Honeywell International Inc.

General Electric Company

Ankita Sinha

Maksood Moidin Kadike

Andrea Antonini

John Joyson

Dinesh Ramalingam

Vivek Kalyan

Ravindra Shankar Ganiger

David Raju Yamarthi

Narayanan Payyoor

Kudum Shinde

Tod Robert Steen

Venkata Subramanya Sarma Devarakonda

Rajesh Kumar Undipalli

Himanshu Gupta

Dinesh Rakwal

Hrishi Ragesh

Aman Srivastava

Methods, devices, and systems for ground traffic aircraft management are described herein. One device includes a user interface, a memory, and a processor configured to execute executable instructions stored in the memory to receive airport information associated with an airport, generate, using the airport information, a map of the airport, display an intersection on the map of the airport, receive a selection of the intersection, and display flight information of each of a plurality of aircraft passing through the intersection within a particular period of time and the map of the airport in a single integrated display responsive to receiving the selection of the intersection.

Ground traffic aircraft management

A gas turbine engine includes a fan section having a plurality of fan blades, the fan section configured to generate an airflow through the gas turbine engine, an airflow passage having a core passage and a bypass passage separate from the core passage, a low-speed shaft coupled to and configured to rotate the plurality of fan blades, and a sensor assembly coupled to the gas turbine engine and configured to detect torsional vibration in the low-speed shaft. The sensor assembly includes a plurality of dynamic pressure sensors in the airflow passage. The plurality of dynamic pressure sensors detect a dynamic pressure of the airflow passage that is indicative of the torsional vibration in the low-speed shaft. A damping system is configured to dampen the torsional vibration in the low-speed shaft based on a correlation of a measured torsional vibration and an experimental torsional vibration.

Gas turbine engine having a sensor assembly to detect torsional vibration

Methods, devices, and systems for air traffic control (ATC) flight management are described herein. One device includes a memory, and a processor to execute executable instructions stored in the memory to receive airport information associated with an airport, generate, using the airport information, an ATC flight management analysis that includes an airport map showing locations of aircraft at the airport and a card panel including a number of flight cards, where each respective one of the number of flight cards corresponds to a different respective one of the aircraft at the airport, and a user interface to display the ATC flight management analysis in a single integrated display.

Air traffic control flight management

Methods, devices, and systems for air traffic control flight management are described herein. One device includes a memory, and a processor to execute executable instructions stored in the memory to receive airport information associated with an airport, generate, using the airport information, a card panel including a number of flight cards, wherein each respective one of the number of flight cards corresponds to a different respective aircraft at the airport, and a user interface configured to display the card panel in a timeline view in a single integrated display.

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Bengaluru, India

Ankita Sinha