Military Embedded Systems

Army rotorcraft blade control tech developed by Army Research Lab


March 28, 2016

John McHale

Editorial Director

Military Embedded Systems

Army rotorcraft blade control tech developed by Army Research Lab

ABERDEEN PROVING GROUND, Maryland. U.S. Army researchers at the Army Research Laboratory (ARL) performed a live-fire test on a rotor blade that has individual blade control technology.

"The purpose of this program is to generate some limited ballistic data that could reduce risk and/or encourage Future Vertical Lift designers to consider CTEF technology," says Brian G. Smith, ARL-SLAD aviation analysis team leader.

Specifically, the live fire CTEF experiments explore the ballistic vulnerability of emerging individual blade control technologies and promote the development of components that are threat ready for Army rotorcraft. Researchers fired three shots representative of typical ground fire on a 7-foot span, 10-inch chord rotor blade section with a 4-foot long Continuous Trailing Edge Flap, or CTEF, at ARL's Survivability and Lethality Analysis Directorate's Airbase Experimental Facility 6 and 7.

"We wanted to know what would happen to vehicle performance, or the rotor blade structural integrity, if it is hit by live fire in combat," says Matthew L. Wilbur, ARL Vehicle Technology Directorate senior research engineer working at the NASA Langley Research Center. "This technology may provide reduced noise signature, reduced vibration, enhanced rotor performance and also offer a lighter and more efficient technology for flight control of the helicopter."

The CTEF experiments are being conducted under the Science and Technology Red Teaming initiative that is sponsored by the Office of the Assistant Secretary of the Army for Acquisition, Logistics and Technology, or ASA (ALT). This initiative enables early, in-depth vulnerability assessments of emerging technologies across laboratory, table-top, and live field environments.

A team from ASA (ALT) visited researchers March 4 to observe another round of test firings and to speak with researchers.

"We want to understand how this technology might be applied to future aircraft," said Todd M. Turner, ASA (ALT) Air Portfolio director. "Our goal is to design, develop and demonstrate the next generation of technologies that will provide unmatched vertical lift aircraft performance to meet future operation capabilities."

"The actuators used in the CTEF are not your typical motors -- they are solid-state devices that change shape when an electric current is applied," Wilbur says. "They work great, but if they are damaged they tend to short circuit, which means that the remaining healthy actuators no longer receive the power they need to function. To defeat this failure mode, we devised a method where each actuator has a small fuse in-line with its connection to the power source. For this particular test, that meant fabricating a blade in which each actuator was individually wired and the fuses were external to the blade at the point where the electrical power was distributed."

Wilbur says that in a follow-on activity the researchers hope to begin later this year, small surface-mount fuses will be embedded directly on the actuators, so that no outside electrical power distribution or extensive wiring will be necessary.

"The big active-rotor breakthrough associated with this was the fact that the insertion of the fuses in-line with each actuator worked perfectly," he says. "We acquired high-speed blade performance data during each of the shots, and in each case it is clear that the blade continued to actuate with no degradation in performance other than that attributable to the loss of the damaged actuators."

Funding to conduct this research is the enabling factor, he adds.

"When we don't have money, we do a lot of analysis and we come up with great ideas, but then at some point you have to start building some hardware and sometimes that gets a little harder to do when there's not enough money flowing," he says. "Without the Red Teaming funding this critical vulnerability assessment would not happen early in the applied research phase."