CH324501A - Gas turbine jet engine - Google Patents
Gas turbine jet engineInfo
- Publication number
- CH324501A CH324501A CH324501DA CH324501A CH 324501 A CH324501 A CH 324501A CH 324501D A CH324501D A CH 324501DA CH 324501 A CH324501 A CH 324501A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- jet engine
- turbine jet
- engine
- gas
- Prior art date
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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/123—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB324501X | 1953-02-16 | ||
GB110254X | 1954-02-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH324501A true CH324501A (en) | 1957-09-30 |
Family
ID=26247958
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH324501D CH324501A (en) | 1953-02-16 | 1954-02-16 | Gas turbine jet engine |
Country Status (4)
Country | Link |
---|---|
BE (1) | BE526525A (en) |
CH (1) | CH324501A (en) |
FR (1) | FR1097287A (en) |
GB (1) | GB750307A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1164754B (en) * | 1952-08-15 | 1964-03-05 | United Aircraft Corp | Thrust nozzle for an aircraft jet engine |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3049875A (en) * | 1952-08-15 | 1962-08-21 | United Aircraft Corp | Variable flap plug type nozzle |
US2930186A (en) * | 1954-11-26 | 1960-03-29 | Ashwood Peter Frederick | Discharge nozzles for propulsive jets |
US2982089A (en) * | 1955-06-24 | 1961-05-02 | Gen Motors Corp | Afterburner nozzle |
US3032974A (en) * | 1956-08-24 | 1962-05-08 | United Aircraft Corp | Exhaust nozzle |
US3004385A (en) * | 1958-06-25 | 1961-10-17 | Gen Motors Corp | Variable convergent-divergent jet nozzle |
US3038304A (en) * | 1959-04-17 | 1962-06-12 | Gen Electric | Variable exhaust nozzle configuration |
GB951130A (en) * | 1961-07-28 | 1964-03-04 | Rolls Royce | Improvements relating to jet engines |
GB1127826A (en) * | 1966-06-17 | 1968-09-18 | Rolls Royce | Gas turbine engine |
FR2732408A1 (en) * | 1983-03-16 | 1996-10-04 | Snecma | Nozzles for gas turbine |
US6318070B1 (en) | 2000-03-03 | 2001-11-20 | United Technologies Corporation | Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
US6543224B1 (en) * | 2002-01-29 | 2003-04-08 | United Technologies Corporation | System and method for controlling shape memory alloy actuators |
US7216831B2 (en) | 2004-11-12 | 2007-05-15 | The Boeing Company | Shape changing structure |
US7340883B2 (en) | 2004-11-12 | 2008-03-11 | The Boeing Company | Morphing structure |
US7546727B2 (en) | 2004-11-12 | 2009-06-16 | The Boeing Company | Reduced noise jet engine |
JP5264742B2 (en) | 2006-10-12 | 2013-08-14 | ユナイテッド テクノロジーズ コーポレイション | Variable area fan nozzle for a gas turbine engine fan nacelle with a sliding actuator |
WO2014200403A1 (en) * | 2013-06-14 | 2014-12-18 | Saab Ab | Variable-geometry exhaust nozzle for a jet engine and a method for varying the nozzle |
FR3051228B1 (en) * | 2016-05-12 | 2020-02-14 | Herakles | RIGIDIFICATION OF THE LINK BETWEEN SHUTTERS IN A VARIABLE SECTION NOZZLE |
CN110159454B (en) * | 2019-06-17 | 2023-11-24 | 西安航空学院 | Adjustable jet pipe of solid flushing engine |
-
0
- BE BE526525D patent/BE526525A/xx unknown
-
1953
- 1953-02-16 GB GB4332/53A patent/GB750307A/en not_active Expired
-
1954
- 1954-02-15 FR FR1097287D patent/FR1097287A/en not_active Expired
- 1954-02-16 CH CH324501D patent/CH324501A/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1164754B (en) * | 1952-08-15 | 1964-03-05 | United Aircraft Corp | Thrust nozzle for an aircraft jet engine |
Also Published As
Publication number | Publication date |
---|---|
GB750307A (en) | 1956-06-13 |
FR1097287A (en) | 1955-07-04 |
BE526525A (en) |
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