Honeywell International Inc.

Danny Thomas Kimmel

Grant A Gordon

Xiao Zhu Fan

Grant Lodden

Jason Garde

Brett Gordon Northcutt

Morris G Anderson

Mats Anders Brenner

John R Morrison

James B Cox

Jay Joseph Hansen

Brett Gorrdon Northcutt

In one embodiment, a system includes a vehicle and a laser air data sensor, including a laser transceiver configured to transmit one or more laser light beams, mounted to the vehicle. In some embodiments, a window of the laser transceiver is fixed and oriented to transmit one or more laser light beams away from the vehicle and approximately parallel to a vertical axis of the vehicle. In some embodiments, a window of the laser transceiver is fixed and oriented to transmit one or more laser light beams toward another portion of the vehicle. In some embodiments, the system further includes a processing device configured to control the laser air data sensor to attenuate the one or more laser light beams based on one or more operating parameters of the vehicle.

Laser air data sensor mounting and operation for eye safety

A method of enhancing LiDAR data is provided. The method includes inputting LiDAR data from at least one LiDAR sensor; inputting data from at least one of: at least one static pressure sensor; and at least one total air temperature sensor; and extracting accurate air data parameters by processing one of: the LiDAR data and static pressure data from the static pressure sensor; the LiDAR data and true temperature data from the total air temperature sensor; or the LiDAR data, the static pressure data from the static pressure sensor, and the true temperature data from the total air temperature sensor. The method also includes generating augmented air data based on the extracted accurate air data parameters and outputting the augmented air data.

Enhanced LiDAR air data using supplementary sensor outputs

Systems and methods for the co-location of high-maintenance air data system components into one LRU are disclosed. In at least one embodiment, an air data sensing line-replaceable unit (LRU) comprises at least one pressure sensor and at least one probe or port coupled to the at least one pressure sensor. The at least one probe or port conduits air located outside the air data sensing LRU to the at least one pressure sensor. Further, the at least one probe or port and the at least one pressure sensor are connected to each other by a permanent connection.

Co-location of high-maintenance air data system components into one LRU

A system for power management of air data probes is provided. The system comprises a power source in an aircraft, and two or more air data probes electrically connected to the power source. Each of the air data probes comprises a body structure coupled to a fuselage of the aircraft, and at least one electrical heater coupled to the body structure and in electrical communication with the power source. A switching mechanism is coupled between the power source and the electrical heater of each of the air data probes. The switching mechanism is controllable such that the electrical heater of each of the air data probes is electrically connectable to the power source in parallel or in series.

Architecture for air data probe power supply control

A control circuit for a probe includes: at least one low thermal coefficient resistance (TCR) component placed in a first section of a probe, wherein the at least one low TCR component has low positive temperature resistance coefficient (PTC); at least one high TCR component placed in a second section of the probe and connected in series with the at least one low TCR component, wherein the at least one high TCR component has high PTC, and wherein the at least one high TCR component responds to temperature differently than the at least one low TCR component; and at least one shunt component connected in parallel with the at least one high TCR component, wherein when temperature of the at least one high TCR component exceeds a set temperature point, the at least one shunt component is activated to reduce current flowing through the at least one high TCR component.

Power control for an air data probe

Systems and methods for attitude fault detection based on air data and aircraft control settings are provided. In one embodiment, a sensor monitor for an aircraft attitude measurement system comprises: an aircraft model configured to model a plurality of states, the plurality of states including at least an aircraft attitude state, an aircraft velocity state, a sink rate error state, and a wind velocity state; a propagator-estimator configured to utilize the plurality of states of the aircraft model to process air data measurements and attitude measurements from a first inertial measurement unit of the aircraft attitude measurement system; and a residual evaluator configured to input residual error values generated by the propagator-estimator, wherein the residual evaluator outputs an alert signal when the residual error values exceed a predetermined statistical threshold.

Growing community of inventors

Phoenix, AZ, United States of America

Danny Thomas Kimmel