SBIR/STTR Research Award

High Torque, Direct Drive Electric Motor

Award identifier 9fc11159e9f9e4e35d41c0ba8c9956ee228099bfbb9e7a4bc2715caa6f71bba3Awarding agency National Aeronautics and Space Administration

Award amount

$597,439

Program and phase

SBIR · Phase II

Award year

2011

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BEAR TECHNOLOGIES, LLC
Proposal award date
2011-06-01
Contract end date
2013-06-01
UEI
EKKBGUCGAPD3
Solicitation number
Not reported
Topic code
S5.03

Research abstract

Bear Engineering proposes to advance the development of an innovative high torque, low speed, direct drive motor in order to meet NASA's requirements for such devices. Fundamentally, all electric motors basically work on the same electromagnetic principle: a tangential electromagnetic force attracts the rotor to the stator. Just when the rotor field is closest to the stator field and the electromagnetic attraction is greatest, the power is interrupted and another set of magnetic poles repeats the cycle. Furthermore, the two magnetically attracted elements never make contact, which would otherwise offer the highest force of attraction.The proposed novel motor design, successfully demonstrated at TRL 4 in Phase 1, operates and behaves entirely differently from all other known electric motor designs and is capable of producing incredibly high, direct drive torques at low rotational speeds. Its operational performance is similar to that of a stepper motor with a 1000:1 gearhead attached, but the similarity ends there. The motor is configured such that its length to diameter aspect ratio is opposite that of traditional motors as it has a relatively large diameter and short axial length; this offers all new packaging opportunities. The design also allows for a single, large diameter bearing pair to be used for the motor's output shaft which renders it stiff enough to directly mount the driven elements. The need for additional bearing supports and bearing mounting structure is thus eliminated. By the end of Phase 2, the system will be designed, developed and tested at TRL 6 with Mars environmental conditions.

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 (2009–2014). Reported award amounts total $1,920,406. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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