997-08-12 | General Electric Company | Thrust reverser with variable nozzle |
US5761900A (en) * | 1995-10-11 | 1998-06-09 | Stage Iii Technologies, L.C. | Two-stage mixer ejector suppressor |
US5884472A (en) * | 1995-10-11 | 1999-03-23 | Stage Iii Technologies, L.C. | Alternating lobed mixer/ejector concept suppressor |
US5779150A (en) * | 1996-10-01 | 1998-07-14 | The Boeing Company | Aircraft engine ejector nozzle |
US5941065A (en) * | 1996-11-04 | 1999-08-24 | The Boeing Company | Stowable mixer ejection nozzle |
US5884843A (en) * | 1996-11-04 | 1999-03-23 | The Boeing Company | Engine noise suppression ejector nozzle |
US5908159A (en) * | 1997-02-24 | 1999-06-01 | The Boeing Company | Aircraft chute ejector nozzle |
FR2890378B1 (fr) * | 2005-09-08 | 2009-01-16 | Airbus France Sas | Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot. |
FR2929998B1 (fr) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | Nacelle de turboreacteur a double flux |
FR3000994A1 (fr) * | 2013-01-16 | 2014-07-18 | Aircelle Sa | Tuyere de nacelle a dispositifs de regulation de pression |
US9863366B2 (en) * | 2013-03-13 | 2018-01-09 | Rolls-Royce North American Technologies Inc. | Exhaust nozzle apparatus and method for multi stream aircraft engine |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB834907A (en) * | 1956-10-23 | 1960-05-11 | Rolls Royce | Improvements in or relating to jet propulsion nozzles |
US3055174A (en) * | 1957-01-14 | 1962-09-25 | Boeing Co | Retractable noise suppressor for jet engines |
FR1164936A (fr) * | 1957-01-21 | 1958-10-15 | Bertin Et Cie Soc | Silencieux pour conduits d'échappement et notamment pour tuyères de propulseurs àréaction |
US3032981A (en) * | 1957-02-11 | 1962-05-08 | Boeing Co | Noise suppressor and thrust reverser for jet engine nozzles |
DE1094529B (de) * | 1957-03-01 | 1960-12-08 | Rolls Royce | Strahltriebduese mit zwei einstellbaren Stellungen |
DE1062988B (de) * | 1957-03-12 | 1959-08-06 | Rolls Royce | Strahltriebduese |
US2944624A (en) * | 1957-08-07 | 1960-07-12 | Rolls Royce | Jet noise suppressor nozzle |
GB895922A (en) * | 1958-03-13 | 1962-05-09 | Rolls Royce | Improvements in or relating to aircraft gas-turbine jet propulsion engines |
US3050937A (en) * | 1958-06-09 | 1962-08-28 | Boeing Co | Reversible thrust jet engines and controls therefor |
DE1100385B (de) * | 1958-12-10 | 1961-02-23 | Entwicklungsbau Pirna Veb | Vorrichtung zur Laermbekaempfung des Abgasstrahles eines Strahltriebwerkes durch Zumischen von Frischluft und zur AEnderung der Ausstroemrichtung des Abgasstrahles mittels stellbarer Umlenkplatten |
US3027714A (en) * | 1959-06-11 | 1962-04-03 | Canadair Ltd | Combined thrust reversing and noise suppressing device for turbo-jet engines |
US2987883A (en) * | 1959-06-22 | 1961-06-13 | Boeing Co | Jet engine noise suppression nozzle with aerodynamic supplemental fluting |
-
1964
- 1964-04-24 FR FR972170A patent/FR1401425A/fr not_active Expired
-
1965
- 1965-03-17 GB GB11346/65A patent/GB1057265A/en not_active Expired
- 1965-03-30 US US443974A patent/US3333772A/en not_active Expired - Lifetime
- 1965-04-23 DE DE19651476597 patent/DE1476597B1/de not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2126922A1 (fr) * | 1971-01-20 | 1972-10-13 | Snecma |
Also Published As
Publication number | Publication date |
---|---|
GB1057265A (en) | 1967-02-01 |
DE1476597B1 (de) | 1970-10-15 |
US3333772A (en) | 1967-08-01 |
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