Honeywell International Inc.

Ademco Inc.

Wittenstein Aerospace and Simulation Ltd.

James I Kern

Philip Ferro

William R Blum

Thomas Paul Schmit

Casey Hanlon

Paul T Wingett

Patrick R Lemire

Cherry Lv

Bo Wang

Jeffrey Stuart

Louie Timothy Gaines

Paul S Evans

Justin A Tanner

Michael Landi

Calvin C Potter

Todd Langston

David B Tornquist

Douglas C Smith

Alice DeBiasio

David A Cowling

Christopher Coleman

James Casey Hanlon

Kaja Mohaideen Yousuff

Systems and methods for correcting network connectivity of a connected device are provided. Such systems and methods can include a mobile device determining whether the mobile device can connect to and communicate with a connected device, and the mobile device determining whether the mobile device is connected to a home network. When the mobile device cannot connect to and communicate with the connected device, but is connected to the home network, such systems and methods can include the mobile device transmitting or displaying messages documenting a troubleshooting process to restore the network connectivity between the mobile device and the connected device. Contents of the messages can be dependent on whether some or none of current network connectivity information related to a current network connection between the mobile device and the home network matches stored network connectivity information.

Systems and methods for correcting network connectivity of a connected device

Systems and methods for delaying transmission of an alarm signal responsive to detecting delay actions indicative of progress towards confirming or denying the alarm signal are provided and can include an alarm processing device receiving the alarm signal and determining whether a user device is enrolled in an alarm notification service. When the user device is enrolled in the alarm notification service, the alarm processing device can transmit a notification to the user device, start a delay timer, and determine whether a first delay action associated with the user device is detected prior to expiration of the delay timer. When the first delay action is detected prior to the expiration of the delay timer, the alarm processing device can alter the delay timer consistent with a next delay action associated with the user device and, when the delay timer expires, transmit the alarm signal to the central monitoring station.

Systems and methods for delaying transmission of an alarm signal to a central monitoring station in response to detecting delay actions

An asynchronous reporting mechanism for a remote device in a heating, ventilation and air conditioning environment. Using gateway information, such as a device address, report information may be sent to the user account, or using another approach, the information may be sent directly to the user. An asynchronous message may be sent without user intervention or request.

Asynchronous reporting system

Systems and methods for reducing false alarms and providing a central station with information regarding occupants in a monitored region using a GPS location of a mobile device are provided. Some methods can include receiving a first signal indicative of a detected alarm condition in the monitored region, responsive to receiving the first signal, transmitting a second signal to the mobile device, receiving a third signal from the mobile device indicative of the GPS location of the mobile device, and based on a location of the monitored region and the third signal indicative of the GPS location of the mobile device, determining a likelihood of whether the detected alarm condition is real or false. Additionally or alternatively, some methods can include receiving the signal from the mobile device indicative of the GPS location of the mobile device at predetermined periodic time intervals and irrespective of the detected alarm condition in the monitored region.

Systems and methods for reducing false alarms using the GPS location of a mobile device

A social networking site that communicates with a plurality of human users can also communicate with a plurality of non-human users. Information from one of the non-human users can be automatically received at the site and evaluated. Commands can be automatically transmitted to another of the non-human users in response to the evaluation. A human readable indicator can be posted at a page of the site.

System and method of monitoring, control and configuration of security and lifestyle devices

A human-machine interface assembly includes a user interface and a passive force feedback mechanism. The user interface is configured, upon receipt of an input force that exceeds a null breakout force, to move from a null position to a first control position and, upon receipt of an input force that exceeds a soft stop force, to move beyond the first control position. The passive force feedback mechanism is coupled to the user interface and is configured to supply the null breakout force to the user interface when the user interface is in the null position, and supply the soft stop force to the user interface when the user interface is in the first control position. The soft stop force exceeds the null breakout force and is not supplied to the user interface unless the user interface is in the first control position.

Human-machine interface with passive soft stops

An apparatus is provided for biasing a shaft toward, and releasably securing it in, a predetermined position. The apparatus comprises a magnetic assembly coupled to the shaft for releasably securing the shaft in a predetermined position, a first member coupled to and extending from the shaft for rotating the shaft from the predetermined position, and a spring assembly coupled to the shaft for securing the shaft in the predetermined position.

Apparatus for releasably securing a rotatable object in a predetermined position

A position sensing system includes a plurality of two-axis anisotropic magneto-resistive (AMR) sensors to determine the position of a user interface. A magnetic member is coupled to the user interface, which is movable to a position along a random path. The plurality of two-axis AMR sensors is arranged in a two-dimensional sensor array that is spaced apart from the magnetic member. A signal processor circuit is operable to sense the electrical resistance values of each two-axis AMR sensor, to determine the position of the user interface from the resistance values, and to supply position feedback data representative of the determined position.

Two-dimensional position sensing system

Flight control systems and methods for rotorcraft are provided. The flight control system includes a user input device and a motor in operable communication with the user input device. The motor includes a plurality of winding sets and an armature coupled to the plurality of winding sets. The armature includes multiple magnets. The winding sets and the armature are configured such that when one or more of the plurality of winding sets are selectively energized, the armature moves relative to the one or more of the plurality of winding sets.

Electromechanical flight control system and method for rotorcraft

An active user interface assembly includes a user interface, and one or more feedback motors coupled to the user interface. The one or more feedback motors, when energized, supply a feedback force to the user interface that opposes user interface movement. One of the feedback motors is disposed such that its center of gravity is located at a position relative to the user interface to mass balance the user interface when it is in the null position. The configurations allow for the center of gravity of a feedback motor to be positioned in a manner that alleviates the need for counterbalance weights.

Motor balanced active user interface assembly

A flight control actuation system comprises a controller, electromechanical actuator and a pneumatic actuator. During normal operation, only the electromechanical actuator is needed to operate a flight control surface. When the electromechanical actuator load level exceeds 40 amps positive, the controller activates the pneumatic actuator to offset electromechanical actuator loads to assist the manipulation of flight control surfaces. The assistance from the pneumatic load assist actuator enables the use of an electromechanical actuator that is smaller in size and mass, requires less power, needs less cooling processes, achieves high output forces and adapts to electrical current variations. The flight control actuation system is adapted for aircraft, spacecraft, missiles, and other flight vehicles, especially flight vehicles that are large in size and travel at high velocities.

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Phoenix, AZ, United States of America

James I Kern