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Innovative Approaches to the Fabrication of Composite Rotary Wing Main Rotor Blade Spars with Option

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-10-C-0116
Agency Tracking Number: N081-026-1263
Amount: $1,087,160.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N08-026
Solicitation Number: 2008.1
Timeline
Solicitation Year: 2008
Award Year: 2010
Award Start Date (Proposal Award Date): 2010-07-20
Award End Date (Contract End Date): 2015-10-15
Small Business Information
134 Sandy Dr
Newark, DE -
United States
DUNS: 960998474
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Mark Gruber
 Senior Partner
 (302) 369-5390
 mgruber@accudyne.com
Business Contact
 Mark Gruber
Title: Senior Partner
Phone: (302) 369-5390
Email: mgruber@accudyne.com
Research Institution
N/A
Abstract

Sponsored by NAVAIR, Accudyne Systems completed a Phase 1 SBIR program, developing an equipment and process concept for cost-effective fabrication of composite rotary wing main rotor blade spars. The CH-53K spar was the study focus. The recommended work cell concept combines automated tape placement, woven fabric placement, and pick and place of 45° parallelograms to layup plies, then debulk and place packs for two spars fabricated in tandem. All composite material placement, vacuum bag material application, pack-to-tool debulking, and spar revolution is automated. This Phase 2 program develops the stations on the work cell machinery encompassing the material lay-up portion of the proposed work cell, and then demonstrates them for inclusion in a follow-on full design. Special attention will be paid to placing at rates high enough to allow fabrication of 200 spars per year (4 per week). In Phase 2, Accudyne proposes to complete a Requirements Document to detail requirements learned from NAVAIR, Sikorsky, and Hexcel. Then, Accudyne proposes to develop equipment and the process to demonstrate: 1) unidirectional tape placement into plies and on-line debulking to packs, 2) woven fabric placement into plies and on-line debulking to packs 3) bias parallelogram cut, pick, and place and debulking, 4) cutting of unidirectional tape, woven fabric, and bias parallelograms, and 5) a technical trade study encompassing throughput, tolerances, debulking, quality control, machine maintenance, risks, and final implementation. A final report describing the process, equipment, and trade study will conclude Phase 2. The Phase 2-Option program enhances bias ply placement to considerably accelerate spar fabrication. The enhancement is a 3-axis CNC-controlled ultrasonic knife to complete articulate cuts in the bias parallelograms that comprise the bias plies. The noteworthy benefit is that net shape bias packs can be fabricated with the wide ply down with no further cutting. It is intended that the Phase 2-Option run in concert with Phase 2 for maximum synergy.

* Information listed above is at the time of submission. *

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