SBIR/STTR Research Award

Vortex Control for Low-Noise DEP Urban Aircraft

Award identifier 57b31d62b794b68a4343173a90f2ed73e8a8ab2a9fd116fa0476ff2c3d5c2ed5Awarding agency National Aeronautics and Space Administration

Award amount

$124,996

Program and phase

STTR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Surfplasma, Inc.
Proposal award date
2019-08-19
Contract end date
2020-09-18
UEI
Y96ESVKCPTE9
Solicitation number
STTR_19_P1
Topic code
T15

Research abstract

Suppression of noise from aircraft is a vital NASA goal, especially important for the vision of Urban Air Mobility. Small urban aircraft may utilize Distributed Electric Propulsion along with advanced structural and electric motor/storage technologies to achieve the necessary flight capability. However, these aircraft utilize propellers or fans to achieve the necessary thrust, with attendant community noise issues. We propose to suppress perceived noise, especially during takeoff and landing in urban areas, by limiting the formation of vortical structures near the propulsor tips and trailing edges.nbsp;Tip vortices are common for airfoils, best illustrated by aircraft wings. The pressure difference between top and bottom creates a secondary flow, with a resulting vortex that increases noise and reduces lift. Winglets are effective in countering this effect. However, rotating airfoils ndash; propellers and fans ndash; cannot utilize winglets. Instead we propose to limit the secondary flow and tip vortex by utilizing thin, surface-mounted plasma actuators placed near the rotating blade tip.nbsp;SurfPlasma Inc. is a world leader in plasma actuator technology, having developed boundary layer control devices for many applications, including technology effective in the control of high speed air flows, relevant to aircraft propulsors even at low vehicle speeds. Also demonstrated is a technique for providing the required voltage to rotating systems. The overall objective of the current project is to demonstrate feasibility of plasma actuator-based flow control in rotating systems in order to achieve significant suppression of rotor-induced noise, without loss of thrust.nbsp;Development of this technology will benefit society by helping to enable more efficient intra-city personal transportation, with low infrastructure impact. Noise suppression technology would enhance acceptance of UAM vehicles and increase livability in urban areas and eventually impact larger aircraft and terrestrial fans.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

8 SBIR/STTR records share this UEI (2015–2025). Reported award amounts total $2,715,345. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Science Foundation, National Aeronautics and Space Administration, Environmental Protection Agency, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

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