Second Core Tests Completed for Russian Superjet Engine

Rostec United Engine Corporation’s tests of the second prototype PD-8 engine core confirmed correct operation of components, required temperature and pressure parameters, and compliance with environmental standards By DA Staff / 20 Oct 2021
Rostec PD-8 Engine Core
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Rostec United Engine Corporation has successfully finished testing the core of a second prototype PD-8 engine core, designed for use on its SSJ-NEW aircraft. 

The tests confirmed correct operation of components, required temperature and pressure parameters, and compliance with environmental standards. The next stage of the project is scheduled for the beginning of the next year, and will involve bench tests of the first prototype engine. 

The engine core consists of a high-pressure compressor, a combustion chamber and a high-pressure turbine that drives the propulsion system. Testing of engine cores will continue along with the PD-8 prototype assembly. 

During the launches, the joint operation of the engine core assemblies was evaluated on the test bench, measuring temperature and pressure, as well as the emission of harmful substances and smoke. Results confirmed the correctness of the solutions used in the propulsion system hot section. 

“The development of the PD-8 is carried out by the method of parallel development of the hot section of the engine and compressor, which allows the project to be implemented in less time,” said First Deputy CEO of Rostec State Corporation, Vladimir Artyakov. 

“Rostec State Corporation has already completed tests of the second prototype engine core, which were successful and confirmed the adequacy of the technology used. Now, the assembling stage of the PD-8 prototypes has begun, with bench tests scheduled for early 2022.” 

“Confirmation of design solutions at the stage of engine core tests is important for the entire course of certification work on the PD-8 engine,” said Yury Shmotin, Deputy General Director – Chief Designer of UEC. 

“The plan is to test the engine core on the Central Institute of Aviation Motors (CIAM) altitude test rig under conditions close to actual operation. At the same time, the compressor will be tested as part of an autonomous unit at CIAM for examination and confirmation of the inherent characteristics.”

As of today, the technical design stage of work on the propulsion system has been completed, working design documentation has been released, and prototypes of the engine are being manufactured. Obtaining a type certificate for the PD-8 is scheduled for 2023. 

Posted by DA Staff Connect & Contact

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