Adjustable template for tapered airfoil rib profiles

Geometrical instruments – Area integrators – Electrical

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Details

33174G, 35 26, B41K 132, G01B 314

Patent

active

040940713

ABSTRACT:
An adjustable template that defines the profiles of ribs of a tapered airfoil, such as an aerodynamic wing, includes two templates which are movable with respect to each other, one for defining the top portion of a rib profile and the other for defining the bottom portion of the rib profile, the two templates being held together in juxtaposition to each other so that the spacing between the two templates in a direction perpendicular to the chord of the rib profile is readily variable and so the successive rib profiles of a given tapered airfoil are defined by the templates by successive adjustments of the position of one template with respect to the other.

REFERENCES:
patent: 2435516 (1948-02-01), Samson
patent: 2702944 (1955-03-01), Lane et al.
patent: 3007247 (1961-11-01), Boehm
patent: 3483628 (1969-12-01), Newman
patent: 3832785 (1974-09-01), Miller

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