“Support to Franklin Sp. z o.o. Research and Development Processes for the purpose of testing and implementation of the innovative hybrid air engine Franklin” (Q97844): Difference between revisions
Jump to navigation
Jump to search
(Removed claim: summary (P836): The project focuses on the development of Franklin (R & D) in order to carry out comprehensive tests of innovative aircraft components for placing on the market in the finished product, an engine with reduced unladen mass, reduced consumption of fuel with enhanced reliability as an innovative solution on a global scale. On the newly purchased R & D infrastructure, a firm will carry out R & D work in the following areas: 1- Testing of dynamic o...) |
(Created claim: summary (P836): The subject of the project is the development of Franklin’s R & D facilities in order to carry out comprehensive research on innovative components of an aircraft engine aimed at placing a finished product on the market – an engine with a reduced unladen weight, reduced fuel consumption with increased reliability as an innovative solution in the world. On the newly purchased R & D infrastructure, the company will carry out R & D activities in the...) |
||||||||||||||
| Property / summary | |||||||||||||||
The subject of the project is the development of Franklin’s R & D facilities in order to carry out comprehensive research on innovative components of an aircraft engine aimed at placing a finished product on the market – an engine with a reduced unladen weight, reduced fuel consumption with increased reliability as an innovative solution in the world. On the newly purchased R & D infrastructure, the company will carry out R & D activities in the following areas:1- the dynamic performance of the aeronautical piston engine associated with the microhybrid magneto-electric unit, with particular emphasis on torque testing in angular distribution using a magnetoelectric unit.2- fuel consumption test using a modern control system for regulatory parameters. 3- exhaust composition test in conjunction with the control system.4- flight test on an experimental aeroplane. The investment consists of equipping R & D facilities with the following equipment: Cessna 172-4 local aircraft, crankshaft torsion test device, engine external vibration test device, fuel flow and consumption measurement kit, dynamic position for testing of magneto-electric assembly, magneto-electric unit, magneto-electric unit controller, aeronautical accumulators AH 12V – 300 AH. — 10 pcs, commissioning the design and execution of a set of aluminum castings of the magneto-electric assembly assembly on the engine, designing and execution of an electronic engine control system – FADEC, the aeroplane’s equipment with a fuel consumption measurement system, flight parameters control system and a system of torsion vibration measurement during flight.The entire range is necessary to expand the background of the bad.-development of the company Wnioskod., necessary to guide B. (English) | |||||||||||||||
| Property / summary: The subject of the project is the development of Franklin’s R & D facilities in order to carry out comprehensive research on innovative components of an aircraft engine aimed at placing a finished product on the market – an engine with a reduced unladen weight, reduced fuel consumption with increased reliability as an innovative solution in the world. On the newly purchased R & D infrastructure, the company will carry out R & D activities in the following areas:1- the dynamic performance of the aeronautical piston engine associated with the microhybrid magneto-electric unit, with particular emphasis on torque testing in angular distribution using a magnetoelectric unit.2- fuel consumption test using a modern control system for regulatory parameters. 3- exhaust composition test in conjunction with the control system.4- flight test on an experimental aeroplane. The investment consists of equipping R & D facilities with the following equipment: Cessna 172-4 local aircraft, crankshaft torsion test device, engine external vibration test device, fuel flow and consumption measurement kit, dynamic position for testing of magneto-electric assembly, magneto-electric unit, magneto-electric unit controller, aeronautical accumulators AH 12V – 300 AH. — 10 pcs, commissioning the design and execution of a set of aluminum castings of the magneto-electric assembly assembly on the engine, designing and execution of an electronic engine control system – FADEC, the aeroplane’s equipment with a fuel consumption measurement system, flight parameters control system and a system of torsion vibration measurement during flight.The entire range is necessary to expand the background of the bad.-development of the company Wnioskod., necessary to guide B. (English) / rank | |||||||||||||||
Normal rank | |||||||||||||||
| Property / summary: The subject of the project is the development of Franklin’s R & D facilities in order to carry out comprehensive research on innovative components of an aircraft engine aimed at placing a finished product on the market – an engine with a reduced unladen weight, reduced fuel consumption with increased reliability as an innovative solution in the world. On the newly purchased R & D infrastructure, the company will carry out R & D activities in the following areas:1- the dynamic performance of the aeronautical piston engine associated with the microhybrid magneto-electric unit, with particular emphasis on torque testing in angular distribution using a magnetoelectric unit.2- fuel consumption test using a modern control system for regulatory parameters. 3- exhaust composition test in conjunction with the control system.4- flight test on an experimental aeroplane. The investment consists of equipping R & D facilities with the following equipment: Cessna 172-4 local aircraft, crankshaft torsion test device, engine external vibration test device, fuel flow and consumption measurement kit, dynamic position for testing of magneto-electric assembly, magneto-electric unit, magneto-electric unit controller, aeronautical accumulators AH 12V – 300 AH. — 10 pcs, commissioning the design and execution of a set of aluminum castings of the magneto-electric assembly assembly on the engine, designing and execution of an electronic engine control system – FADEC, the aeroplane’s equipment with a fuel consumption measurement system, flight parameters control system and a system of torsion vibration measurement during flight.The entire range is necessary to expand the background of the bad.-development of the company Wnioskod., necessary to guide B. (English) / qualifier | |||||||||||||||
point in time: 15 October 2020
| |||||||||||||||
Revision as of 22:08, 15 October 2020
Project in Poland financed by DG Regio
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | “Support to Franklin Sp. z o.o. Research and Development Processes for the purpose of testing and implementation of the innovative hybrid air engine Franklin” |
Project in Poland financed by DG Regio |
Statements
1,341,450.0 zloty
0 references
2,439,000.0 zloty
0 references
55.0 percent
0 references
1 September 2017
0 references
30 June 2019
0 references
FRANKLIN SP. Z O.O.
0 references
Przedmiotem projektu jest rozwój zaplecza B+R firmy Franklin w celu wykonania kompleksowych badań innowacyjnych modułów składowych silnika lotniczego zmierzających do wprowadzenia na rynek gotowego produktu - silnika o zmniejszonej masie własnej, zmniejszonym zużyciu paliwa o zwiększonej niezawodności stanowiącego rozwiązanie nowatorskie w skali światowej. Na nowo zakupionej infrastrukturze B+R firma prowadzić będzie prace B+R w następujących obszarach:1- badanie dynamicznych wielkości pracy lotniczego silnika tłokowego powiązanego z zespołem magneto-elektrycznym w mikrohybrydę, ze szczególnym naciskiem na badania momentów obrotowych w rozkładzie kątowym z zastosowaniem zespołu magnetoelektrycznego.2- badanie zużycia paliwa przy zastosowaniu nowoczesnego systemu sterowania parametrami regulacyjnymi. 3- badanie składu spalin w powiązaniu z systemem sterowania.4- badania w locie na samolocie eksperymentalnym. Inwestycja polega na wyposażeniu zaplecza B+R o następującą aparaturę: Samolot uźywany Cessna 172 - 4 miejscowy, urządzenie do badania drgań skrętnych wału korbowego, urządzenie do badań wibracji zewnętrznych silnika, zestaw do pomiaru przepływu paliwa oraz zużycia, Stanowisko dynamiczne do badań zespołu magneto-elektrycznego, zespołu magneto-elektrycznego, sterownika zespołu magneto-elektrycznego, akumulatorów lotniczych AH 12V – 300 AH. – 10 szt , zlecenie wykonania zaprojektowania i wykonania kompletu odlewów aluminiowych elementów montaźowych zespołu magneto-elektrycznego na silniku, zaprojektowania i wykonania systemu sterowania elektronicznego pracą silnika – Fadec , wyposażenie samolotu o system pomiarowy zużycia paliwa, system kontroli parametrów lotu i system pomiaru drgań skrętnych podczas lotu.Całość ww. zakresu jest niezb. aby rozbudować zaplecze bad.-rozw. firmy Wnioskod., niezbędne do prowadz. prac B+R. (Polish)
0 references
The subject of the project is the development of Franklin’s R & D facilities in order to carry out comprehensive research on innovative components of an aircraft engine aimed at placing a finished product on the market – an engine with a reduced unladen weight, reduced fuel consumption with increased reliability as an innovative solution in the world. On the newly purchased R & D infrastructure, the company will carry out R & D activities in the following areas:1- the dynamic performance of the aeronautical piston engine associated with the microhybrid magneto-electric unit, with particular emphasis on torque testing in angular distribution using a magnetoelectric unit.2- fuel consumption test using a modern control system for regulatory parameters. 3- exhaust composition test in conjunction with the control system.4- flight test on an experimental aeroplane. The investment consists of equipping R & D facilities with the following equipment: Cessna 172-4 local aircraft, crankshaft torsion test device, engine external vibration test device, fuel flow and consumption measurement kit, dynamic position for testing of magneto-electric assembly, magneto-electric unit, magneto-electric unit controller, aeronautical accumulators AH 12V – 300 AH. — 10 pcs, commissioning the design and execution of a set of aluminum castings of the magneto-electric assembly assembly on the engine, designing and execution of an electronic engine control system – FADEC, the aeroplane’s equipment with a fuel consumption measurement system, flight parameters control system and a system of torsion vibration measurement during flight.The entire range is necessary to expand the background of the bad.-development of the company Wnioskod., necessary to guide B. (English)
15 October 2020
0 references
Identifiers
RPKP.01.02.01-04-0015/17
0 references