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International
Aviation & Space Salon
August 19-24, 2003, FRI named after M.M.Gromov, Zhukovsky, Russia
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SALUT'S ENGINES

D-436T1/T2 aircraft by-pass tur bojet engine

The D-436T1/T2 engine is intended to power shorthaul and medium-haul airliners TU-134M, TU-334-100, TU-334-200, TU-230 and other aircraft. The D-436T1/T2 engine is a new more powerful and efficient modification of the D-36 engine, that has been developed with regard to the international requirements for this class of engines. D-436T1/T2 Engine Design Features: high bypass ratio, three-shaft layout with few bearings, modular construction, thrust reverser, electronic and hydromechanical engine con- trol system, versatile engine mount. Main Advantages Offered by D-436T1/T2 Engine: low specific fuel consumption and low specific mass, high reliability and ease of maintenance, low levels of emissions and noise, high efficiency of engine monitoring and diagnostic system. A vast assimilation of design features of the D-36 basic engine that enjoys a long proven track record of about 5 million flight hours accumulated from extensive service on JK-42, An-72 and An-74 aircraft, guarantees reliable and durable performance of the D- 436T1/T2 engine. The versatile mount makes it possible to use the engine in different aircraft without changing the engine design and arranging the engine under/over the wing, inside the fuselage or at both sides of the fuselage.

Experimental and design gas dynamic studies made on the D-436T1 engine have shown a 3-% fuel efficiency growth potential, using the same core. Thus, the specific fuel consumption at the maximum cruise condition will be 0.592 kg/kgf *h.

BASIC SPECIFICATIONS D-436T1/D-436T2
Take off power:
(SL, static, Tamb = 30 `C, Pamb = 760 mm Hg)
Thrust,kgf .......................7500/8200
Specific fuel consumption, kg/kgf* h . .0,370/0,376
Inlet gas temperature, й ............ .1470/1525
Maximum cruise power:
(H = 11000m, flight Mach number = 0.75, SA)v Thrust, kgf ...................... .1500/1600
Specific fuel consumption, kg/kgf*h . . .0,608/0,617
Bypass ratio ...................... .4,91/4,97
Pressure ratio ......................22,7/26,1
Fan diameter, mm ..................1360/1360
Dry mass, kg .................... . .1450/1450


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MMPP "SALUT"
- is the first in Russia to master the serial production of aircraft engines.

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