Flying aid device for a fly-by-wire aircraft

Aeronautics and astronautics – Aircraft control – Pilot operated

Patent

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Details

244220, 244228, 244229, B64C 1304, B64C 1312, B64C 1350

Patent

active

060006625

ABSTRACT:
A flying aid device for a fly-by-wire aircraft which has at least two mechanically independent control columns (M1, M2). The device (1) includes: a system (SO) for detecting multiple control corresponding to simultaneous operation of at least two of the control columns (M1, M2); and informing systems (S1, S2, S3, S4), each of which is associated with one of the control columns (M1, M2) and is intended to generate within the control column (M1, M2), when the detection system (SO) detects multiple control, a tactile sensation that informs a pilot of the aircraft who is operating the control column (M1, M2) of the multiple control.

REFERENCES:
patent: 2566409 (1951-09-01), Greene
patent: 5062594 (1991-11-01), Repperger
patent: 5125602 (1992-06-01), Vauvelle
patent: 5149023 (1992-09-01), Sakurai et al.
patent: 5291113 (1994-03-01), Hegg et al.
patent: 5456428 (1995-10-01), Hegg
patent: 5694014 (1997-12-01), Hegg et al.
Hegg, J.W. et al., Digital Avionics Systems Conference. No. Conf. 13, Oct. 30, 1994 pp. 305 to 308, (Hegg et al.).

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