ES226416A1 - Improvements in rotors for compressors and axil circulation turbines (Machine-translation by Google Translate, not legally binding)
- Google Patents
Improvements in rotors for compressors and axil circulation turbines (Machine-translation by Google Translate, not legally binding)
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.)
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.)
BRITOL AEROPLANE Co Ltd
Original Assignee
BRITOL AEROPLANE Co Ltd
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 BRITOL AEROPLANE Co LtdfiledCriticalBRITOL AEROPLANE Co Ltd
Priority to ES0226416ApriorityCriticalpatent/ES226416A1/en
Publication of ES226416A1publicationCriticalpatent/ES226416A1/en
Structures Of Non-Positive Displacement Pumps
(AREA)
Abstract
Improvements in rotors for axial circulation compressors and turbines, characterized by a rotor of the kind described, in which the pin is connected, at least, to a paddle-carrying disc, at one end of the drum assembly, and is also coupled to a shank-like part that extends axially into the interior of the drum assembly and which, in turn, at its end opposite the pin is connected to another paddle-carrying disc, at a radial distance from the rotor axis, which, at least, it is not appreciably greater than the radial distance to which the spike-like part is connected to the spike. (Machine-translation by Google Translate, not legally binding)
ES0226416A1956-01-311956-01-31Improvements in rotors for compressors and axil circulation turbines (Machine-translation by Google Translate, not legally binding)
ExpiredES226416A1
(en)
Centrifugal rotary electro-compressor homopolar for insufflation of air under pressure to one or more pneumatic horns (Machine-translation by Google Translate, not legally binding)