Ingenieria en aeronautica
Páginas: 2 (434 palabras)
Publicado: 19 de marzo de 2012
M250 turboprop
Powering the world’s light aircraft
M250 turboprop
Powering the world’s light aircraft
The M250-B17 turboprop engine series represents the latest refinement of a rugged andhighly reliable small turboprop engine. As a part of the M250® family, the first M250-B15 turboprop has grown with the core engine into a family of highly successful engines for light fixed-wingaircraft, culminating in today’s 450shp M250-B17.
● Low direct operating cost ● Single and twin engine applications ● Simplified, compact construction ● Excellent power-to-weight ratio ● Multi-fuelcapability ● Factory authorised support network
Power 450shp
Width 19.4in
Length 45in
Weight 212lb
Certification 1971
simply delivers more
The M250 turboprop is popular due to itssmall size and high power-to-weight ratio, which make it ideal for Original Equipment Manufacture Type Certified (OEMTC) designs and for Supplemental Type Certificate (STC) conversions of existingpiston-engined designs. Over 1,400 M250 turboprops are flying, with over five million flight hours. This lightweight, high-powered engine operates on all certified aircraft fuels, a feature favoured byoperators taking them into remote regions of the world.
The M250 turboprop enjoys the benefits from a continuous improvement culture which has seen the M250 remain at the forefront of small gasturbine engine design. The M250-B17 has a factory authorised global support network of overhaul, maintenance, service centres and spare parts.
EIS 1971
Performance
Sea level static rating Deliveredshaft horsepower
B17C B17F, F/C, F/2
Measured gas temperature (° C)
B17C B17F, F/C, F/2
Sfc lb/shp-hr (max)
B17C B17F, F/C, F/2
Take-o * Normal cruise Cruise A (90%) Cruise B (75%)
450380 377 314
420 369 332 277
810 752
810 738
0.613 0.657 0.635 0.656 0.637 0.670 0.673 0.715
*Measured gas temperature for takeo up to 810°is permitted provided maximum torque is not...
Powering the world’s light aircraft
M250 turboprop
Powering the world’s light aircraft
The M250-B17 turboprop engine series represents the latest refinement of a rugged andhighly reliable small turboprop engine. As a part of the M250® family, the first M250-B15 turboprop has grown with the core engine into a family of highly successful engines for light fixed-wingaircraft, culminating in today’s 450shp M250-B17.
● Low direct operating cost ● Single and twin engine applications ● Simplified, compact construction ● Excellent power-to-weight ratio ● Multi-fuelcapability ● Factory authorised support network
Power 450shp
Width 19.4in
Length 45in
Weight 212lb
Certification 1971
simply delivers more
The M250 turboprop is popular due to itssmall size and high power-to-weight ratio, which make it ideal for Original Equipment Manufacture Type Certified (OEMTC) designs and for Supplemental Type Certificate (STC) conversions of existingpiston-engined designs. Over 1,400 M250 turboprops are flying, with over five million flight hours. This lightweight, high-powered engine operates on all certified aircraft fuels, a feature favoured byoperators taking them into remote regions of the world.
The M250 turboprop enjoys the benefits from a continuous improvement culture which has seen the M250 remain at the forefront of small gasturbine engine design. The M250-B17 has a factory authorised global support network of overhaul, maintenance, service centres and spare parts.
EIS 1971
Performance
Sea level static rating Deliveredshaft horsepower
B17C B17F, F/C, F/2
Measured gas temperature (° C)
B17C B17F, F/C, F/2
Sfc lb/shp-hr (max)
B17C B17F, F/C, F/2
Take-o * Normal cruise Cruise A (90%) Cruise B (75%)
450380 377 314
420 369 332 277
810 752
810 738
0.613 0.657 0.635 0.656 0.637 0.670 0.673 0.715
*Measured gas temperature for takeo up to 810°is permitted provided maximum torque is not...
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