SBIR/STTR Research Award

Non-Contact Propeller De-Icing System

Award identifier 046b8865204b005ada2fa997934a4d6acfdcb07ee0420a1c47ef328c4dc4ede2Awarding agency Department of Defense · Navy

Award amount

$69,919

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
DIVERSIFIED TECHNOLOGIES, INC.
Proposal award date
Not reported
Contract end date
Not reported
UEI
ZNG4WKWT2YM4
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Diversified Technologies, Inc. (DTI) proposes to develop a reliable, non-contact, retrofittable de-icing power transfer technology to improve the propeller de-icing system for the E-2C, C-2, P-3 and C-130 turboprop aircraft. The proposed system willoperate efficiently with low noise and weight. Specifically, DTI proposes to utilize the available 400 Hz electrical power to operate a rotating transformer to couple power to the spinner. The power transfer system will be adapted to the T56-A-425/427turbine engines, and retrofittable by removing the existing carbon brush and ring assemblies. The transformer primary couples over a full arc or sector that coincides with the existing brush assembly volume. Circuit impedance matching elements can beinserted to cancel the reactive effects of the transformer making the net result a purely resistive power transfer from the generator standpoint. Variations of the concept are applicable to a diverse set of military and commercial rotorcraft and fixed wingaircraft.During Phase I DTI will design, build, and test a full-scale power transfer system to prove technical feasibility and, optionally, perform an aircraft integration study to show retrofit capability. The proposed non-contact approach will significantly increase the reliability and reduce the maintenance requirements for the de-icing power transfer system. The system will be retrofitted into the available volume for minimum engine impact. It hasadditional power transfer capability in the event greater de-icing power is desired. This concept is applicable to a wide range of military and fixed-wing aircraft and rotorcraft, as well as rotating systems such as air surveillance radars. The completelyencased, non-contact system does not generate, and is unaffected by, airborne contaminants; is impervious to the presence of corrosive hydraulic fluids; and has no permanent magnet to attract contaminating ferromagnetic particles. The elimination ofspurious electrical noise by removing the brushes will also improve radar, electronic countermeasure system, and avionics operation.

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

166 SBIR/STTR records share this UEI (1989–2025). Reported award amounts total $65,542,650. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, Department of Energy, Department of Agriculture, Environmental Protection Agency, National Science Foundation

Agency intelligence

Department of Defense

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