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Flight
tests will resume next week on Honeywell's new AS900 turbofan, with
a second, more comprehensively instrumented engine replacing the
PowerPoint that had racked up four hours in two flights since January
29.
The
first test flight lasted more than two hours with engine testing
at altitudes up to 25,000 feet. Engine power settings as high as
93.6% (26,300 rpm) N2 were achieved during the testing and windmill
data was collected during the descent after a scheduled engine shutdown
at 23,500 feet.
In the
second flight the engine demonstrated full thrust at Mach 0.8 at
41,000 ft, meeting all objectives at that altitude.
The
break in flight-testing gave Honeywell time to push its tested Boeing
720 into the paintshop. As the test engine attracts more attention
(and who could miss a VW minibus-sized protuberance on the side
fuselage of a Boeing?), the powers that be decided it was time for
AlliedSignal's name and livery to be retired from the venerable
workhorse.
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AS900 Flies in Record Time
Asian Aerospace 2000 -- "It's not every day you
get to do something like this," an excited Steve Loranger told
Show News after the successful first flight of Honeywell's new AS900
engine for the Avro RJX and Bombardier Continental business jet. "It's
really something to take a clean sheet of paper, design it the way you
want it, and then fly it!"
The January 29 flight of the AS900 on Honeywell's Boeing 720 testbed marked
a number of major firsts for Honeywell said Loranger, president of engines
and systems at Honeywell:
- The fastest engine development ever at Honeywell (and its predecessor
AlliedSignal), taking only 12 months from initial design to first run,
and another 18 months to first flight. Design to delivery will be 3-1/2
years, paring 12 months off previous programs.
- The first fully integrated propulsion developed by Honeywell, including
engine, nacelle, thrust reversers, control systems and all engine mounted
accessories and plumbing.
- The largest fan propulsion engine built by Honeywell.
- The first test of a new data collection and real-time telemetry system
that will allow measurement of up to 500 parameters on the test engine.
An aggressive development schedule calls for certification in March 2001
after 400 hours of flight test on three engines, and a total of 7,500 hours
running time and 30,000 cycles on the 17 engines in the program. Further
testing will complete the program at 13,000 hours and 50,000 cycles.
Partners with Honeywell in the Integrated Powerplant System (IPPS) include
GKN Westland (nacelle), ITP of Spain and Orenda of Canada (static structural
parts), Tech Span Aero, and AIDC of Taiwan (responsibility for the fan).
The AS900 is a 7,000-pound-thrust-class engine with a 34.2-inch fan and
a bypass ratio of 4.2. The engine is configured with four axial compressor
stages, including two variable-geometry stators, a single centrifugal compressor,
an effusion-cooled combustor, a two-stage high-pressure turbine and a three-stage
low-pressure turbine driving a high-efficiency fan. All discs in the AS900
are designed for a 15,000-cycle life, and the engine will be offered with
an on-condition maintenance program from introduction into service, or,
for those choosing fixed maintenance periods, mature hot section and compressor
zone inspection intervals set at 3,500 hours and 7,000 hours, respectively.
By John Morris
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