RU2003127159A - MULTI-ROTOR MULTI-STAGE EXTERNAL COMBUSTION ENGINE - Google Patents

MULTI-ROTOR MULTI-STAGE EXTERNAL COMBUSTION ENGINE Download PDF

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Publication number
RU2003127159A
RU2003127159A RU2003127159/06A RU2003127159A RU2003127159A RU 2003127159 A RU2003127159 A RU 2003127159A RU 2003127159/06 A RU2003127159/06 A RU 2003127159/06A RU 2003127159 A RU2003127159 A RU 2003127159A RU 2003127159 A RU2003127159 A RU 2003127159A
Authority
RU
Russia
Prior art keywords
rotor
combustion engine
external combustion
stage external
stage
Prior art date
Application number
RU2003127159/06A
Other languages
Russian (ru)
Inventor
Иван Федорович Суслов (RU) Суслов Иван Федорович (RU)
Иван Федорович Суслов
Original Assignee
Иван Федорович Суслов (RU) Суслов Иван Федорович (RU)
Иван Федорович Суслов
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 Иван Федорович Суслов (RU) Суслов Иван Федорович (RU), Иван Федорович Суслов filed Critical Иван Федорович Суслов (RU) Суслов Иван Федорович (RU)
Priority to RU2003127159/06A priority Critical patent/RU2003127159A/en
Publication of RU2003127159A publication Critical patent/RU2003127159A/en

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  • Turbine Rotor Nozzle Sealing (AREA)

Claims (1)

Многороторный многоступенчатый двигатель внешнего сгорания по патенту №1722239, отличающийся тем, что двигатель имеет один корпус, в котором установлено не меньше трех роторов, составляющих, например, две ступени двигателя высокого давления с промежуточными газопроводными каналами, на валах роторов имеется турбина, на центральном роторе расположен вал отбора мощности.The multi-rotor multi-stage external combustion engine according to patent No. 1722239, characterized in that the engine has one housing in which at least three rotors are installed, comprising, for example, two stages of a high-pressure engine with intermediate gas ducts, there is a turbine on the rotor shafts, on the central rotor the power take-off shaft is located.
RU2003127159/06A 2003-09-08 2003-09-08 MULTI-ROTOR MULTI-STAGE EXTERNAL COMBUSTION ENGINE RU2003127159A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2003127159/06A RU2003127159A (en) 2003-09-08 2003-09-08 MULTI-ROTOR MULTI-STAGE EXTERNAL COMBUSTION ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2003127159/06A RU2003127159A (en) 2003-09-08 2003-09-08 MULTI-ROTOR MULTI-STAGE EXTERNAL COMBUSTION ENGINE

Publications (1)

Publication Number Publication Date
RU2003127159A true RU2003127159A (en) 2005-03-20

Family

ID=35453896

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2003127159/06A RU2003127159A (en) 2003-09-08 2003-09-08 MULTI-ROTOR MULTI-STAGE EXTERNAL COMBUSTION ENGINE

Country Status (1)

Country Link
RU (1) RU2003127159A (en)

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20050204