wingtip
Aerospace
- Jan 29, 2004
- 2
Hi,
This is on a similar subject to my other post today. Some aircraft under development ,e.g. The JSF, are developing a 270V DC power system rather than 115V 400Hz used on previous aircraft. Does anyone have an explanation for this change in power system design...what are the advantages? Could the change be driven mainly by the emergence of powerful DC motors which can replace hydraulic actuators?
This is on a similar subject to my other post today. Some aircraft under development ,e.g. The JSF, are developing a 270V DC power system rather than 115V 400Hz used on previous aircraft. Does anyone have an explanation for this change in power system design...what are the advantages? Could the change be driven mainly by the emergence of powerful DC motors which can replace hydraulic actuators?