IT1245582B - Camera di combustione con ugello per un motore ipersonico - Google Patents

Camera di combustione con ugello per un motore ipersonico

Info

Publication number
IT1245582B
IT1245582B ITMI910790A ITMI910790A IT1245582B IT 1245582 B IT1245582 B IT 1245582B IT MI910790 A ITMI910790 A IT MI910790A IT MI910790 A ITMI910790 A IT MI910790A IT 1245582 B IT1245582 B IT 1245582B
Authority
IT
Italy
Prior art keywords
combustion chamber
displacement body
nozzle
flow
external wall
Prior art date
Application number
ITMI910790A
Other languages
English (en)
Italian (it)
Inventor
Joachim Kretschmer
Original Assignee
Messerschmitt Boikow Blohm Gmb
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Boikow Blohm Gmb filed Critical Messerschmitt Boikow Blohm Gmb
Publication of ITMI910790A0 publication Critical patent/ITMI910790A0/it
Publication of ITMI910790A1 publication Critical patent/ITMI910790A1/it
Application granted granted Critical
Publication of IT1245582B publication Critical patent/IT1245582B/it

Links

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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Supercharger (AREA)
ITMI910790A 1990-03-31 1991-03-22 Camera di combustione con ugello per un motore ipersonico IT1245582B (it)

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 ITMI910790A0 (it) 1991-03-22
ITMI910790A1 ITMI910790A1 (it) 1992-09-22
IT1245582B true 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 (enrdf_load_stackoverflow)
FR (1) FR2660416A1 (enrdf_load_stackoverflow)
GB (1) GB2243877A (enrdf_load_stackoverflow)
IT (1) IT1245582B (enrdf_load_stackoverflow)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
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
RU2183762C1 (ru) * 2000-12-07 2002-06-20 Государственное унитарное предприятие Машиностроительное конструкторское бюро "Факел" им. акад. П.Д. Грушина Двухрежимный сопловой блок для ракетного двигателя
DE10208161A1 (de) * 2002-02-26 2003-09-18 Alban Geissler Düsenantriebssystem
FR2840030B1 (fr) * 2002-05-21 2005-03-04 Eads Launch Vehicles Moteur a tuyere a noyau central pour lanceur spatial
RU2323362C1 (ru) * 2006-09-14 2008-04-27 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Двигатель для летательного аппарата
RU2391546C1 (ru) * 2008-12-17 2010-06-10 Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ управления вектором тяги жидкостного ракетного двигателя
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)

* Cited by examiner, † Cited by third party
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 (enrdf_load_stackoverflow) * 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

Also Published As

Publication number Publication date
ITMI910790A1 (it) 1992-09-22
FR2660416A1 (fr) 1991-10-04
GB2243877A (en) 1991-11-13
ITMI910790A0 (it) 1991-03-22
GB9106049D0 (en) 1991-05-08
DE4010471C2 (enrdf_load_stackoverflow) 1992-11-19
DE4010471A1 (de) 1991-10-02

Similar Documents

Publication Publication Date Title
IT1245582B (it) Camera di combustione con ugello per un motore ipersonico
IT7821994A0 (it) Camera di combustione ibrida di turbina a gas con iniezione graduale del combustibile pre-miscelato.
RU94031217A (ru) Прямоточный воздушно-реактивный двигатель
IT7828046A0 (it) Camicia per la camera di combustione di un motore a turbina a gas.
ATE129779T1 (de) Schubumkehrvorrichtung mit verbesserter umlenkung der gasstrahlen.
IT1248490B (it) Dispositivo per far turbinare l'aria per un motore a combustione interna.
FR2674317B1 (fr) Chambre de combustion de turbomachine comportant un reglage du debit de comburant.
JPS6414519A (en) Combustion chamber casing for turbo jet engine containing air intake hole
ATE20953T1 (de) Abgassschalldaempfer einer waermekraftmaschine.
JPS5472317A (en) Exhaust bypass apparatus for turbo-charger
IT7821307A0 (it) Iniettore del combustibile per impianti d'iniezione di motori endotermici.
GB1055234A (en) Ultra-high temperature combustion chambers
GB1074562A (en) Silencers for gases
ATE518100T1 (de) Vorrichtung für eine brennkammer einer gasturbine
BE762599A (fr) Dispositif de commande pour les aubes de guidage disposees a l'orifice d'admission des moteurs a turbine a gaz
DE69205244D1 (de) Zusatzbrennkammer für eine indirekt befeuerte Gasturbine.
BE870333A (fr) Tube d'admission d'air refroidi pour chambre de combustion de turbine a gaz
FR1516319A (fr) Dispositif de réglage du débit du carburant d'un moteur à turbine à gaz
SE9902377D0 (sv) Gasflödesregulator
IT1060613B (it) Condotto di ingresso di attenuazione del suono particolarmente per un motore a turbina a gas
SU1754913A1 (ru) Регулируемое сопло
IT1257194B (it) Sistema di aspirazione a geometria variabile per un motore endotermicodi un veicolo.
IT1265714B1 (it) Siringa per uso medico con ago a scomparsa automatica non riutilizzabile.
DK0496094T3 (da) Dyse til tilførsel af sekundærluft
IT8125856A0 (it) Valvola di aspirazione per motore a combustione interna, munita di cavita' con tubo termodispersore emetodo di raffreddamento della valvola stessa.

Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970326