SBIR/STTR Research Award

Improved Full Authority Digital Engine Control (FADEC) System

Award identifier 4c7d805a99782c34a68ec1cec517bc2a8c3b3e67b846200adb4d9630bdd74070Awarding agency Department of Defense · Air Force

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2010

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ORBITAL RESEARCH INC
Proposal award date
2010-03-17
Contract end date
2010-12-24
UEI
JQTYNHJ9CWN6
Solicitation number
2009.3
Topic code
AF093-174

Research abstract

Current Full Authority Digital Engine Controls (FADECs) and Electronic Engine Controls (EECs) perform their tasks by using multiple IC chips and several printed circuit boards. Tasks performed by these chips include power regulation, communications, actuator drive, sensor monitoring, processing capable of number crunching, prognostic health management, and fault detection and isolation. Implementations of these FADEC functions on a system-on-a-chip (SOC) will improve performance and reduce the size, weight, and thermal footprint of FADEC systems on traditional turbine engines. Orbital Research Inc. proposes to develop a high temperature SOC for aircraft engine FADECs and EECs using discrete and custom high temperature (200oC - 220oC) components. This SOC will provide the interfaces to most inputs and outputs on existing and next generation turbine engine EECs, and will provide the state-of-the-art prognostic and diagnostic functions. In order to accomplish the Phase I goal of demonstrating design and fabrication techniques that meet the requirements called out in the solicitation Orbital will adapt its existing high-temperature ASICs as follows: Modify design rules for synthesis, emulation, simulation and layout for use in the manufacturing process. Incorporated necessary layout rules. Compare the simulation results to compute improvement in area, power consumption, and bandwidth. BENEFIT: During Phases I and II of this project Orbital Research Inc will design, develop, and test a prototype system-on-a-chip (SOC) implementation of FADEC functions to improve performance and reduce the size, weight, and thermal footprint of FADEC systems on traditional turbine engines. The temperature tolerance of the SOC developed herein opens numerous applications for the military market, including advanced engine and flight controls, unmanned aerial vehicles, directed energy systems, military control units, actuators, and more-electric systems. Projected applications for the developed SOC temperature-tolerant control technology in the civilian sector are equally attractive and include commercial aircraft, automotive, ground-based power generation, oil industry, and harsh industrial processing applications. In addition to significant high temperature intelligent interface needs for commercial aircraft (a high-temperature distributed control system reduces the wiring harness complexity by a factor of 10 or more while saving weight), significant automotive and oil/gas drilling markets exist.

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

121 SBIR/STTR records share this UEI (1991–2025). Reported award amounts total $41,189,372. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, Department of Health and Human Services, National Aeronautics and Space Administration, National Science Foundation, Department of Education, Department of Energy

Agency intelligence

Department of Defense

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