NASA SBIR 2020-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 20-1- A1.09-5690
SUBTOPIC TITLE:
 Inflight Icing Hazard Mitigation Technology
PROPOSAL TITLE:
 Low Power Rechargeable Anti-Icing System for Urban Air Mobility Vehicles
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Innovative Dynamics, Inc.
2560 North Triphammer Road
Ithaca, NY 14850
(607) 257-0533

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Mr. Joseph Gerardi
E-mail:
jg@idiny.com
Address:
2560 North Triphammer Road Ithaca, NY 14850 - 9726
Phone:
(607) 591-1742

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Patricia Stein
E-mail:
patricia@idiny.com
Address:
2560 North Triphammer Road Ithaca, NY 14850 - 9726
Phone:
(607) 257-0533
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 3
Technical Abstract (Limit 2000 characters, approximately 200 words)

Next-generation Urban Air Mobility vehicles will require All Weather Capability, including flight into known icing conditions. Ice or frost build-up on propeller surfaces decreases aerodynamic efficiency, resulting in loss of lift when even a small amount of ice builds on rotor-blade surfaces. This can lead to the loss of the aircraft in just minutes. Electrically powered quad-copters have no viable ice protection options today, primarily due to power and weight limitations.

 

IDI proposes development of a Low Power Anti-Icing System specific for short range, short endurance UAM missions. The proposed approach will feature a fast response icing sensor combined with a unique Rechargeable Rotor-Blade Anti-Icing System utilizing smart materials and embedded energy storage components that can be pre-charged independent of the UAM main battery pack. Unique to this design is the ability to wirelessly recharge the rotor de-ice system at electric vehicle docking stations using inductive coupling during scheduled UAM battery pack recharge cycles. 

During the Phase I Program IDI will develop a rechargeable ice protection system design and power management strategy. A prototype will be demonstrated in the Penn State AERTS Rotor Blade Icing Test Facility. Phase II will continue the development and test on a full scale UAM.

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

This research supports NASA’s goal to develop icing hazard mitigation technologies necessary for integrating UAS into the National Airspace System. The resulting system could be used to help support various ongoing icing research programs in the NASA Glenn Icing Tunnel and on NASA’s Icing Research Aircraft.

 

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

The Low Power Anti-Icing System can be applied on commercial quad-copter propellers for flight in instrument meteorological conditions. A wireless rechargeable deicer could be sold as a self-contained feature of next generation propellers. The low-power light-weight requirements give it a significant market advantage over current systems.

Duration: 6

Form Generated on 06/29/2020 21:02:44