The Saturn/Lyulka AL-34 was an unbuilt turboshaft/turboprop engine for rotary and fixed-wing aircraft, proposed by the Soviet Union in the early 1990s. In turboprop form, the engine was offered for light aircraft such as the Sukhoi Su-86 eight-passenger business airplane, [1] the Myasishchev M-101T Gzhel business jet, [2] the ROS-Aeroprogress T-101 Grach nine-passenger aircraft, [3] its derivative T-108 Zolotoy Orel nineteen-passenger aircraft, [4] and the Krunichev T-511 "AIST-M". [5] As a turboshaft, the AL-34 was proposed to power the Mil Mi-54 [6] and the Kazan Ansat [7] helicopters. The engine was also considered for unconventional aircraft such as the Mil Mi-30L Vintoplan tiltrotor aircraft, [8] and it was to be an auxiliary engine for powering the boundary layer control system and air cushion on the EKIP flying saucer (a flying wing aircraft). [9]
The AL-34 was one of the few engines to use a recuperator to recover and reuse waste heat from combustion. [10]
The engine came in two versions. The AL-34-1 was an engine that produced 550 horsepower (410 kW) in cruise conditions. [2] It weighed 363 pounds (165 kilograms), which included a compact, 88 lb (40 kg) recuperator. The AL-34-2 was a twin-configuration engine producing 1,100 hp (820 kW), weighing about 1,200 lb (540 kg), and using a common gearbox in a single module. [11]
In October 2000, Saturn/Lyulka confirmed that it was still developing the AL-34 engine in the 1,000 to 1,500 hp (750 to 1,120 kW) power range, and it was working with Kawasaki on stationary powerplant applications. [12] The AL-34 would cost 200-240 thousand dollars, and it would require about 22 million dollars to complete development. [13] As late as January 2004, the engine was still being proposed for the T-511 "AIST-M" derivative of the Krunichev T-411 Aist light utility aircraft. [5] However, the AL-34 never entered production.
Data from [10] [2] (for AL-34-1 only)
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