System and method of augmenting power in a rotorcraft
摘要
<p>The present application relates to a regenerative or hybrid drive system (201;301;401;501) for an aircraft (101). The drive system (201;301;401;501)includes the use of a power augmentation device (209;309;409;509) to selectively engage the drive system of an aircraft to store power. The power in the power augmentation device (209;309;409;509) being configured to release a power burst to systems within the aircraft to perform critical flight maneuvers.</p>
