APPENDIX 1 TO ANNEX B
Demonstrator proposals for discussions
with government
1. COMMUNICATIONS
UAV
There is a potential market for low, medium,
or high altitude (and low, medium or high endurance) UAVs to create
a communications relay network as an alternative to military and
commercial satellite communications Network.
Applications: FOAS, civil communications.
2. HIGH PERFORMANCE
UAV
There are many potential military uses for UAVs
in the Deep Strike role. These could be used for a range of C4ISTAR
roles (especially ISTAR) as well as combat roles (SEAD and Strike).
The likely technologies would encompass sensors and sensor fusion
as well as survivable vehicle technologies (ranging from high
speed Cruise Missile-type vehicles to stealthy vehicles).
Applications: FOAS.
3. POWERED WING
Next generation civil wing technologies (wind
design & manufacture, power plant and wing systems) integrated
into an overall optimum wing demonstration.
Applications: Next generation civil aircraft.
4. ADVANCED COMPOSITE
DEMONSTRATOR
Demonstration of an advanced design, manufacture,
assemble and maintain capability for primary composite wing structures.
Applications: Next generation civil aircraft.
5. ADVANCED METALLIC
DEMONSTRATOR
Demonstration of an advanced design, manufacture,
assemble and maintain capability for next generation metallic
systems.
Applications: Next generation civil aircraft.
6. AIR TRAFFIC
MANAGEMENT
A ground based demonstrator should be considered,
which includes simulation of an Air Traffic Control environment
operating with a static Flight Simulator. It could well be that
the system operates this synthetic environment using a number
of distributed simulators or control sites. Such a simulation
capability would address issues of the new ATM system, communications,
taxiway guidance, enhanced and synthetic vision and "free
flight" to a much greater capability than an aircraft could
do. In terms of dual use, the demonstrator would explore the requirement
for the operation of military aircraft and UAVs within the civil
ATM structure. Most of the UK avionics companies, airlines and
airport authorities would gain value for such a system.
Applications: Civil and Military Air Traffic
Management Systems.
7. MORE ELECTRIC
AIRCRAFT DEMONSTRATORS
The More Electric Aircraft represents the optimisation
of current hydraulic, electrical and hydraulic power systems from
a top-down, whole aircraft approach, and concludes that electricity
should be the primary power source. This technology is applicable
to a wide range of platforms, including civil passenger aircraft,
helicopters and unmanned aerial vehicles. However, a number of
key system, product, component, material and process technologies
need to be demonstrated, to achieve the ultimate benefits in efficiency,
weight, safety and maintenance. To progress the evolution of the
More Electric Aircraft, sub-system and component demonstrators
are also required to confirm the benefits and reliability. The
electric motors/generators, and associated power electronics,
need to achieve a higher power density and to survive harsh environments.
Novel topologies of electromagnetic machines need to evolve from
concepts into demonstrators, in conjunction with advances in materials
and manufacturing processes.
The DTI is already sponsoring the development
of electric actuation to replace the hydraulic actuation system
for control of flying surfaces. The main driver is to reduce the
very high maintenance costs and hence lifecycle costs of hydraulics.
Projects such as HEAT, REACTS and TIME address aspects of the
work, but do not take the concepts to a full flight simulation,
unlike our US and EU associates. This could be extended to fly
a hybrid or fully electric military aircraft. A military aircraft
would be desirablenot just because of dual use, but because
it does not need the certification of the civil aircraft. Such
flight demonstration provides both significant technical risk
reduction, and superior credibility when marketing new products.
Applications: Civil and Military Aircraft,
including helicopters and UAVs.
8. SMART EQUIPMENT
DEMONSTRATORS
Technologies such as the More Electric Aircraft
introduce equipment with integrated computing power. This information
processing capability could be utilised to significantly improve
safety and availability. Detection and isolation of faults would
be more effective, by locally monitoring the condition of critical
equipment. This capability would evolve into the prediction of
the remaining life for all the key systems and equipment on an
aircraft. This information could then be integrated into the spares
supply-chain and maintenance system, thereby reducing operating
costs. Demonstration at equipment and system levels required to
advance this technology.
Applications: Civil and Military Aircraft,
including UAVs.
9. AIR PLATFORM
PRECISION ENGAGEMENT
Modelling and demonstration of full "sensor
to shooter" systems, including on and off board sensors,
for a variety of platforms and network systems.
Applications: Eurofighter/Typhoon air to
ground and future platforms.
10. ADVANCED
ENGINEERING PROCESS
DEMONSTRATORS
The majority of today's engineering development
processes depend upon prototypes to demonstrate performance and
integrity. This represents significant investment in time, resources
and money. By integrating design rules with Computer Aided Design
(CAD) tools, system requirements could be automatically processed
and a compliant design generated within hours rather than weeks
or months. Successful demonstration of this "digital product"
concept will enable a significant reduction in time to market,
and ensure "right first time" design. The digital product
could then evolve into a "virtual test" capability,
whereby validation and certification testing, peculiar to the
aerospace industry, may be modelled before hardware is produced.
Demonstration will be key in proving such capabilities, but the
potential benefit of more than a 50 per cent reduction in product
introduction lead time would contribute to making UK industry
more competitive.
Applications: Civil and military design and
proving process.
11. C41/ISTAR ARCHITECTURE/INFRASTRUCTURE
There are a range of potential demonstrations,
which are required to demonstrate integration and interoperability
of C41 and ISTAR in a UK or coalition environment.
12. INFORMATION
SYSTEMS OF
SYSTEMS ARCHITECTURES
A synthetic environment demonstrator to evaluate
trade-offs between investment in various domain C41STAR assets.
Applications: Military requirements.
13. DISTRIBUTED
NETWORK OF
COMMUNICATION ASSETS
To predict, explore and demonstrate how flexible
communications systems can perform and inter-operate, giving the
UK a lead in the provision of infrastructure for international
operations. Demonstrate the application of security and protection
measures.
Applications: Military, civil and emergency
operations.
14. NEXT GENERATION
LARGE CIVIL
ENGINE
The ability to offer reliable service entry
for a complete powerplant demands whole-engine technology validation
prior to inclusion in a final product. This demonstrator programme
allows for this and is centred on core turbomachinery validation
in a fully integrated engine environment. Developments in the
engine core to minimise environmental impact and life cycle costs
will continue with core turbomachinery running at increased temperatures
and pressures and with increased emphasis on active control systems
and variable geometry aerodynamics. Planned developments in these
latter fields will allow simplification of the overall engine
architecture with consequent additional benefits in weight, efficiency
and unit cost.
Applications: Large Civil Aircraft.
15. MORE ELECTRIC
ENGINE
It is planned to run a first generation "More
Electric Engine" in 2004-05. This will incorporate electrically
driven accessories and electrical generators embedded within the
core of the engine. The further development of this technology
and the validation of a flight viable system requires a major
investment in both an underpinning technology programme and in
the development of an integrated approach to the engine and airframe
power systems requirements and architectures. The More Electric
Engine/Aircraft is critical to achieving long-term industry goals
for improved safety/reliability and reduced operating costs.
The More Electric Engine and the Next Generation
Large Civil Engine programme will increasingly become integrated
into a single vehicle as the technology matures and marketable
product become available. However the electric technologies within
the engine are likely to become of such criticality to the engine
operation and performance that a "More Electric Demonstration
Unit" will be required long-term. This is envisaged as being
a similar arrangement to industry's High Temperature Demonstration
Unit programme, which, with the support of HMG, has operated as
an ongoing demonstration vehicle to validate critical core engine
technology developments.
Applications: Large Civil Aircraft.
16. HIGH TEMPERATURE
DEMONSTRATOR UNIT
This vehicle provides a validation route for
core engine technologiesprimarily low emissions combustor
technology and high efficiency turbines where the emphasis is
on reduced cooling. Both of these elements require an underpinning
technology acquisition programme covering Materials, Heat Transfer,
Aerodynamics and Combustion chemistry. All of these programmes
will benefit civil and military applications, but it must be emphasised
that whereas the drive for new technology in these areas has traditionally
come from the military sector, technology development is now increasingly
driven by the needs of the civil sector with subsequent spin-out
to military applications.
Application: Civil and Military Aircraft.
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