← Back to NASA Technology Projects

Flight Adaptive Blade for Optimum Rotor Response (FABFORR)

Completed TRL 5 (started at 4, targeting 5)

Description

While past research has demonstrated the utility and benefits to be gained with the application of advanced rotor system control concepts, none have been implemented to date on a production military or commercial rotorcraft. A key contributor to this fact is the inherent cost associated with installation and maintenance of these control systems, since many system designs require the replacement of a helicopter's rotor blades, rotor hub components, or both. The proposed work addresses this deficiency through the development of an on-blade full-span camber control system that reaps many of the known benefits of advanced rotor control, in a retrofit design approach that has the potential to achieve production status due to its lower risks and costs compared to previous system concepts. The design leverages past work in the use of smart-material actuated bistable tabs for rotor blade tracking, with a newer integral actuation concept that will lead toward a more robust and flightworthy design.

Benefits

Retrofit blade controls may enhance the performance, and reduce both acoustic emissions and blade-induced vibrations of suitably equipped rotorcraft over baseline vehicles. Since this capability could be achieved using technology that does not require the re-blading of an existing helicopter, a significant commercial product improvement program for a variety of aircraft would be possible. Military operators would also realize improved mission capability and reduced aircraft downtime with these anticipated improvements.

Having the capability to alter the spanwise camber of rotor blades could be used to investigate aeromechanics issues of rotorcraft that could lead to the development of optimal operational profiles to maximize the utility and cost-effectiveness of existing and future helicopter designs incorporating these control features.

Details

Technology areaFlight Vehicle Systems > Aeroscience > Aeroacoustics
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationContinuum Dynamics, Inc., Ewing, NJ
Start date2010-01-29
End date2010-07-29

Project contacts

Listed on TechPort itself — the most direct way to ask about this specific project.

How to get involved

This is early/mid-stage (TRL 5) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.