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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||416/1 ; 416/33|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 0|
A power management system is disclosed for an advanced helicoptor having both lift and thrust propulsion units and at least one power plant which comprises, a signal generator for generating a first signal which is proportional to the power available from the power plant, a power use gage connected to the lift propulsion unit which has an output that varies according to the amount of power used by that propulsion unit and a circuit which is connected to the power use gage and which receives the first signal for generating a second signal which is proport...
In the operation of a helicopter engine wherein operating conditions change power demands, such as wherein under flight conditions an increase in rotor blade pitch causes a demand for increased engine power, a process for making excess power available for a thrusting device of the helicopter when no such demand for increased power is made, comprising generating a first signal which is proportional to the total amount of engine power available, continuously sensing the amount of engine power utilized under the flight conditions, generating a second signal...