Caldeira
Alexandre Padrin Caldeira, Jaguariuna, Sp BR
Patent application number | Description | Published |
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20120170732 | Methods and Devices for Providing a Called Party's Name to a Setup Message - Disclosed are communication devices and methods of a communication devices that include accessing the contact list of the memory by the controller, initiating communication based upon the contact list input by the controller and generating by the controller, a setup message that includes communication address data populating a field for a communication address and includes identification data populating a field for identification information. The disclosed method can further include transmitting a call setup message signal of a control channel, such as a stand-alone dedicated control channel including a populated field for identification information. Moreover, additional data populating a field for additional information can also be included in the call setup message signal. The additional data can represent for example, the purpose of the call, such a personal call or a business call or any other additional information. | 07-05-2012 |
Fabricio Reis Caldeira, Sao Jose Dos Campos - Sp BR
Patent application number | Description | Published |
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20090062973 | STALL, BUFFETING, LOW SPEED AND HIGH ATTITUDE PROTECTION SYSTEM - A flight control system moves elevators according to a pilot command summed with an automatic command. The flight control system monitors a set of flight parameters to determine if the flight vehicle is operating inside a permitted envelope. The flight controls system incorporates automatic protections thru the automatic elevator command if the flight vehicle is close to its envelope limits. The exemplary illustrative non-limiting implementation herein provides automatic protections in order to protect the flight vehicle from low speeds, high attitude, stalls and buffetings. | 03-05-2009 |
20100217460 | FLIGHT CONTROL SYSTEM - A flight control system commands drag devices such as flight spoilers according to pilot or autopilot longitudinal command. Furthermore, the flight control system monitors a set of flight parameters to determine whether the aircraft is operating inside the permitted safe envelope, hence, incorporating envelope automatic exceeding disengagement. This invention allows the aircraft to descend in a steeper glide path than the 3° used in the normal approach, while keeping speeds unchanged. | 08-26-2010 |
20110054720 | STALL, BUFFETING, LOW SPEED AND HIGH ATTITUDE PROTECTION SYSTEM - A flight control system moves elevators according to a pilot command summed with an automatic command. The flight control system monitors a set of flight parameters to determine if the flight vehicle is operating inside a permitted envelope. The flight controls system incorporates automatic protections thru the automatic elevator command if the flight vehicle is close to its envelope limits. The exemplary illustrative non-limiting implementation herein provides automatic protections in order to protect the flight vehicle from low speeds, high attitude, stalls and buffetings. | 03-03-2011 |
20130138274 | Flight Control System Mode And Method Providing Aircraft Speed Control Through The Usage Of Momentary On-Off Control - A longitudinal control law is designed to optimize the flying qualities when aircraft is set to approach configuration, i.e. when the flap lever is set to the landing position and landing gears are locked down. Under such circumstances, the effort of trimming the aircraft speed can be extremely reduced by the usage of a momentary on-off switch or other control in the sidestick, instead of or in addition to a conventional trim up-down switch, making easier the task of airspeed selection by the pilot. This control law provides excellent handling qualities during approach and landing, with the benefit of not needing or using radio altimeter information in safety-critical applications. | 05-30-2013 |
Fabricio Reis Caldeira, Sao Jose Dos Campos BR
Patent application number | Description | Published |
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20140249704 | STEEP APPROACH PERFORMANCE IMPROVEMENTS AND OPTIMIZATION - A flight control system can achieve a relatively steep descent (using drag devices such as flight spoilers) at relatively low speeds while retaining good airplane handling qualities from the pilot's point of view. The system and method optimize the drag device's positioning used to perform steep approach to improve performance. | 09-04-2014 |
Fabrício Reis Caldeira, Sao Jose Dos Campos-Sp BR
Patent application number | Description | Published |
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20130138274 | Flight Control System Mode And Method Providing Aircraft Speed Control Through The Usage Of Momentary On-Off Control - A longitudinal control law is designed to optimize the flying qualities when aircraft is set to approach configuration, i.e. when the flap lever is set to the landing position and landing gears are locked down. Under such circumstances, the effort of trimming the aircraft speed can be extremely reduced by the usage of a momentary on-off switch or other control in the sidestick, instead of or in addition to a conventional trim up-down switch, making easier the task of airspeed selection by the pilot. This control law provides excellent handling qualities during approach and landing, with the benefit of not needing or using radio altimeter information in safety-critical applications. | 05-30-2013 |
Nancy Manuela Caldeira, Neuilly Sur Seine FR
Patent application number | Description | Published |
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20120085261 | CERAMIC PARTICLES AND COATING COMPOSITIONS INCLUDING SAID PARTICLES - The present invention relates to coating compositions for metallic devices, especially for aircrafts, to provide protection against corrosion. The coating composition comprises ceramic particles having at least one active material substantially homogeneously distributed throughout each particle. The active material being releasable in the presence of a liquid by solubilization into the liquid. | 04-12-2012 |