UA93619U - combustion chamber - Google Patents

combustion chamber

Info

Publication number
UA93619U
UA93619U UAU201404451U UAU201404451U UA93619U UA 93619 U UA93619 U UA 93619U UA U201404451 U UAU201404451 U UA U201404451U UA U201404451 U UAU201404451 U UA U201404451U UA 93619 U UA93619 U UA 93619U
Authority
UA
Ukraine
Prior art keywords
rich
mix
fuel
air
combustion chamber
Prior art date
Application number
UAU201404451U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Сергій Іванович Сербін
Наталія Олександрівна Гончарова
Олександр Костянтинович Чередніченко
Original Assignee
Національний Університет Кораблебудування Імені Адмірала Макарова
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 Національний Університет Кораблебудування Імені Адмірала Макарова filed Critical Національний Університет Кораблебудування Імені Адмірала Макарова
Priority to UAU201404451U priority Critical patent/UA93619U/en
Publication of UA93619U publication Critical patent/UA93619U/en

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/34Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Abstract

Combustion chamber which comprises a housing, nozzle with swirler mounted in the casing, and after the swirler flue is installed, this is formed with shells of rich and poor fuel-air mix combustion zones, between those narrowing of the burning zone of rich fuel mix is placed, there are openings for air supply , at that the ratio of the diameter of the narrowing of the shell of the combustion zone of rich air-fuel mix to the diameter of the shell of combustion zone of rich fuel-air mix is 0,4-0,55.
UAU201404451U 2014-04-25 2014-04-25 combustion chamber UA93619U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201404451U UA93619U (en) 2014-04-25 2014-04-25 combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201404451U UA93619U (en) 2014-04-25 2014-04-25 combustion chamber

Publications (1)

Publication Number Publication Date
UA93619U true UA93619U (en) 2014-10-10

Family

ID=56277544

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201404451U UA93619U (en) 2014-04-25 2014-04-25 combustion chamber

Country Status (1)

Country Link
UA (1) UA93619U (en)

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