Rigging of aircraft wing flaps

Details Rigging of aircraft wing flaps Rigging of aircraft wing flaps

1995-03-08

1996-10-15

Kashnikow, Andres

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244214, 244213, 244117R, 33 1BB, 24418, B64C 916

Patent

active

055646557

ABSTRACT:
Apparatus, method and an arrangement for rigging an aircraft wing flap are provided. The apparatus (27) is for measuring horizontal and vertical positioning of a trailing edge (21) of a wing flap (14, 15) relative to a flap track beam (6) upon which the flap (14, 15) is mount for deployment movement. The flap track beam (6) is affixed to a wing main torsion box (1) behind which the flap (14, 15) is deployable. The apparatus (27) engages the trailing edge (21) of the flap (14, 15) to allow accurate horizontal and vertical positional measurement of the trailing edge.

REFERENCES:
patent: 2665489 (1954-01-01), Cunningham
patent: 5033695 (1991-07-01), Foshee et al.
patent: 5161757 (1995-11-01), Large
patent: 5407153 (1995-04-01), Kirk et al.

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