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Approved for public release; distribution unlimited. Review completed by the AMRDEC Public Affairs Office 15 Nov 2012; FN6125 Technology for the Future of Vertical Lift Presented by: Layne B. Merritt Chief Engineer, Aviation Development Aviation and Missile Research, Development and Engineering Center 22 November 2012 Presented to: Italian Vertical Lift Community

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Page 1: Technology for the Future of Vertical Lift - aofs.org · Technology for the Future of Vertical Lift Presented by: ... OH-58D Kiowa Warrior RQ-7B Shadow RQ-11B ... Size . Scale . Risk

Approved for public release; distribution unlimited. Review completed by the AMRDEC Public Affairs Office 15 Nov 2012; FN6125

Technology for the Future of Vertical Lift

Presented by:

Layne B. Merritt Chief Engineer, Aviation Development

Aviation and Missile Research,

Development and Engineering Center

22 November 2012

Presented to: Italian Vertical Lift Community

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Bottom Line Up Front

• Aviation S&T supports both the current helicopter and future rotorcraft fleets in improving survivability, performance, and affordability

• Current efforts are focused on platforms, power, mission systems, and sustainment

• Future efforts are focused on the Joint Multi-Role (JMR) – Future Vertical Lift Technologies – Unmanned and Autonomous Systems

Army Aviation S&T balances the needs of the current and future fleets

Current Future

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Aviation S&T Supports the Current Fleet and Future Vertical Lift

Compound Rotorcraft

Tiltrotor

Advanced Rotorcraft

UH-60M Black Hawk

OH-58D Kiowa Warrior

RQ-7B Shadow

RQ-11B Raven

MQ-1C Gray Eagle

CH-47F Chinook

AH-64D Apache

MQ-5B Hunter Puma

UH-72A Lakota

Future Vertical Lift

Aircrafts Designed for Future 2025

RC-12

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Why Future Vertical Lift?

CH-47 Basic Design Is 70+ Years Old UH-60 Basic Design Is Nearly 50 Years Old AH-64 Basic Design Is Nearly 50 Years Old OH-58 Basic Design Is Nearly 50 Years Old

They Will Not Last Forever

However…

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Future Vertical Lift (FVL) Rotorcraft Vision

• FVL describes a family of vertical lift aircraft – Includes multiple sizes/classes of vehicles – Considers the vertical lift needs across the

DoD – Achieves significant commonality between

platforms – Addresses the capability gaps identified in

the Army Aviation Operations CBA, and the OSD-sponsored Future Vertical Lift CBA

• Objective vehicle attributes – Scalable common core architecture – Integrated aircraft survivability – Speed 170+ kts – Range 424 km (combat radius) – Performance at 6,000 feet and 95⁰F (“6k/95”) – Shipboard Compatible – Fuel Efficient – Supportable – Affordability – Optionally Manned – Commonality

Light Medium Heavy Ultra

Worldwide operations

Affordability

Performance

Survivability

Sustainability

Environmental

Range Payload

Fuel Efficiency Station Time

Speed

Operational Availability

Operations & Support Costs

Survivability IR/RF/Laser

Kinetic Threat Small Arms

Affordability Size

Scale Risk Future

Aviation Capabilities

6K/95 All Weather Ops in Degraded Visual

Environment

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JMR Technology Demonstrator (TD)

Purpose: • Demonstrate transformational vertical

lift capabilities to prepare the DoD for decisions regarding the replacement of the current vertical lift fleet

Products: • Demonstrated and refined set of

technologically feasible and affordable capabilities

• Technology maturation plans • Cost analysis for future capabilities • Two demonstrator test bed aircraft

Payoff: • Reduced risk for critical technologies • Acquisition workforce with improved

skill sets to develop specifications and analyze technical data

• Data readily available to support future DoD acquisitions

Capability to Perform Worldwide Operations

Affordability

Performance

Survivability

Sustainability

Environmental

Range Payload

Fuel Efficiency Station Time

Speed

Operational Availability

Operations & Support Costs

Survivability IR/RF/Laser

Kinetic Threat Small Arms

Affordability Size

Scale Risk

Future Aviation

Capabilities

6K/95 All Weather Ops in Degraded Visual

Environment

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Special Challenge - DVE

Over the last ten years, DVE conditions are the leading contributor of aviation deaths and loss of aircraft

Degraded Visual Environment

Aircraft Control

Characteristics Symbology &

Cueing

Sensors

•Complex, Multi-disciplinary Problem •Multiple Operating Environments •Potentially Very Expensive

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Incremental Build on Capabilities

FOUNDATION LAYER Improved Flight Controls, Navigation, SVB

Existing Sensors TTPs, Training

Display MFD, HUD, HMD

Symbology BOSS, BFT, Threats

Digital Databases Terrain, Obstacles, Wires

Crew Warning Visual, Aural, Tactile

Passive Sensors Multi-function, all-aspect

capability

Video Enhancement Brownout, wire/obstacle detection

Active Sensor(s) Multi-function - MMW, 3D LADAR

Multi-Ship Collaboration Networking, Digital Interoperability

Overlay Symbology

Fuse WFOV sensor video

Network with other a/c

Terrain/Obstacle/Threats

Fuse active sensor data

“Remove” brownout, detect obstacles

Synthetic Vision (All-weather)

Display NFOV sensor video

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New Focus - Autonomy

Army Unmanned Aircraft Systems, across all tactical echelons supporting Army and Joint operations, provide the Warfighter a disproportionate advantage through:

• Near real-time situational awareness,

• Multi-role capabilities on demand (including communications, reconnaissance, and armed response), and

• System employment from dynamic retasking through autonomous operations.

Focus Areas • Near Term (Now -- 2015)

– Improved Endurance/Range – Precision Engagements – Multi-mission capability – Optionally Piloted Vehicle Concepts – Improved Propulsion Systems

• Mid Term (2016 – 2025) – Increased commonality – Cognitive Aiding Software – Improved Survivability (onboard and swarm ASE) – Lethal/Non-Lethal Payloads – All Weather Capability – Fully Compliant Sense and Avoid

• Far Term (2026 – 2035) – Autonomous Behavior – Swarming and other Teaming Capabilities – Self Healing Network

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Army Aviation S&T Focus Areas

Power (15%) • Increased Fuel Efficiency Engines • Lightweight Drive Trains • Improved Reliability and Durability • Reduced Weight/Vibration • Alternative Concept Engines

• Advanced Air Vehicle System Concepts

• Joint Multi-Role Technology Demonstrator

• Rotorcraft Airframe Technology • Platform Durability and Damage

Tolerance • National Rotorcraft Technology

Center • Reduced Vibrations • Reduced Acoustic Signature • Adaptive Vehicle Management • Improved Vehicle Performance

Platforms (54%)

Operations Support & Sustainment (7%) • Reduced Maintenance Actions • Improved Reliability • Improved Mission Readiness • Reduced Spares Logistics • High Rel Prognostics/Diagnostics

Mission Systems (21%) • DVE Mitigation • Common Human Machine Interface • Increased Levels of Autonomy • Manned-Unmanned Intelligent

Teaming • Reduced Vehicle Signatures • Threat Warning Sensors • Active Jammers & Decoys • Weapons Integration

• Advanced Concept Studies • Configuration Trades & Analysis

Concept Design & Evaluation (3%)

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• AMRDEC maintains several levels of international engagement with various international partners in mutual areas of interest

• Interest Areas

– Engines and Drive Trains – Platform Design and Structures – Rotors and Vehicle Management – Aircraft and Occupant Survivability – Unmanned and Autonomous Systems – Maintainability and Sustainability – Basic Research in Rotorcraft Technologies

International Cooperation

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Questions

Layne B. Merritt Chief Engineer Aviation Development US Army [email protected]