Aircraft DC starter-generator torque controller

Electricity: motive power systems – Limitation of motor load – current – torque or force

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

318432, H02P 700

Patent

active

050516701

ABSTRACT:
A source of terminal voltage is connected to the armature current input terminal of a DC shunt motor whereby armature current is supplied to the armature. A monitor monitors the terminal voltage and armature current in a determined manner and varies the shunt field current in a manner whereby the air gap flux density of the motor is varied to control the torque of the motor drive shaft.

REFERENCES:
patent: 3749991 (1973-07-01), Kuniyoshi
patent: 3845372 (1974-10-01), Ringland et al.
patent: 3962612 (1976-06-01), Kawasaki
patent: 4060753 (1977-11-01), Okuyama et al.
patent: 4103211 (1978-07-01), Gardner et al.
patent: 4217529 (1980-08-01), Bourke et al.
patent: 4300081 (1981-11-01), Van Landingham

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Aircraft DC starter-generator torque controller does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft DC starter-generator torque controller, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft DC starter-generator torque controller will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1699145

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.