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BG97904U - GAS TURBINE ENGINE - Google Patents

GAS TURBINE ENGINE

Info

Publication number
BG97904U
BG97904U BG097904U BG9790493U BG97904U BG 97904 U BG97904 U BG 97904U BG 097904 U BG097904 U BG 097904U BG 9790493 U BG9790493 U BG 9790493U BG 97904 U BG97904 U BG 97904U
Authority
BG
Bulgaria
Prior art keywords
gas turbine
turbine engine
attached
vanes
pipeline
Prior art date
Application number
BG097904U
Other languages
Bulgarian (bg)
Other versions
BG17Y1 (en
Inventor
Йордан Арабов
Original Assignee
Йордан Арабов
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 Йордан Арабов filed Critical Йордан Арабов
Priority to BG97904U priority Critical patent/BG17Y1/en
Publication of BG97904U publication Critical patent/BG97904U/en
Publication of BG17Y1 publication Critical patent/BG17Y1/en

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  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)

Abstract

Газотурбинният двигател е приложим в моторните превозни средства и в автомобилната промишленост. Той е с опростена конструкция и повишена надеждност. С използването му се намалява специфичният разход на енергия и се повишава коефициентът на полезно действие. Газотурбинният двигател включва въздушен компресор (2), свързан директно с газова турбина (6), към която радиално са закрепени лопатки (24). Газовата турбина (6) е монтирана след горивната камера (4) и пред ауспухното устройство (7). Отворите на лопатките (24) са свързани с радиални канали (22), входно пространство (21) и с изходно пространство (25). Към последното е монтиран тръбопровод (17), закрепен към радиатор (18), който е свързан чрез тръбопровод (15) и центробежна помпа (20) с входното пространство (21) на газовата турбина (6). 1 претенция, 2 фигуриThe gas turbine engine is applicable in motor vehicles and in the automotive industry. It has a simplified design and increased reliability. With its use, the specific energy consumption is reduced and the coefficient of useful action is increased. The gas turbine engine includes an air compressor (2) connected directly to a gas turbine (6) to which vanes (24) are radially attached. The gas turbine (6) is mounted after the combustion chamber (4) and in front of the exhaust device (7). The openings of the vanes (24) are connected to radial channels (22), an inlet space (21) and an outlet space (25). A pipeline (17) is attached to the latter, attached to a radiator (18), which is connected by a pipeline (15) and a centrifugal pump (20) to the inlet space (21) of the gas turbine (6). 1 claim, 2 figures

BG97904U 1993-06-24 1993-06-24 GASTERWORK ENGINE BG17Y1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
BG97904U BG17Y1 (en) 1993-06-24 1993-06-24 GASTERWORK ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BG97904U BG17Y1 (en) 1993-06-24 1993-06-24 GASTERWORK ENGINE

Publications (2)

Publication Number Publication Date
BG97904U true BG97904U (en) 1995-01-31
BG17Y1 BG17Y1 (en) 1996-02-29

Family

ID=3925279

Family Applications (1)

Application Number Title Priority Date Filing Date
BG97904U BG17Y1 (en) 1993-06-24 1993-06-24 GASTERWORK ENGINE

Country Status (1)

Country Link
BG (1) BG17Y1 (en)

Also Published As

Publication number Publication date
BG17Y1 (en) 1996-02-29

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