Nolan B Phillips, 497829 Standley St, North Richland Hills, TX 76180

4083656, Apr 11, 1978

Mar 21, 1975

5/560587

James L. Braswell - Hurst TX
Cecil E. Covington - Hurst TX
Nolan B. Phillips - Fort Worth TX
Reggie J. Tomerlin - Cleburne TX
Robert M. Wohlfeld - Dallas TX

Textron, Inc. - Providence RI

B64C 2732

416226

A composite rotor blade has a nose spar of fiber reinforced plastic with the fibers extending spanwise the length of the spar and at the root encircling a transverse hub attachment structure with the spar provided with a tubular inner liner of cross ply filament wound fiberglass forming a closure for the nose spar with a blad afterbody structure including skins for integrating the afterbody with the nose spar and liner. Preferably the spar has an inner liner and an outer liner both of cross ply filament wound fiberglass in multi layers. The blade afterbody structure includes honeycomb filler having cells extending in the direction of blade thickness.

2018027, Sep 27, 2018

Mar 24, 2017

15/469463

- Fort Worth TX, US
Mark E. Wasikowski - Keller TX, US
Andrew Ryan Maresh - Lewisville TX, US
Nolan B. Phillips - Bedford TX, US

B64C 27/00
B64C 27/473

In one embodiment, a rotor blade may comprise a blade body, a spar structure, and a blade nose. The blade body may comprise a skin, wherein the skin is configured to form an airfoil shape, and wherein the airfoil shape comprises an inboard end, an outboard end, a leading edge, and a trailing edge. The spar structure may comprise a first spar cap and a second spar cap, wherein the first spar cap is coupled to an upper portion of the skin, and wherein the second spar cap is coupled to a lower portion of the skin. The blade nose may comprise a cavity, wherein the cavity is configured to house a plurality of modular weights at a plurality of radial blade locations, wherein the plurality of radial blade locations comprises a range of locations between the inboard end and the outboard end.

2014010, Apr 24, 2014

Oct 23, 2012

13/658407

- Fort Worth TX, US
Loan Thanh Vo - Hurst TX, US
Frank Bradley Stamps - Colleyville TX, US
Nolan Phillips - Bedford TX, US

BELL HELICOPTER TEXTRON INC. - Fort Worth TX

B23P 15/04
B32B 41/00
B32B 37/16
B32B 38/00
B64C 27/473

29 2351, 2988971, 416230, 156 64

A method of constructing a composite component includes at least one of laterally and longitudinally aligning a material strip relative to a concavity of a layup tool, at least one of laterally and longitudinally extending the material strip to a predetermined location relative to the layup tool, wherein the material strip is substantially rectangular, and vertically abutting the material strip to the concavity of the layup tool, wherein the longitudinally extending the material strip includes at least one of (1) measuring a longitudinal distance of the material strip and (2) aligning a longitudinal end of the material strip with a longitudinal distance indicium and wherein the laterally extending the material strip includes at least one of (1) measuring a lateral distance of the material strip and (4) aligning a lateral end of the material strip with a lateral distance indicium.