SBIR/STTR Research Award

Revolutionary Coaxial Propulsors for Ultra-Quiet eVTOL

Award identifier 5823467f6c7d755d3d0c687b9fd408a67aa66869cf6edac909115a10124c43a9Awarding agency Department of Defense · Air Force

Award amount

$149,830

Program and phase

STTR · Phase I

Award year

2021

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
HARMONY AERONAUTICS LLC
Proposal award date
2020-12-05
Contract end date
2021-06-05
UEI
PSFJNKPTDJJ2
Solicitation number
X20.D
Topic code
AFX20D-TCSO1

Research abstract

Recently, the aerospace industry has witnessed a surge in interest in multirotor UAM (urban air mobility) systems for short-range personnel and cargo transportation for both civilian and military applications. This has resulted in significant capital investment and the development of numerous eVTOL (electric Vertical Take-off and Landing) aircraft. Soon, skies will be filled with busy buzzing multirotor aircraft, generating a new urban and suburban soundscape that is both different and louder than ever before. This intrusion of acoustic irritants into the last quiet recesses of life must be stopped if eVTOL are to be accepted by the public. Undesirably high sound levels are particularly problematic during hover and transition to cruise when the vehicle is close to people. During this time the propeller disk loading and rotational speeds are high creating high levels of annoying tonal noise. To address this, Harmony Aeronautics LLC will design and develop adaptable ultra-quiet coaxial propulsors for today’s diverse array of emerging eVTOL aircraft which will be 8 times (18dB) quieter than existing eVTOL propellers. Several in-house acoustic and rotor aerodynamic simulation tools have been developed. The acoustic code models the primary sources of rotor and propeller noise generation: thickness, loading, and broadband noise. The aerodynamic code predicts performance characteristics based on design parameters. These programs will be combined with high-fidelity 3D CFD simulation for a comprehensive analysis of propeller performance and rotor flowfield characteristics, and will be used to develop aeroacoustically optimized modular coaxial propulsors with minimal noise disturbances. A high blade solidity coaxial rotor configuration will be used to minimize the rotor RPM, as the blade tip speed is the primary driver of tonal noise. The impulsive unsteady loading caused by rotor-rotor and rotor-airframe interactions will be further attenuated using a novel double swept blade planform shape that dephases the acoustic effect of these interactions. Harmony Aeronautics has developed a hover-optimized prototype of the quiet coaxial rotor system and incorporated it into a sub-scale 22lb drone and a full-scale 550lb personal air vehicle. This was the result of participation in the Boeing sponsored GoFly challenge, a $2 million X-prize contest to develop a quiet, compact, high-endurance eVTOL personal air vehicle. The full-scale vehicle generated ~72dBA of noise in hovering flight at 50 feet, approximately 25 dBA quieter than a light helicopter in hover, and unprecedented for an aircraft of this size. The success of this quiet coaxial rotor demonstrates a promising solution to reducing eVTOL aircraft noise. Similar quieting techniques will be used to design propellers and integrate them into single coaxial propulsor units which will be scaled according to application requirements as demonstrated in the sub-scale and full-scale vehicles.

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

2 SBIR/STTR records share this UEI (2021–2022). Reported award amounts total $899,627. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: Department of Defense

Agency intelligence

Department of Defense

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