Segmented rotor blade trim tab

Details Segmented rotor blade trim tab Segmented rotor blade trim tab

2006-08-01

2006-08-01

Look, Edward K. (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Articulated, resiliently mounted or self-shifting impeller...

Sectional, staged or nonrigid working member

C416S22300B

Reexamination Certificate

active

07083383

ABSTRACT:
A trim tab assembly for a helicopter rotor blade includes a plurality of metal panels that are secured to the trailing edge of a composite material helicopter blade. Each of the metal panels can be bent relative to the rotor blade to tune the aerodynamic properties of the rotor blade.

REFERENCES:
patent: 2760588 (1956-08-01), Zeerip
patent: 4188171 (1980-02-01), Baskin
patent: 2004/0253108 (2004-12-01), Schmaling et al.

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