Transonic_C1_Compressor_Fiberglass_Blade_Construction.pdf

PDF 5 MB Posted

Attached to
Wind Tunnel Compressor Rotor Blades Federal contract opportunity
Solicitation number
FA9101-17-R-1000
Issued by
Department of the Air Force Materiel Command Test Center

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PWT TRANSONIC C1 COMPRESSOR

Fiberglass composite rotor blades Row A 31 blades Row B 33 blades Row C 33 blades

DistributionA‐Approved for Public Release, Distribution Unlimited

Blade Root

Portions of fiberglass ground (LE side) away to show steel strong back construction

Blade Root

Portions of fiberglass ground (TE side) away to show steel strong back construction

Bushings installed in strong back provide lubrication as blade swings on blade pin

Blade Sections, Root Section

Fiberglass blade skin and spar box construction near root section

Blade Sections, Mid Section construction near midsection of blade

Blade Sections, Tip Section construction near tip of blade

Blade Sections, Chord Section

Fiberglass blade construction; mid‐span to tip section

Blade with Row C Cuff

Fiberglass blade construction.

Person in photo is 6’1”.

Blade without Cuff

Fiberglass blade without cuff. The blade without a cuff is universal and can be configured by the addition of the appropriate cuff to be used in either Row A, B or C.

Blade with Cuff in Compressor

Fiberglass blade with cuff installed in the compressor. The blade swing is limited by the spacer mounted to each side of the blade.

Row C Cuff

Fiberglass blade cuff is attached to blade using foaming core splice adhesive with the blade and cuff in an alignment fixture.

Row C Cuff

Blade Attachment to Rotor Disc

Fiberglass blade attachment to rotor disc requires a steel adaptor attached to the disc with the blade pinned to the adaptor to allow the blade to swing.

Blade swing limits transmission of bending moments into the rotor disc.

File details come from the government source that posted it. Updated .