PL3971406T3 - Sekcja komory spalania ze zintegrowanym deflektorem i sposób wytwarzania sekcji komory spalania - Google Patents

Sekcja komory spalania ze zintegrowanym deflektorem i sposób wytwarzania sekcji komory spalania

Info

Publication number
PL3971406T3
PL3971406T3 PL21191880.0T PL21191880T PL3971406T3 PL 3971406 T3 PL3971406 T3 PL 3971406T3 PL 21191880 T PL21191880 T PL 21191880T PL 3971406 T3 PL3971406 T3 PL 3971406T3
Authority
PL
Poland
Prior art keywords
combustion chamber
chamber section
manufacturing
integrated baffle
baffle
Prior art date
Application number
PL21191880.0T
Other languages
English (en)
Inventor
Chris Udo Maeding
Original Assignee
Arianegroup Gmbh
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 Arianegroup Gmbh filed Critical Arianegroup Gmbh
Publication of PL3971406T3 publication Critical patent/PL3971406T3/pl

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
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • 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
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
PL21191880.0T 2020-09-21 2021-08-18 Sekcja komory spalania ze zintegrowanym deflektorem i sposób wytwarzania sekcji komory spalania PL3971406T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102020124530.0A DE102020124530A1 (de) 2020-09-21 2020-09-21 Brennkammerabschnitt mit integriertem Leitblech und Verfahren zum Herstellen eines Brennkammerabschnitts

Publications (1)

Publication Number Publication Date
PL3971406T3 true PL3971406T3 (pl) 2024-07-08

Family

ID=77398454

Family Applications (1)

Application Number Title Priority Date Filing Date
PL21191880.0T PL3971406T3 (pl) 2020-09-21 2021-08-18 Sekcja komory spalania ze zintegrowanym deflektorem i sposób wytwarzania sekcji komory spalania

Country Status (6)

Country Link
US (1) US11846255B2 (pl)
EP (1) EP3971406B1 (pl)
JP (1) JP7339986B2 (pl)
DE (1) DE102020124530A1 (pl)
ES (1) ES2978955T3 (pl)
PL (1) PL3971406T3 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118836465B (zh) * 2024-08-05 2026-02-06 北京航空航天大学 一种环形燃烧室的冷却系统及其加工方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2558484A (en) * 1947-06-25 1951-06-26 Daniel And Florence Guggenheim Cooling jacket and heat-resistant cap for combustion chambers
US3242668A (en) * 1961-06-05 1966-03-29 Aerojet General Co Means for reducing rocket motor combustion chamber instability
US3200589A (en) * 1961-11-03 1965-08-17 North American Aviation Inc Two stage baffled injector
US3242670A (en) 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
DE1257489B (de) * 1965-05-15 1967-12-28 Boelkow Gmbh Raketentriebwerk fuer fluessige Treibstoffe mit einer Hauptbrennkammer und einer Vorbrennkammer
GB1102138A (en) * 1969-05-26 1968-02-07 Boelkow Gmbh Injection device for jet propulsion units
DE2356572C3 (de) * 1973-11-13 1979-03-29 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Flüssigkeitsgekühlte Raketenbrennkammer mit Schubdüse
DE19901422C2 (de) 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk
CN105841193B (zh) * 2016-05-18 2018-07-20 葛明龙 两种航空航天涡扇发动机
DE102016209650B4 (de) 2016-06-02 2019-03-14 Arianegroup Gmbh Einspritzvorrichtung für ein raketentriebwerk
WO2018045351A1 (en) * 2016-09-01 2018-03-08 Additive Rocket Corporation Additive manufactured combustion engine
DE102017129321B4 (de) 2017-12-08 2024-11-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammervorrichtung, Fahrzeug

Also Published As

Publication number Publication date
JP2022051696A (ja) 2022-04-01
US20220090562A1 (en) 2022-03-24
EP3971406B1 (de) 2024-03-20
ES2978955T3 (es) 2024-09-23
JP7339986B2 (ja) 2023-09-06
DE102020124530A1 (de) 2022-03-24
US11846255B2 (en) 2023-12-19
EP3971406A1 (de) 2022-03-23

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