|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/75R ; 244/78 ; 91/510 ; 60/911|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 26 인용 특허 : 0|
An emergency supply system for maintaining the emergency flight control of a high-performance aircraft of aerodynamically unstable design having three energy systems, namely, two identical hydraulic systems, connected in parallel for redundancy, for actuation of the control surfaces of the aircraft required for its ability to fly, and an electric on-board system having at least one generator, a rechargeable battery and a non-rechargeable emergency battery, the three energy systems being interconnectible in terms of energy by a power transmission unit, an...
An emergency supply system for maintaining the emergency flight control of a high-performance aircraft of aerodynamically unstable design comprising two substantially identical parallel-connected hydraulic systems for actuating the control surfaces of the aircraft required for flight, the hydraulic systems under normal operating conditions being supplied with energy by two independent hydraulic pumps operatively connected to the propulsion system of the aircraft, each hydraulic system including at least two subsystems operatively connected to at least on...