ITMI910790A0 - Camera di combustione con ugello per un motore ipersonico - Google Patents
Camera di combustione con ugello per un motore ipersonicoInfo
- Publication number
- ITMI910790A0 ITMI910790A0 IT91MI790A ITMI910790A ITMI910790A0 IT MI910790 A0 ITMI910790 A0 IT MI910790A0 IT 91MI790 A IT91MI790 A IT 91MI790A IT MI910790 A ITMI910790 A IT MI910790A IT MI910790 A0 ITMI910790 A0 IT MI910790A0
- Authority
- IT
- Italy
- Prior art keywords
- nozzle
- combustion chamber
- hypersonic engine
- hypersonic
- engine
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
-
- 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
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4010471A DE4010471A1 (de) | 1990-03-31 | 1990-03-31 | Brennkammer mit duese fuer einen hyperschallantrieb |
Publications (3)
Publication Number | Publication Date |
---|---|
ITMI910790A0 true ITMI910790A0 (it) | 1991-03-22 |
ITMI910790A1 ITMI910790A1 (it) | 1992-09-22 |
IT1245582B IT1245582B (it) | 1994-09-29 |
Family
ID=6403526
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ITMI910790A IT1245582B (it) | 1990-03-31 | 1991-03-22 | Camera di combustione con ugello per un motore ipersonico |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE4010471A1 (it) |
FR (1) | FR2660416A1 (it) |
GB (1) | GB2243877A (it) |
IT (1) | IT1245582B (it) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4222947C2 (de) * | 1992-07-11 | 1995-02-02 | Deutsche Aerospace | Strahltriebwerk |
DE4237860A1 (de) * | 1992-11-10 | 1994-05-11 | Schlafhorst & Co W | Fadenführungstrommel |
DE10208161A1 (de) * | 2002-02-26 | 2003-09-18 | Alban Geissler | Düsenantriebssystem |
US10094336B2 (en) | 2014-04-17 | 2018-10-09 | Raytheon Company | Articulated diffuser and door for submerged ram air turbine power and cooling control |
CN107120210B (zh) * | 2017-06-25 | 2023-05-23 | 北京航天三发高科技有限公司 | 一种超音速喷管 |
CN115183269B (zh) * | 2022-07-21 | 2023-06-20 | 中国航发沈阳发动机研究所 | 一种采用陶瓷基叶片和整流支板整流的加力燃烧室 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB757457A (en) * | 1953-09-10 | 1956-09-19 | Snecma | Rocket control |
GB805418A (en) * | 1955-10-05 | 1958-12-03 | Power Jets Res & Dev Ltd | Jet propulsion plant |
US3060679A (en) * | 1958-10-24 | 1962-10-30 | Gen Electric | Powerplant |
GB875496A (en) * | 1959-12-07 | 1961-08-23 | Gen Electric | Improvements in or relating to ducted-fan gas turbine jet propulsion engines |
US3192712A (en) * | 1962-12-31 | 1965-07-06 | Gen Electric | Load balancing arrangement for annular variable area jet exhaust nozzle |
DE1892865U (de) * | 1963-01-08 | 1964-05-14 | Bristol Siddeley Engines Ltd | Strahltriebwerk. |
GB1069872A (en) * | 1963-02-19 | 1967-05-24 | Bristol Siddeley Engines Ltd | Engine fuel supply systems |
GB1114181A (en) * | 1964-05-28 | 1968-05-15 | Bristol Siddeley Engines Ltd | Fuel control systems for aircraft |
GB1044243A (en) * | 1965-04-20 | 1966-09-28 | Rolls Royce | Jet propulsion engines |
GB1132236A (en) * | 1965-08-03 | 1968-10-30 | Mini Of Technology | Supersonic fluid flow exhaust nozzles |
FR2182647B1 (it) * | 1972-05-02 | 1975-08-29 | Snecma | |
DE2255306C3 (de) * | 1972-11-11 | 1975-06-12 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Aerodynamische Flammenhalterung für luftatmende Strahltriebwerke |
-
1990
- 1990-03-31 DE DE4010471A patent/DE4010471A1/de active Granted
-
1991
- 1991-03-21 GB GB9106049A patent/GB2243877A/en not_active Withdrawn
- 1991-03-22 IT ITMI910790A patent/IT1245582B/it active IP Right Grant
- 1991-03-26 FR FR9103610A patent/FR2660416A1/fr active Pending
Also Published As
Publication number | Publication date |
---|---|
GB9106049D0 (en) | 1991-05-08 |
ITMI910790A1 (it) | 1992-09-22 |
DE4010471A1 (de) | 1991-10-02 |
IT1245582B (it) | 1994-09-29 |
FR2660416A1 (fr) | 1991-10-04 |
GB2243877A (en) | 1991-11-13 |
DE4010471C2 (it) | 1992-11-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
0001 | Granted | ||
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19970326 |