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Goodrich Aerospace Services Private Limited patents


Recent patent applications related to Goodrich Aerospace Services Private Limited. Goodrich Aerospace Services Private Limited is listed as an Agent/Assignee. Note: Goodrich Aerospace Services Private Limited may have other listings under different names/spellings. We're not affiliated with Goodrich Aerospace Services Private Limited, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "G" | Goodrich Aerospace Services Private Limited-related inventors


Method of applying brake to a hoist by electromagnetic means in a permanent magnet motor

Embodiments herein relate to a permanent magnet (pm) motor driven hoist with a motor based electromagnetic brake. The hoist includes a direct current (dc) power source, a pm motor having stator coils and a pm rotor operably coupled to a cable drum with a cable wrapped thereon. ... Goodrich Aerospace Services Private Limited

Dual mode aircraft indicator sign

A device for forming a dynamic image on an aircraft sign includes a plurality of light sources, an input power line, a first timer and a second timer both connected to an enable input and a plurality of delay circuits each connected to a different one of the light sources. The system also includes a counter having a plurality of counter outputs, the counter receiving a counting pulse from the first timer in a dynamic mode of operation and disable signal from the second timer after expiration of a preset time, the expiration of the preset time causing the device to transfer from the dynamic mode to a static mode where each of the plurality of light sources are simultaneously illuminated.. ... Goodrich Aerospace Services Private Limited

Valve assembly having a manual override unit

A valve assembly includes a housing, an actuator, a plunger, a cover, a valve body, and a manual override unit. The actuator is received within the housing and is disposed between a first annular wall and a second annular wall. ... Goodrich Aerospace Services Private Limited

Electrical architecture for slat/flap control using smart sensors and effectors

A centralized control system and/or method for controlling an aircraft are provided. The centralized control system includes a controller configured to receive a device signal and transmit a control signal, a communication bus connected to the controller being configured to transport the device signal and the control signal, a plurality of devices connected to the controller using the communication bus, wherein at least one of the plurality of devices includes at least one of a sensor being configured to collect the device signal and an effector configured to respond to the control signal, and a bus communication circuit configured to communicate over the communication bus to the controller.. ... Goodrich Aerospace Services Private Limited

Actuator mechanism

An actuator system comprising a rotatable lock mechanism defining a path for an actuator pin as the actuator is expanded and retracted, wherein the lock mechanism defines an entry passage through which the pin enters as the actuator extends, a guide surface along which the pin travels from the entry passage as the actuator retracts, a locking recess into which the pin is guided by the guide surface, and an exit passage into which the pin is guided as it is caused to leave the lock recess by extension of the actuator and subsequent retraction; whereby a detent surface is provided to prevent the pin returning back into the lock recess when the actuator is extended to cause the pin to leave the lock recess.. . ... Goodrich Aerospace Services Private Limited

Hybrid material pitot tube

A pitot tube includes a substantially cylindrical body portion having an interior defining a flow passage and a tip portion extending along a pitot tube axis from the body portion. The tip portion includes a disk, a tip cover and a high thermal conductive insert disposed between the disk and the tip cover and in thermal contact with both.. ... Goodrich Aerospace Services Private Limited

Variable sweep angle motor drive

A windshield wiper system for an aircraft is provided and includes a motor, an output shaft, a wrap spring and crank rocker mechanism (wscrm) to which the motor and the output shaft are coupled and a controller. By way of the wscrm, first directional rotation input to the wscrm from the motor via a two-stage gear reduction is converted such that the output shaft drives wiper blade oscillation through a first sweep angle and second directional rotation input to the wscrm from the motor is converted such that the output shaft drives wiper blade oscillation through a second sweep angle. ... Goodrich Aerospace Services Private Limited

Twin wire bending kinetic energy attenuation system

A mechanism for decreasing kinetic energy includes a carriage to connect to an object, a first wire passing through a top portion of the carriage, a second wire coterminous with the first wire at a top end and a bottom end, a spreading wheel axially fixed in a center position of the carriage between the first and second wires to plastically deform the first and second wires from a substantially parallel configuration to conform to a circumferential surface on two opposing sides of the spreading wheel as the carriage moves from the top to the bottom end, and a pair of despreading wheels axially parallel to and oriented proximal to the spreading wheel such that the first and second wires are deformed by a circumferential surface of each of the despreading wheels such that they are deformed again as the carriage moves from the top to the bottom end.. . ... Goodrich Aerospace Services Private Limited

Powerless self operated landing gear uplock system

A systems and methods for uplock systems are provided. An uplock system may comprise a body, a hook having an opening defining at least a first surface and a second surface, the hook being rotationally engaged with the body, a first biasing member configured to bias the hook in a first rotational direction relative to the body, and a cam in operable communication with the hook and the body such that the hook has at least a first stable position and a second stable position relative to the body when biased in the first rotational direction.. ... Goodrich Aerospace Services Private Limited

Adjustable interface pressure device

A method and system to provide an occupant support device includes a first inflatable tube, a second inflatable tube disposed parallel to the first inflatable tube, a third inflatable tube disposed at a relative angle to the first inflatable tube, above the first inflatable tube and below the second inflatable tube, a fourth inflatable tube disposed parallel to the third inflatable tube, below the first inflatable tube and above the second inflatable tube, and an inflation device to selectively provide a low pressure and a high pressure to at least one of the first inflatable tube, the second inflatable tube, the third inflatable tube, and the fourth inflatable tube.. . ... Goodrich Aerospace Services Private Limited

Occupant restraint system and method of operating

An occupant restraint system includes a plurality of occupant residences each including a restraint assembly having a latch mechanism manually movable between a latched state and an unlatched state and an electric lock mechanism movable from an unlocked state to a locked state when the latch mechanism is in the latched state. The control console includes an electronic display of the plurality of occupant residences and a user interface for actuating the electric lock mechanism between the locked state and the unlocked state. ... Goodrich Aerospace Services Private Limited








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