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ALDECOA LECANDA CLAUDIO
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ALDECOA LECANDA CLAUDIO
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Priority to ES1971174228UpriorityCriticalpatent/ES174228Y/es
Publication of ES174228UpublicationCriticalpatent/ES174228U/es
Application grantedgrantedCritical
Publication of ES174228YpublicationCriticalpatent/ES174228Y/es
Structures Of Non-Positive Displacement Pumps
(AREA)
Ropes Or Cables
(AREA)
Abstract
Mecanismo de seguridad y apertura de paracaídas pra bombas de aviación de vuelo rasante esencialmente caracterizado porque la pieza de amarre posterior del paracaídas, lleva en su parte anterior un eje hueco interiormente y ciego, en cuyo interior discurre la pieza de anclaje introducida en la pieza de amarre de la bomba, cuya pieza de anclaje está obligada en todo momento por un muelle, y fijada a su vez a la pieza de amarre por una varilla de seguro afianzada por un cable, al avión.
ES1971174228U1971-11-151971-11-15Mecanismo de seguridad y apertura de paracaidas para bombas de aviacion de vuelo rasante.
ExpiredES174228Y
(es)
The impact of flight operating techniques upon engine maintenance costs(Flight operating techniques influence upon engine maintenance costs and new engine design, specifically Pratt and Whitney JT 3 C-12 on Boeing 720 aircraft)
Operating techniques and maintenance practices for the Lockheed SST(Operation and maintenance of Lockheed L-2000 double delta SST aircraft with high thrust engine and large delta wings, designed to meet civil aviation requirements)
An analysis of longitudinal control during landing approach(Aircraft longitudinal control during landing approach, investigating back side operation characteristics by closed loop system analysis regarding pilot and aircraft as elements)
Development of supersonic aircraft components of flight safety(Flight safety standards and air traffic control problems of supersonic aircraft passenger service)
Method of compensating the airplane's turning moment in landing with a brake parachute in a strong side wind(Brake parachute for compensating turning moment of aircraft landing in strong side wind)
Aerodynamic design philosophy of the Boeing 737(Aerodynamic design of Boeing 737 covering data of analytical studies, wind tunnel and flight tests, aerodynamic parameters and drag, flap system size, efficiency, wing geometry and handling qualities)
The aerodynamic merging of wings, fuselage and cockpit(Open jet wind tunnel testing of Meteor sailplane, examining aerodynamic merging of wings, fuselage and cockpit)