Casado Montero
Carlos Casado Montero, Madrid ES
Patent application number | Description | Published |
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20090275276 | Control system for pressurization, ventilation and air conditioning of an aircraft - It consists of two electrically fed pneumatic independent compressors (CAC) ( | 11-05-2009 |
20130193271 | DRAINAGE MAST OF THE COMPARTMENT OF THE AUXILIARY POWER UNIT OF AN AIRCRAFT - A drainage mast ( | 08-01-2013 |
20140373552 | METHOD AND SYSTEM FOR STARTING UP AN AIRCRAFT TURBOMACHINE BY REAL-TIME REGULATION OF AIR FLOW - The start-up system comprises a control loop, which regulates in real time the opening of a valve of an air feed of a start-up turbine based on the current measured speed of rotation of a rotor of the turbomachine and a predetermined speed value, said start-up turbine being capable of turning the rotor of the turbomachine for the purpose of the start-up. | 12-25-2014 |
20140373553 | METHOD AND SYSTEM FOR STARTING UP AN AIRCRAFT TURBOMACHINE - A start-up system including a control system controlling a partial opening of an air intake valve of a start-up turbine during a first phase of the start-up. The start-up turbine is capable of turning a rotor of the turbomachine for the purpose of the start-up, so as to prevent the rotor from encountering critical frequencies of the turbomachine | 12-25-2014 |
Carlos Casado Montero, Getafe ES
Patent application number | Description | Published |
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20130181088 | AIRCRAFT VERSATILE POWER SYSTEM - An aircraft versatile power system ( | 07-18-2013 |
Carlos Casado Montero, Getafe (madrid) ES
Patent application number | Description | Published |
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20150021438 | DRAINAGE MAST OF THE COMPARTMENT OF AN AIRCRAFT SUBJECTED TO A NEGATIVE PRESSURE - A drainage mast able to drain effectively the liquid contained in the compartment of an aircraft when the pressure within the compartment is lower than the outside pressure without using any pressure control active device and without causing any significant perturbation to the aerodynamic behavior of the aircraft. The drainage mast is configured with a cross section area decreasing from its entry section to the compartment to its outlet section and is disposed at an acute angle α relative to the compartment in the airflow direction. The entry and outlet sections have two perpendicular symmetry axes of different length, the entry section is arranged with its longer axis of symmetry substantially parallel to the airflow direction. The drainage mast has a symmetrical configuration with respect to a plane substantially perpendicular to the fuselage envelope passing through the longer axis of symmetry of the entry section. | 01-22-2015 |