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More electric, advanced hydromechanics propeller control components.

Descrizione del progetto

Potenziamento dei motori a turboelica con nuclei centrali e sistemi di controllo innovativi

Il nucleo centrale ARDIDEN3 è stato originariamente progettato per i motori turboalbero. Il progetto PROPCONEL, finanziato dall’UE, intende adattare e migliorare l’ARDIDEN3 per l’uso nei motori turboelica a corto raggio dell’aviazione d’affari. Questo obiettivo sarà raggiunto riprogettando la camera di combustione, la turbina, lo scarico propulsivo e il sistema di controllo per soddisfare meglio i requisiti delle applicazioni turboelica. Il nucleo centrale sarà integrato con una innovativa scatola di trasmissione, una presa d’aria e un avanzato sistema di controllo dell’elica «più elettrico». Quest’ultimo comprenderà un’unità di controllo dell’elica, un limitatore di velocità e una pompa dell’olio ausiliaria. Dopo aver definito le specifiche di progetto e prodotto i componenti del sistema di controllo, PROPCONEL condurrà dei test rigorosi.

Obiettivo

The project proposal is aimed in category of Business Aviation/Short Range turboprop engines. The baseline core of ARDIDEN3 will be improved with focus, first of all upon combustion chamber for higher altitude operation, specific turbine and propulsive exhaust and specific control system. This way it will better fit with turboprop application. For this purpose the ARDIDEN3 core will be integrated with an innovative gear box, air inlet and advanced more electric propeller control system.
Objective of the project proposal is to research, design, manufacture test and verify a new advanced, more electric propeller control system consisting of Propeller Control Unit, Overspeed Governor and Auxiliary Oil Pump, useful for operational conditions of the improved Turboprop engine developed by Turbomeca.
The objective will be achieved by the following steps:
1. Definition of propeller control system design specifications with respect to the increased level of power influences due to the specific characteristic of the improved Turboprop engine.
2. Design of the Propeller Control Unit, Overspeed Governor and Auxiliary Oil Pump.
3. Production of the Propeller Control System equipment.
4. Testing of the Propeller Control Unit, Overspeed Governor and Auxiliary Oil Pump within internal testing procedures, and validation within environmental external testing and verification directly on the Turboprop engine demonstrator, in order to demonstrate the achievements.
Based on the dynamic modeling, research and verification the new technical specifications will be established. Based on them a suitable, advanced more electric propeller control system will be designed, produced and tested.

JIHOSTROJ is a company experienced and approved for design and production of propeller governors.
VZLU is a research and testing establishment with more than 90 years of experience and tradition in aerospace activities.

Meccanismo di finanziamento

CS2-IA - Innovation action

Coordinatore

JIHOSTROJ AS
Contribution nette de l'UE
€ 245 380,00
Indirizzo
BUDEJOVICKA 148
382 32 VELESIN
Cechia

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Regione
Česko Jihozápad Jihočeský kraj
Tipo di attività
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Collegamenti
Costo totale
€ 350 542,85

Partecipanti (1)