Woodbine Labs, Inc.

10624 Kenridge Dr.
Cincinnati, OH 45242
4 Employees

SBIR Award Summary

Total Number of Awards 6
Total Value of Awards $1.88MM
First Award Date 05/17/02
Most Recent Award Date 04/20/09

Key Personnel

Last Name Name Awards Contact
Ravenhall Mr. Richard Ravenhall 6 Message

6 Awards Won

Phase 1 SBIR

Agency: Navy
Topic: N091-031
Budget: 04/20/09 - 10/20/09

This proposal is for development of novel concepts and technology for design and processing of enhanced performance titanium matrix composite (TMC) helicopter masts. Such masts will be capable of drop-in replacement, be highly resistant to corrosion and stress corrosion cracking, have high fatigue capability, be lighter weight, have capability f...

Phase 1 SBIR

Agency: Defense Advanced Research Projects Agency
Topic: SB082-007
Budget: 03/10/09 - 11/15/09

This proposal is to develop and demonstrate technologies that will enable implementation of aircraft-engine titanium matrix composite (TMC) shafts that are significantly lighter weight and potentially permit engine sub-critical vibratory operation. Current and under-development advanced engines employ long length, nickel-alloy shafts that satis...

Phase 2 SBIR

Agency: Air Force
Topic: AF04-188
Budget: 05/09/05 - 09/09/07

This proposal is to develop and demonstrate technologies for a JSF TMC shaft. Two possible JSF TMC shaft configurations are possible. One is a large diameter, thick wall, very high torque, bottle shaped LP shaft that transmits torque from the LP turbine to both the engine s fan and an in-line lift-fan-shaft. The other is a stepped configurati...

Phase 1 SBIR

Agency: Air Force
Topic: AF04-188
Budget: 04/14/04 - 01/14/05

This proposal is to develop and demonstrate technologies for a VAATE TMC tapered counter-rotating shaft. The GEAE VAATE engine incorporates counter-rotating inner/outer shafts. The inner shaft has a long length, relatively small diameter and is tapered along its length. To satisfy dynamic and torsion requirements (high frequency along with hi...

Phase 2 SBIR

Agency: Air Force
Topic: AF02-185
Budget: 08/27/03 - 10/27/05

Titanium matrix composite LP shafts have large potential benefits. However, the high torque of current engines requires that oriented fiber TMC shafts have a wall thickness greater than normally considered manufacturable. A Phase I program addressed an innovative approach for (1) integrating shaft design, tool design and shaft processing, (2) ...

Phase 1 SBIR

Agency: Air Force
Topic: AF02-185
Budget: 05/17/02 - 02/17/03

This proposal is to develop and demonstrate a concept for a light-weight/lower-cost integrated process for producing TMC aircraft engine LP shafts. Such shafts will significantly benefit propulsion systems of advanced fighter aircraft like the JSF. The proposed integrated process will reduce the weight of a TMC JSF type LP shaft by approximate...