2010.06.03
北京
航空发动机
(TRENT
1000)
与发动机有不解之缘。在与几百台船用发动机实际打过彻头彻尾的技术交道后,
发动机的每一个部件连同它们的作用深深地刻印在脑海中了, 若同入木三分。
在美国波音航空公司的宣传网点,一下子看中了由ROLLS-ROYCE公司设计与制造的最新款航空发动机
TRENT1000,便有些爱不释手了。航空发动机与船用发动机在外型、结构和原理等多方面几乎完全不同。但爱屋及乌,对有形有质的物的眷念之情在内心深处油然而生。感觉眼泪都快要夺眶而出了。赶紧移情它物,顺着眼前看到的发动机样体,做了一番若即若离的跟踪。。。。。。
结构(以TRENT900代替)
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LPT
IPT HPT
IPC FAN
LPT
IPT
HPT
IPC
FAN
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技术
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优势
World-Class fuel
performance
At entry into service (EIS) of the Boeing 787, the Trent 1000 will
be the most efficient engine for the aircraft, delivering the
lowest fuel consumption. Engine testing has already demonstrated
this level of performance. Our development programme has run an
engine over 15% better than the performance of our first Trent,
Trent 700 when it first entered service. This is equivalent to a
fuel saving of $2.3m per aircraft per year.
The Trent three-shaft retention has been demonstrated as
world-class through in service operation. With its titanium wide
chord fan, short, well-supported rotors, this design can save up to
1% in fuel burn. This is equivalent to a fuel
saving of $155,000 per aircraft per year.
As part of the Trent family, the Trent 1000 benefits from the
flow of technology from later members of the family, such as the
Trent XWB. Planned technology development will flow into the Trent
1000, delivering a further 1.5% reduction in new engine fuel
consumption by 2015, delivering a further saving of $230,000 per
aircraft per year.
Industry leading environmental
credentials
The Trent 1000 is the quietest engine for the Boeing 787 and is the
only engine that will achieve London airports QC1 departures and
QC0.5 arrivals noise bands across all 787 aircraft variants.
The engine has been designed for low emissions and achieves over
40% margin to CAEP6 emissions legislation. Our fuel efficiency also
contributes to the aircraft target of delivering 20% lower CO2 than
the previous generation aircraft it replaces.
Delivering greatest availability and lowest burden
through design for service
The Trent 1000 has been designed for ease of maintenance with
accessories mounted on the fan case and has borescope ports
positioned regularly and at eye level. This allows the Trent 1000
to require 50% lower scheduled line maintenance than its
competitor.
Advances in Engine Health Monitoring data capture and analysis, and
dedicated health monitoring sensors throughout the engine ensure
the Trent 1000 has 20% more predictive monitoring system capability
than previous engines.
Advanced technology and designs such as the low speed swept
titanium fan blade and heated engine stator sections reduce foreign
object and ice ingress into the engine. This removes a cause of
maintenance burden and increasing engine availability.
Operational and Financial confidence
The Trent 1000 will be the most mature and robust engine for the
Boeing 787 from EIS having already accumulated over 6,000 hours and
12,000 cycles development engine running. Through powering four of
the flight test aircraft the Trent 1000 will also build up more
flight test experience prior to service.
The Trent 1000 is supported through Rolls-Royce services, providing
financial confidence and peace of mind.
Rolls-Royce delivers on its commitments. In 2004 when the Trent
1000 was first selected to power the Boeing 787 a number of
programme objectives were set. A clear date for first engine run
was established; a 74,000lb capable engine certification date was
set and maturity and performance goals were identified. We are
proud to have achieved all our targets on time and will continue to
achieve the targets that we have set ourselves moving forward.
前景
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开发
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Programme
milestones
The Trent 1000 development programme has been condensed to achieve
more development milestones in a shorter period of time than any
other Trent engine. The Trent 1000 has already
achieved twice as many engine cycles than the Trent 900 at first
flight.
The Trent 1000 has completed the high-cyclic Extended Range Twin
Operations (ETOPS) testing required in order to ensure that the
engine is ready to support customers operations at extended range
with greater flexibility.
Customer
selection
-- Engine downselect
In April 2004, after an intense period of technical reviews, Boeing
selected the Trent 1000 to power the Boeing 787 Dreamliner.
-- Engine on decision
Air
New Zealand was the first 787 customer to make an engine
selection. This placed the Trent 1000 as the
launch engine for the 787-9 variant of the aircraft.
-- First engine delivery
The first set of Trent 1000 engines, from
Rolls-Royce were despatched 4th June
2007.
-- Engine certification
The engine has been certified for thrusts up to
74,000lbs to cover the full Boeing 787 Dreamliner family.
Design and
manufacture
-- Preliminary concept defined
The first part of a stringent review to ensure that we are able to
offer a solution that will fulfil the market opportunities and
customer requirements that can be fully supported with the right
technology.
--
Full concept defined
The preliminary concept is refined with more detail to fully meet
all the design requirments of the Boeing 787 Dreamliner, with the
right supply chain support.
--
First engine run
Testing and
certification
-- Bird strike testing
As part of the essential safety testing of the engine, the
simulated bird strike testing whilst demonstrating resistance to
significant damage and acceptable power loss. The
engine completed two tests fired into the fan at aircraft take-off
speeds: the multiple medium size of 1.1kg bird; and single large
bird 2.5kg bird.
-- Engine fan blade off testing
The Fan
blade off test simulates the extremely unlikely event of a blade
failing in service and is part of the madatory safety
testing. Conditions simulate a fan blade failing
at full take-off speed. The engine must
demonstrate a number of key criteria as well as containing the
blade within the fancase structure. The extreme
conditions involve containment energy equivalent to dropping a 1
ton car off a 200ft cliff.
--Arnold Engineering Development Center (AEDC) testing
The altitude
testing was completed in a purpose built facility in Tulahoma,
Tennessee that reporoduces atmospheric conditions from sea-level to
over 40,000ft. The engine successfully
demonstrated its capability over the full flight envelope.
-- 747
flying test bed
A converted
Boeing 747 was used as a flying testbed for the first time on 19
June 2007, as part of the Trent 1000 development
programme. The flight testing validated aircraft
interfaces and cerified performance of the nacelle.
--Extended Twin OPerations (ETOPs) testing
ETOPs
testing began 12 June 2008 to complete the required 3,000
cycles. The testing simulates the most arduous
service conditions including 3 simulated cycles that represent a
single engine diversion of up to 330 minutes.
--
Stennis Noise testing
Noise
testing was completed and proved that the noise profile of the
engine was within the expected margins.
--
150 hour endurance test
The 150 hour
endurance test is one of the most important of any engine
development programme. As well as defining operational temperature
and speed limits, it also gives a good indication of the durability
and capability of an engine. The development engine was laid out
for inspection by the certifying authority and customers.
Building maturity
--
Maintainability demonstration
In September
07 a number of customers and teams from Boeing came to the
Rolls-Royce training facility in Derby to take part in the Trent
1000 familiarisation course and to verify the maintainability of
the engine. The lessons learnt were used to make
improvements in the accessibility of components.
--
Service leader maturity (KHI)
The first phase of the service
leader testing was completed in November 2008 at the Kawasaki Heavy
Industries(KHI) facility. The engine was stripped
and laid out to identify lessons and share with customers.
-- ETOPS
testing completion.
This testing
simulates approximates 2 years continuous service demonstrating
reliability levels for the airworthiness authorities with over 3000
cycles and 950 hours.
The
testing was completed with maximum levels of rotor unbalance to
imitate worse case conditions at five different thrust
ratings. In addition 3 simulated diversion
cycles, each with 330 minutes at maximum continuous thrust
levels.
模拟
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