Tool for selectively bending the trailing edge tab of a helicopt

Metal deforming – With indication of condition or position of work – product,... – Work drawn or extruded through die

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72298, 72311, 72319, 298896, B21C 5100, B21D 700, B21D 5392

Patent

active

051116766

ABSTRACT:
A tool mountable on a helicopter blade for selectively bending the trailing edge trim tab of the blade about a selected axis along the span of the trim tab, and including a device to counterbalance the weight of the trim tab bending mechanism so that the true degree of bending of the trim tab can be determined at any time during the bending operation. The tool also includes apparatus for simultaneously calibrating the counterbalance device and the mechanism used to measure the degree to which the tab has been bent, prior to commencing the bending operation.

REFERENCES:
patent: 2297055 (1942-09-01), Grad
patent: 2359277 (1944-10-01), Saunders
patent: 2422042 (1947-06-01), Roberts
patent: 3280607 (1966-10-01), Esken

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