ES420875A1 - Improvements in the construction of gas turbines. (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements in the construction of gas turbines. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES420875A1
ES420875A1 ES420875A ES420875A ES420875A1 ES 420875 A1 ES420875 A1 ES 420875A1 ES 420875 A ES420875 A ES 420875A ES 420875 A ES420875 A ES 420875A ES 420875 A1 ES420875 A1 ES 420875A1
Authority
ES
Spain
Prior art keywords
sections
impeller
translation
construction
combustión
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
ES420875A
Other languages
Spanish (es)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SOLER GIRALT SIMO PRATS
Original Assignee
SOLER GIRALT SIMO PRATS
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 SOLER GIRALT SIMO PRATS filed Critical SOLER GIRALT SIMO PRATS
Priority to ES420875A priority Critical patent/ES420875A1/en
Publication of ES420875A1 publication Critical patent/ES420875A1/en
Expired legal-status Critical Current

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Improvements in the construction of gas turbines, of the kind comprising a rotor with one or several sections of compressor impeller and one or more sections of impeller turbine, between which are interspersed combustión chambers, essentially characterized by the fact of having in a housing, one or more stator sections coaxial and in axial series, and one or more rotor sections alternated between the above, all these sections having an inner crown of guide vanes and impeller forming an axial passage of combustión gases, and an outer crown of impeller blades and conductors forming an axial passage of intake air, the ends of the same side of each of the two axial passages, connected respectively with the exhaust gas outlet and with the air inlet, respectively. Of admission, while the ends of the other side are respectively connected to the gas outlet and to the air inlet of one or more chambers. For combustión. (Machine-translation by Google Translate, not legally binding)
ES420875A 1973-11-20 1973-11-20 Improvements in the construction of gas turbines. (Machine-translation by Google Translate, not legally binding) Expired ES420875A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES420875A ES420875A1 (en) 1973-11-20 1973-11-20 Improvements in the construction of gas turbines. (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES420875A ES420875A1 (en) 1973-11-20 1973-11-20 Improvements in the construction of gas turbines. (Machine-translation by Google Translate, not legally binding)

Publications (1)

Publication Number Publication Date
ES420875A1 true ES420875A1 (en) 1976-08-01

Family

ID=8465446

Family Applications (1)

Application Number Title Priority Date Filing Date
ES420875A Expired ES420875A1 (en) 1973-11-20 1973-11-20 Improvements in the construction of gas turbines. (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES420875A1 (en)

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