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DAVILA MINGUEZ
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DAVILA MINGUEZ
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Application filed by DAVILA MINGUEZfiledCriticalDAVILA MINGUEZ
Priority to ES427570ApriorityCriticalpatent/ES427570A1/en
Publication of ES427570A1publicationCriticalpatent/ES427570A1/en
Hydrostatic retropultruder group or fluid accelerator characterized by comprising motor pumps that determine the suction of the water and are driven by the turbine step of the motor group, said water being sent with a first acceleration to the intake nozzle in which a cause of its inclination in relation to the normal plane a second acceleration takes place, happening next to the fixed camera of the accelerator, that has a wear in the form of hollow tubes by which the water circulates and where a movement of rotation takes place, caused by the turbine of the second group that prints to the water a new acceleration or limit speed with which it is thrown to the exhaust nozzle so that its impact with the water produces an impulse in the opposite direction to the direction of the ejected jet. (Machine-translation by Google Translate, not legally binding)
ES427570A1974-06-221974-06-22Hydrostatic retropropulsum group or fluid acelerator. (Machine-translation by Google Translate, not legally binding)
ExpiredES427570A1
(en)
Visualization of the flow in a supersonic axial compressor(Flow visualization in supersonic axial compressor by short exposure schlieren photography of shock wave patterns in rotating annular cascade of compressor blades)
Low-speed jet noise from a 1. 83-meter/6-ft/ fan for turbofan engines(Fan induced low speed jet noise from turbofan engines, discussing results of far field sound measurements for simulated nacelle configurations with and without acoustic liners)
DEVICE FOR SETTING THE ANGLE BETWEEN ROTATING PARTS, DRIVING PARTS AND DRIVEN PARTS IN THE DRIVING MECHANISM OF THE FUEL INJECTION PUMP OF AN ICE ENGINE.
Experimental research of the effect of the angle of rotation of stator blades on the operation of a small size turbine stage(Experimental determination of effect of angle of rotation of stator blades on operation of small size turbine stage)