Motor RM2 is licenčná verzia engineand De Havilland Ghost 50. Licenciu zakúpila spoločnosť Svenska Flygmotor, in ktorej mala väčšinový podiel since 1941 the company Volvo.
Motor RM2 was designed to drive lietadla SAAB J-29 Tunnan. Engine slúžil spoľahlivo except for one nešťastnú udalosť, has ever explored it occurred to nasatiu branca and his an death. To sa that never happens, occurred to modify the marriage nasávania.
Other vývojom formed verzia engineand, marked as RM2A with the chamber prídavného spaľovania, poháňajúca prototype SAAB J-29D Tunnan. Other modifications of a final verzia RM2B. Licenčná production version of RM2 and RM2B prebiehala in rokoch 1952-1955.
Technical information:
Výrobca: Svenska Flygmotor AB (SFA), according to the bible
Type (Type): jednoprúdový (Turbojet)
Dĺžka (Lenght) : 3073 mm (121 in)
Priemer (Diameter): 1346 mm (53 in)
Dry hmotnosť (Dry weight): 1006 kg (2.218 lb)
Part of the engineand (Components):
Compressor (Compressor): single stage odstredivý (Single stage centrifugal flow)
Spaľovacia chamber (Combustors): 10 komôr (10 chambers)
Turbine (Turbine): Single-stage (Single-stage)
Fuel (Fuel type) : kerosene (Kerosene)
Performance (Performance):
Maximálny ťah (Maximum thrust): 22,2 kN pri 10250 rpm (5,000 lbf at 10,250 rpm)
The total kompresný ratio (Overall pressure ratio): 4,6
Merná consumption of fuel (Specific fuel consumption): 0,46 kg/h/N (up to 1.02 lb / hr / lbf)
Source:
www.airpowerworld.info
http://en.wikipedia.org/wiki/De_Havilland_Ghost
www.flightglobal.com.
Motor RM2 was designed to drive lietadla SAAB J-29 Tunnan. Engine slúžil spoľahlivo except for one nešťastnú udalosť, has ever explored it occurred to nasatiu branca and his an death. To sa that never happens, occurred to modify the marriage nasávania.
Other vývojom formed verzia engineand, marked as RM2A with the chamber prídavného spaľovania, poháňajúca prototype SAAB J-29D Tunnan. Other modifications of a final verzia RM2B. Licenčná production version of RM2 and RM2B prebiehala in rokoch 1952-1955.
Technical information:
Výrobca: Svenska Flygmotor AB (SFA), according to the bible
Type (Type): jednoprúdový (Turbojet)
Dĺžka (Lenght) : 3073 mm (121 in)
Priemer (Diameter): 1346 mm (53 in)
Dry hmotnosť (Dry weight): 1006 kg (2.218 lb)
Part of the engineand (Components):
Compressor (Compressor): single stage odstredivý (Single stage centrifugal flow)
Spaľovacia chamber (Combustors): 10 komôr (10 chambers)
Turbine (Turbine): Single-stage (Single-stage)
Fuel (Fuel type) : kerosene (Kerosene)
Performance (Performance):
Maximálny ťah (Maximum thrust): 22,2 kN pri 10250 rpm (5,000 lbf at 10,250 rpm)
The total kompresný ratio (Overall pressure ratio): 4,6
Merná consumption of fuel (Specific fuel consumption): 0,46 kg/h/N (up to 1.02 lb / hr / lbf)
Source:
www.airpowerworld.info
http://en.wikipedia.org/wiki/De_Havilland_Ghost
www.flightglobal.com.
