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Inconex Handelgesellschaft M B
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Inconex Handelgesellschaft M B
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Priority to ES0200943ApriorityCriticalpatent/ES200943A1/en
Publication of ES200943A1publicationCriticalpatent/ES200943A1/en
A gas turbine engine, especially for jet turbomotors, characterized in that the input side of the engine is formed by a compressor with at least one diagonal passage and one or several axial passages, and the side of outlet, by a distributor and one or more turbine passes, an annular combustión chamber with injector bodies being arranged between the inlet and outlet passages. (Machine-translation by Google Translate, not legally binding)
ES0200943A1951-12-141951-12-14A gas turbine engine, especially for jet turbomotors (Machine-translation by Google Translate, not legally binding)
ExpiredES200943A1
(en)