Honeywell International Inc.

Sunit Kumar Saxena

Anita Sure

Gowtham Kumar Vankayala

Deepak Bhimrao Mahajan

Raghuveer Hanumanthrao Desai

Abhijit Kulkarni

Pandu Ranga Rao Somarowthu

Craig Giffen

William Tyson, Iii

Anand Vivek Ravi

Stephen Frederic Yates

Cristian E Anghel

Hariharan Saptharishi

Gobinathan Baladhandapani

Deepak Pitambar Mahajan

Shouvik Das

Gokul Murugesan

Shrikant P Rao

Mark Poling

Niranjan Kalyandurg

Rafeek Sainudeen

Sukumar De

George Rajan Koilpillai

Newel Stephens

Kartik Brahmbhatt

Vivek Ashok Joshi

Naman Rawal

Ezekiel Poulose

Venkatesan Santhirahasan

Milan Rajne

Sivakumar Kangarajan

Vaibhav Baranwal

Aniruddha A

Bharath Kumar Kabbur

Tarak Saha

Mobile apparatus and methods for ultraviolet (UV) light sanitization of an aircraft. The mobile apparatus generally comprises a mobile platform, such as a trolley, that has integrated therewith circuitry and devices that control and actuate ultra-violet C-spectrum (UV-C) light sources that are mechanically coupled to the trolley. The proposed mobile apparatus includes a controller that receives input from an operator and, optionally, from dosimeters mounted on the proposed system and/or within the aircraft. Based on the inputs received, the controller provides guidance to the operator in the form of alerts and messages, as well as automatically adjusting components of the mobile apparatus to adapt itself to a specific aircraft type.

Apparatus and method for ultraviolet (UV) light sanitization of an aircraft

A control system in a UVC-based aircraft sanitization system for controlling the UVC-based aircraft sanitization system to maintain a desired UVC (ultraviolet C) radiation level at a target surface in an aircraft under varying operating conditions is disclosed. The control system includes a controller configured to: receive measured radiation feedback from a radiation measurement device (e.g., dosimeter) on the target surface that identifies a radiation level that is applied at the target surface by the UVC-based aircraft sanitization system; and generate a UVC source control command for UVC sources in the UVC-based aircraft sanitization system. based on the received measured radiation feedback, to control the UVC sources to increase or decrease radiation level output (e.g., identify the amount of increase or decrease from the UVC sources) to generate sufficient radiation to achieve the desired radiation level at the target surface.

System and method for controlling a UVC based aircraft sanitization system

Systems and methods for controlling a searchlight mounted to an aerial vehicle. The systems and methods receive angular data representing a directional angle of a beam of the searchlight and location data representing a global location of the aerial vehicle from a sensor system of the aerial vehicle. The systems and methods determine coverage of the beam of the searchlight on ground based on the angular data and the location data. Based on the coverage of the beam, the aerial vehicle is controlled to change the global location, the display is controlled to depict the coverage of the beam on a map including historical coverage of the beam, and/or the searchlight actuator is controlled to adjust the direction of the beam.

Methods and systems for searchlight control for aerial vehicles

Modular apparatus and methods for ultraviolet (UV) light sanitization of an aircraft. The modular apparatus generally comprises a base frame that is universal, and multiple interchangeable modular kits to adapt the base frame to different aircraft cabin geometries. The base frame has integrated therewith circuitry and devices that control ultra-violet C-spectrum (UVC) light sources that are located on a frame of the modular kit. Various embodiments of the modular kits have five parts, and assemble the same way, for different aircraft cabin geometries.

Modular apparatus with universal base frame for ultraviolet (UV) light sanitization of an aircraft and methods for producing same

Methods and systems are provided for autonomously operating a retractable lighting arrangement. One method involves obtaining a current speed of the vehicle when the lighting arrangement is in an extended state, and when the current speed is greater than a threshold when the lighting arrangement is in the extended state, verifying one or more illumination elements associated with the lighting arrangement are in a deactivated state and thereafter automatically signaling an actuation arrangement associated with the lighting arrangement to transition the lighting arrangement from the extended state to a retracted state.

Retractable lighting systems and autoretraction methods

Systems and methods for an aircraft lighting system (ALS) are provided. The method includes co-locating a central light source subsystem including a blue light generator, red light generator, and green light generator, and a light generating control unit (LGCU) comprising a processor, and distributing a plurality of passive light-heads around an external surface of the aircraft. Each passive light-head of the plurality of passive light-heads is operationally coupled to a first side of a respective light switch of a respective plurality of light switches, the light switch being coupled on a second side to a light emitting output of the central light source subsystem. Controlling and actuating the light generators and the light switches in accordance with a load profile is performed by a light generating control unit (LGCU).

Architecture and method for aircraft lighting system using a centrally located red, green, and blue (RGB) light source subsystem and a plurality of distributed passive light-heads

Methods, devices and systems are provided for harmonizing output display characteristics of one component with those of other components onboard a vehicle, such as an aircraft. A line-replaceable unit (LRU) suitable includes a display driver to be coupled to a display command bus, a data storage element to maintain calibration information for the display driver, and a control module coupled to the display driver and the data storage element to identify a current state of an input command signal from the display command bus, identify an adjustment for the display driver based on the calibration information using the current state of the input command signal, and automatically operate the display driver in accordance with the adjustment.

LRUs and related night vision display harmonization methods

An aircraft collision avoidance system includes a plurality of three-dimensional (3D) light detection and ranging (LIDAR) sensors, a plurality of sensor processors, a plurality of transmitters, and a display device. Each 3D LIDAR sensor is enclosed in an aircraft exterior lighting fixture that is configured for mounting on an aircraft, and is configured to sense objects within its field-of-view and supply sensor data. Each sensor processor receives sensor data and processes the received sensor data to determine locations and physical dimensions of the sensed objects. Each transmitter receives the object data, and is configured to transmit the received object data. The display device receives and fuses the object data transmitted from each transmitter, fuses the object data and selectively generates one or more potential obstacle alerts based on the fused object data.

Lidar-based aircraft collision avoidance system

Systems and methods for moving an illumination spot of a searchlight beam at a constant groundspeed. The method includes receiving state data comprising an attitude for the mobile platform. The method computes an elevation angle, theta, of the beam as a function of the attitude, an elevation actuator angle and a known mounting orientation for the searchlight. Responsive to receiving a searchlight control command from a user input device, the method determines a respective rate of change of theta, dtheta/dt, and rate of change of Psi, dPsi/dt, required to maintain the constant groundspeed of the illumination spot, as a function of the state data. The method updates theta responsive to the determined dtheta/dt and generates actuator control commands for an elevation actuator based thereon. The method updates Psi responsive to the determined dPsi/dt, and generates actuator control commands for an azimuth actuator based thereon.

Searchlight control systems and methods for moving a beam of light emitted by a searchlight on a mobile platform at a constant ground speed

An aircraft lighting system (ALS) and apparatus which includes: a lighting generator control unit (LGCU) controlling a light source generator for generating a first, second and third type of light to each passive light head; a light bus coupled to the light source generator to receive the first, second, and third types of light and for converting the first type of light to a fourth type of light; a plurality of light transmission elements coupled to the light source generator; a plurality of light switches responsive to a switch command from the LGCU to optically not direct or direct light from the light bus to a light transmission element; a light conversion element connected for converting the first type to the fourth type of light; and the LGCU configured to command the light source generator to generate light in accordance with a load profile.

Aircraft lighting system to enable sharing of optical energy between light assemblies with passive light heads

A spherical electromagnetic machine includes a spherical stator, a plurality of longitudinal slots, a plurality of latitudinal slots, a plurality of longitudinal coils, a plurality of latitudinal coils, a first hemispherical shell rotor, and a second hemispherical shell rotor. The longitudinal slots and latitudinal slots are formed in, and are spaced evenly around, the outer surface. The longitudinal coils are disposed within a different one of the longitudinal slots. The latitudinal coils are disposed within a different one of the latitudinal slots. The first and second hemispherical shell rotors are mounted for rotation relative to the spherical stator body and have magnets on their inner surfaces. A Lorentz force causes movement of the first and second hemispherical shell rotors when electrical current is supplied to one or more of the longitudinal coils or to one or more of the latitudinal coils.

Spherical electromagnetic machine with two degrees of unconstrained rotational freedom

Provided systems and methods for an aircraft lighting system (ALS) include a centralized blue generator that supplies blue light to a plurality (N) of passive light-heads distributed at various locations on the aircraft. A load profile for use of the N passive light-heads during all flight phases and operational phases is developed and uploaded into the system. Each of the passive light-heads is operationally coupled to the blue light generator via a respective light transmission element that is gated with a respective one of N light switches. A light generating control unit (LGCU) is coupled to the blue light generator, and controls the generation and actuation of blue light, in addition to controlling light switch positions, as a function of navigation data and the load profile. Each of the N passive light-heads comprises a respective light conversion element to convert the blue light into red, green, or white light.

Architecture and method for aircraft lighting system using a centralized blue light source and a plurality of distributed passive light-heads

Systems and methods for an auto-land system for a rotorcraft are provided. The system includes, a search light (SL) assembly configured to receive user input directing the SL to a point of interest (POI) and determine an actual SL orientation and an actual SL range to the POI; and, a searchlight controller operationally coupled to the search light assembly, and configured to: responsive to receiving a command to auto-land at the POI, begin (i) generating a desired trajectory from the rotorcraft actual orientation and rotorcraft actual range to the POI; (ii) generating guidance commands for navigating the rotorcraft in accordance with the desired trajectory; (iii) monitoring an actual SL range and an actual SL orientation; and (iv) generating controlling commands for the searchlight assembly in accordance with the coordinates of the POI.

Searchlight auto-land system

A system for transferring data between an on-board server and an off-board server of a vehicle is provided. The system comprises: a light mounted to an exterior of a vehicle; an external network comprising an external wireless access point comprising a first antenna positioned on the exterior of the vehicle at the location of the light, the external network configured to automatically connect to an off-board server, the off-board server located outside the vehicle; an internal network comprising internal wireless access point comprising a second antenna, the second antenna positioned on the interior of the vehicle at the location of the light, the internal network configured to automatically connect to an on-board server, the on-board server internal to the vehicle; and a circuit coupled to the external access point and to the internal access point, the circuit configured to transfer data bi-directionally between the off-board server and the on-board server.

System and method for bi-directional communication of data between servers on-board and off-board a vehicle

A lighting device including a plurality of light-emitting semiconductor devices. The light-emitting semiconductor devices are separated into at least two subgroups. The lighting device further includes a plurality of optics separated into at least two subgroups, which are arranged relative to the plurality of light-emitting semiconductor devices such that each one of the plurality of light-emitting semiconductor devices of a first subgroup is located at a focal point of a respective optic of a first subgroup of the plurality of optics, and such that each one of the plurality of light-emitting semiconductor devices of a second subgroup is located at a focal point of a respective optic of a second subgroup of the plurality of optics. The optical properties of the first subgroup and second subgroup of the plurality of optics are different. The lighting device further includes a controller module configured to control at least two current signals supplied from a power source to each of the at least two subgroups of light-emitting semiconductor devices, respectively. The controller module is configured to modify the beam width and the peak intensity of the emitted beam of light by varying the magnitude of the respective at least two current signals.

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Karnataka, India

Sunit Kumar Saxena