HONEYWELL UNCREWED AERIAL SYSTEMS AND URBAN AIR MOBILITY SYSTEMS OVERVIEW DAVID SHILLIDAY VP/GM, ADVANCED AIR MOBILITY Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. AEROSPACE SUSTAINABILITY PRODUCTS SUSTAINABLE AVIATION FUEL (SAF) HONEYWELL AEROSPACE TRADING (HAT) HONEYWELL FLIGHT EFFICIENCY HIGH EFFICIENCY MODE (HEM) FOR 131-9 APU ELECTRIC PROPULSION HYDROGEN FUEL CELL ELECTRIC POWER mVCS with Solstice® Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. AVIATION ROADMAP TO ZERO EMISSIONS Entry into service 2020 2025 2030 2035 2040 2045 2050 Challenge: Fuel Storage and Systems Challenge: Production Capacity Sustainable Aviation Fuels Hydrogen Challenge: Range Batteries Fuel cells and H2 burning turbines Challenge: Fuel Storage and Infrastructure AERO SOLUTIONS IN EVERY WORKSTREAM Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. HONEYWELL MAKES THIS FUTURE A REALITY HONEYWELL UAM/UAS by providing vehicle systems and integration for OEMs across all vehicle categories Dedicated business unit to address the needs of the uncrewed aerial systems and urban air mobility, with a specific focus on transportation applications COMPLETE SYSTEM for integration and value MAJOR SUB-SYSTEM to balance modularity with specialization OUR VISION AIR CARGO is autonomous from warehouse to your house – same day delivery anywhere in the populated world REGIONAL AIR TRAVEL is ubiquitous with electric urban air taxis that pick up and drop off passengers in every neighborhood DEFENSE SYSTEMS are supported with attritable drone systems that improve communication, coordination and safety INTEGRATED PROPULSION AND AVIONICS SYSTEM INDIVIDUAL PRODUCTS to create a unique system INTEGRATED PROPULSION SYSTEM INTEGRATED AVIONICS SYSTEM Thermal management Compact fly-by-wire Turbo-generated electricity Vehicle management Motor Actuation Motor control Detect and avoid Battery management system (Partner) Communications Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. Honeywell Confidential - ©2020 by Honeywell International Inc. All rights reserved. HONEYWELL UAS | CERTIFIABLE EXPERIENCE For UAM OEMs that need technologically superior and low C-SWAP solution for their vehicles, Honeywell is the leading provider of certifiable integrated UAM systems because of our decades of experience designing and certifying aerospace products and our investments in UAM technology Developing System Solutions That Allow Simpler Integration Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. Long Tradition of Successful Certification Experience Trusted Leader in Safety and Reliability HONEYWELL CREATES THE CRITICAL SYSTEMS THAT MAKE DISRUPTIVE AVIATION POSSIBLE LOW COST: electrification, automation and vertical takeoff + fixed wing cruise flight reduce operating cost by 35% - 75% QUIET OPERATIONS: small rotors with low tip speed leads to 100x quieter operations compared to helicopters HIGH SAFETY: multiple rotors and automated flight control eliminate single point failure and supports robust vertical takeoff SUSTAINABLE: all-electric powertrain eliminates pollutants and carbon emissions at point of application Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. INTEGRATED AVIONICS SYSTEM Integrated Avionics System is composed of Vehicle management system Autonomous tactical nav & DAA Fly-by-wire Connectivity Mature and certifiable system for a faster EIS • Demonstration units for FBW, DAA and connectivity products already delivered to other customers MODULAR ARCHITECTURE to support simplified vehicle operations (SVO), autonomy and third party integration CUSTOMIZED AND SCALABLE SOLUTION for your aircraft ELIMINATES RISKS & CHALLENGES WITH FEDERATED SYSTEMS Simplify supply chain COMPOSED OF BEST-IN-CLASS SUBSYSTEMS with lowest C-SWAP in their category Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. INTEGRATED PROPULSION SYSTEM Integrated Propulsion System is composed of Turbogenerator Motors Thermal Management Motor Controllers Mature and certifiable system for a faster EIS • Flight test hardware available 2023, production units in 2023/2024 timeframe HIGH POWER DENSITY up to 1MW available through turbogenerator system; electric motors can be stacked for additional power CUSTOMIZED AND SCALABLE SOLUTION with 3 cooling ratings and both axial and radial flux motor designs SYSTEM INTEGRATION OF DESIGNS For simpler and quicker packaging of solutions HIGH VOLUME PRODUCTION Made possible through our motor partnerships Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. AERO SECURING THE FUTURE OF AVIATION Won Won Vertical Aerospace – Integrated avionics, compact fly-by-wire system Lilium – Integrated avionics, compact flyby-wire system, e-motor Won Won Archer Aviation – Flight control actuation, thermal management system Hyundai Supernal – Integrated avionics Won Won HIGHLIGHTS • $7B+ in content awards across multiple customer types with varying missions and EIS dates • Applying existing technology, tailoring offerings, & creating new products • Wins across all Honeywell Aerospace key business units • $10B+ in pipeline over next 5 years Dual-use cargo customer – Compact fly-bywire system Pipistrel (Nuuva 300 – Compact fly-by-wire system, VersaWave SATCOM • Potential to generate ~$2B in revenue by 2030 LAUNCHING A REVOLUTION IN AERIAL TRANSPORTATION AND LOGISTICS Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. OEM LANDSCAPE Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. RULEMAKING LANDSCAPE Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. HONEYWELL ADVANCED AIR MOBILITY SUMMIT Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. PRODUCT OVERVIEWS VEHICLE MANAGEMENT SYSTEM Designed for UAM and Cargo UAVs • Cockpit displays • Flight management system • Navigation solutions • Radar altimeter • Connectivity • Remote data concentrator • Satcom • Sensors and radios MODULAR ARCHITECTURE provides seamless upgrade path to SVO and autonomy SEAMLESS INTEGRATION with third party applications BUILT-IN CONNECTIVITY to integrate with ground systems System weight 70 LBS. Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. COMPACT FLY-BY-WIRE ELECTRONIC CONTROL ENVELOPE PROTECTION TRIPLE REDUNDANCY of wing surfaces and thrust reduces pilot workload and training with dissimilarity DIMENSIONS: 9.0” X 8.1” X 3.4” WEIGHT: 4 lbs. POWER: 18 Watts MTBF: 50,000 – 65,000 hours DESIGNED FOR SC-VTOL regulations INTERFACES ADAPTABLE with actuators and motors to various aircraft configuration “Even for a non-pilot, the aircraft is incredibly easy to fly” – CEO of a UAM OEM based in Europe INCLUDES CONTROL LAW PASSIVELY COOLED implementation Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. NO MAINTENANCE REQUIRED Heritage from air transport FLY-BY-WIRE SYSTEMS Selected on multiple EVTOL PLATFORMS ACTUATION • Linear and rotary electromechanical actuation • COTS design/hardware opportunity Over 60 YEARS of experience and 250 QUALIFIED actuator components LINEAR ballscrew, low & high loads/rates BRUSHLESS MOTOR with or without brake ROTARY compound planetary or hingeline RELIABILITY./AVAILABILITY single channel or redundancy, high reliability designs 28 VDC, 270 VDC, and 900 VDC INTEGRATED MOTOR DRIVE and actuator control electronics or separate control unit SAFETY high integrity, fail passive ACTUATOR OUTPUT position sensing (VDT, resolver, hall effect) Seamless integration with Honeywell compact fly-by-wire system Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. HONEYWELL SMALL UAV SATCOM TECHNICAL SPECIFICATIONS POWER SPECIFICATIONS Standby 17W Terminal Class 15 Max Data Rate 200kbps (100Kbps) 44W Tx Power 11.4 dBm Maximum 53W Coverage Inmarsat BGAN (L-Band) Recommended Supply 28V GPS (Connected to Network) Typical Yes SIZE IP Background Data Connectivity Streaming 8, 16 and 32 Kbps SATCOM Data Unit Antenna HARDWARE WEIGHT 5.5”x2.9”x1.9” SATCOM Terminal 1kg 5.6”x4.4”x2” CLICK HERE TO VIEW PRODUCT VIDEO No hosted video compression • 720P HD FMV STREAMING @ 10-15FPS Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. THERMAL MANAGEMENT Micro Vapor Cycle System provides active cooling in compact, lightweight unit • 20% more cooling than alternatives • 35% lighter than alternatives • Uses low Global Warming Potential Solstice ZD refrigerant • Oil free technology eliminates scheduled maintenance reducing operating costs • Air-cooled silicon-carbide motor controller for lower weight and obsolesce protection 3 variants for 6, 11, 20 kW of cooling One unit can provide cooling for Avionics Cabin Batteries Motors and motor controllers Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. ELECTRIC PROPULSION • High power density 50-125kW electric propulsion • motors and controllers Axial or radial flux designs INTEGRATED AIR COOLED EPU • Can be stacked or mounted side-by-side for additional power • Supports direct drive and geared solutions Adaptable to various vehicle configurations LIQUID COOLED MOTOR High volume, low-cost achieved through automotive-scale mass production LIQUID COOLED MOTOR CONTROLLER Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. GPSDOME ANTI-JAM DEVICE • Add-on device provides protection against jamming • Null steering algorithm • Low power consumption: less than 0.8W • Matchbook-size OEM board • Not ITAR controlled Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. 1-MEGAWATT TURBOGENERATOR • Industry-leading power density • Uses traditional jet fuel or sustainable aviation fuel (SAF) • Proven HGT1700 power core flies on every Airbus A350 • Tailorable for any hybrid architecture; scalable for higher and lower power needs Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. FUEL CELL POWER Group 1, 2 and 3 fixed wing Group 2 VTOL Group 1 VTOL 7-10x Endurance Silent and low thermal signature Battery Endurance (hr.) Fuel Cell Endurance (hr.) sUAS 3 to 5.5 20 to 48 VTOL sUAS 0.5 to 1 5 to10 Loitering munitions 0.15 to 0.3 1 to 2 No moving parts; high reliability relative to IC engines Air-transportable “printer” fuel cartridge greatly simplifies combat logistics Cross-leverage investment in UAM / AAM Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. MULTIPLE FUELING APPROACHES Gaseous H2 Tank Liquid H2 Tank Solid State H2 Cartridge Gaseous Hydrogen: Straightforward and being deployed today Liquid Hydrogen: Higher energy density, but added complexity Solid State Hydrogen: Low complexity and easy logistics, higher cost Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. ADVANCE SENSING TECHNOLOGIES Heavy Duty Pressure Board Level Pressure Air Flow IMU Thermal Switch Temperature Speed / Direction Position Proximity / Magnetic Micro-Force Current LVDT/RVDT Humidity Particle Barcode Scanning Gas Basic Switches Sealed Switches Limit Switches Pressure Switches Toggle Switches PB/Rocker Switches Controls / Relay Elevator Interlock Switches / Monitors Pressure Load Torque Vibration / Acceleration Service Display / Amplifiers Calibration & Repair Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. Hazardous / Safety Switches STANDARD MEMS IMUS i808 High grade RLG IMU Due mid-2022 HG4930 (i500) FOG replacement IMU In Production i300 Low weight, mid performance I808 AA / BA Gyro-Compass Capable Not ECCN = 7A994 HG4930CA/CB/CS HG4930BA/BB/BS HG4930AA/AB/AS i300 i300 In Production i200 High value MEMS IMU In Production Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. i200 Size (mm) Weight (g) Power (w) Gyro Range °/s Data Rate (Hz) 130 x 150 x 140 3,000 7.5 480 100/600 Size (mm) Weight (g) Power (w) Gyro Range °/s Data Rate (Hz) 65 x 51 x 35.5 140 <2 400 100/600 Size (mm) Weight (g) Power (w) Gyro Range °/s Data Rate (Hz) 42 x 28 x 14 35 0.5 490 300 Size (mm) Weight (g) Power (w) Gyro Range °/s Data Rate (Hz) 42 x 28 x 14 35 0.5 490 300 HOUSED INS/GNSS NAVIGATORS I800 BA IMU HGuide n888/880 Dual RF input as standard RLG IMU Due Q4, 2022 100% Fit*, Form, Function compatible In Development 3-freq GPS, GLONASS, Galileo & Beidou SBAS, PPK, RTK, PPP as standard HG4930 CA IMU HGuide n580 FOG replacement IMU In Production HGuide n380 Honeywell HGSF Navigation software g080 GNSS 16gb onboard storage In Production I300 IMU OEM/unhoused variants available Aiding sources – DMI, DVL Compatible with most LiDAR systems High value MEMS IMU HGuide Post-Processing compatibility In Production In Production Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. Honeywell HGuide g080 GNSS card * n880 has larger footprint 27 HGUIDE O360/N380/N580/N888 INS/GNSS HGUIDE n380/n580/n888 KEY CHARACTERISTICS HGuide o360 HGuide n380 HGuide n580 HGuide n888 Size 7.1cm x 4.5cm x 1.2cm 9cm x 6cm x 4.8cm 9cm x 6cm x 6cm 13cm x 14cm x `5cm Weight <30g 320g 450g <3kg Power Consumptio n 3W 3.5W 7W 7.5W Operating Temperature Range -40C to +85C Supply Voltages Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. 3.3VDC -40C to +71C -40C to +85C +9VDC to +36VDC GNSS Signals Dual RF - GPS, GLONASS, Galileo, Beidou, IRNSS, QZSS and SBAS GNSS Capability SBAS, Post-Processed Kinematic (PPK) and Real-Time Kinematic (RTK) Internal logging Capacity Comms User Supplied using SD Slot 16GB Primary Nav 1MBit, RS-422; Secondary Nav, 1MBit, 5V CMOS; RTCM Corrections, 28 HGUIDE O360/N380/N580/N888 INS/GNSS HGUIDE n380/n580 PERFORMANCE CHARACTERISTICS Position Accuracy Horizontal (m, 1σ) n580 n888 Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. Horizontal (m/s, 1σ) Vertical (m/s, 1σ) 0.025 (RTK) 0.8 (SBAS) o360 n380 Vertical (m, 1σ) Velocity 0.01 with RTK 0.4 with SBAS 0.025 (RTK) 0.4 (SBAS) <0.015 Heading Pitch/Roll (°, 1σ) (°, 1σ) <0.06 <0.015 <0.08 0.03 <0.03 <0.015 TBD TBD <0.01 29 HGUIDE N380/N580/N888 INS/GNSS HGUIDE n380/n580 PERFORMANCE AFTER GNSS OUTAGE Position Accuracy Position Accuracy Heading Horizontal Velocity Vertical Velocity Horizontal (m, 1σ) Vertical (m, 1σ) Static (°, 1σ) (m/s, 1σ) (m/s, 1σ) Outage (s) 3 10 30 60 3 10 30 60 3 10 30 60 3 10 30 60 3 10 30 60 o360 0.08 0.20 1.4 5.0 0.6 0.15 0.45 1.0 0.070 0.085 0.095 0.120 0.015 0.04 0.10 0.20 <0.01 0.02 0.03 0.04 n380* 0.12 0.30 2.5 0.06 0.2 0.75 0.10 0.125 0.15 0.03 0.08 0.16 0.02 0.04 0.06 n580 0.08 0.10 1.0 0.05 0.10 0.30 0.01 0.03 0.04 0.02 0.04 0.06 <0.01 0.01 0.02 3.5 n888 Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved. * N380 outage performance not like-for-like 0.70 0.05 0.15 0.03 THANK YOU Honeywell Confidential - © 2022 by Honeywell International Inc. All rights reserved.
