Emergency supply system for an aircraft control system

Details Emergency supply system for an aircraft control system Emergency supply system for an aircraft control system

1986-08-20

1988-07-05

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft control

244 78, 91510, 60911, B64C 1342

Patent

active

047549408

ABSTRACT:
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, and wherein the two hydraulic systems are divided into subsystems associated with single or several rudder functions which, if necessary, can be disconnected singly.

REFERENCES:
patent: 2616264 (1952-11-01), Grant et al.
patent: 2619304 (1952-11-01), Feeny et al.
patent: 2977071 (1961-03-01), Plotkowiak et al.
patent: 3315085 (1967-04-01), Mileti et al.
patent: 3877346 (1975-04-01), Koopmann et al.
Oelhydraulik und Pneumatik 10 (1966), No. 1, pp. 10-14.

Affiliated with

Also associated with

Rating

Emergency supply system for an aircraft control system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Emergency supply system for an aircraft control system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Emergency supply system for an aircraft control system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2328042