SBIR/STTR Research Award

Integrated High Frequency Electric Propulsor for Turbo-Electric Aircraft

Award identifier 52135c65a80c5339f37296f216e0c0c3d545c3d5331a5b50037071dc7ca31fa0Awarding agency National Aeronautics and Space Administration

Award amount

$739,431

Program and phase

SBIR · Phase II

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
HINETICS LLC
Proposal award date
2019-12-18
Contract end date
2021-12-17
UEI
U1L3YYF21K35
Solicitation number
SBIR_18_P2
Topic code
A1

Research abstract

We propose the development of a high efficiencynbsp;integrated electric turbofan directly driven with anbsp;high frequency, air-core synchronous motor. If the projected efficiency and specific power are achieved, this technology cannbsp;increase the viability ofnbsp;turbo-electric airplanes for commercial air transport, leading to significantly lower carbon emissions and fuel use. The key innovation is the use of high fundamentalnbsp;frequenciesnbsp;and a mostly air-core electromagnetic architecture. The aerospace industry employs 400 Hz lsquo;acrsquo; to keep component weights low. Hinetics is planning to introduce products that push these frequencies up by an order of magnitude. The machine is transformed from the traditional metal-intense design to a composite and silicon-intense design. The new architecture is projected to improve machine power density by a factor of two over current best-in-class machines, with simplifiednbsp;air cooling, while achieving 98% efficiency. Additionally, the radially thin geometry, with self-pumped air cooling, lends itself nicely to integration within a ducted turbofan. A proof of concept high frequency MW scale motor has been developed by the University of Illinois under a NASA funded project. The design leverages recent advances in Wide Band-Gap (WBG) power electronic devices to obtain anbsp;high fundamental frequency while keeping current and voltage harmonics low. Hinetics LLC will build on this technology to develop an integrated electric tail-cone propulsor for commercial transport aircraft.nbsp; Computer modeling in thenbsp;SBIR Phase I projectnbsp;has confirmed thatnbsp;the high frequency motor can be tightly integrated with a propulsion fan at the scale of NASA#39;s STARC-ABL airplane concept and achieve high efficiency (2 points higher than best-in-class) whilenbsp;retaining cooling andnbsp;power-to-weight advantages. In Phase II, Hinetics would like to validate this with a hardware demonstration, and build partnerships with Tier I suppliers to commercialize the technology.nbsp;

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

10 SBIR/STTR records share this UEI (2018–2025). Reported award amounts total $3,946,285. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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