Dielectric Measuring Tool for Radome Checkout

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    Information disclosed in this document was developed under the U.S. Government Small Business Innovation Research (SBIR)program. The information contained in this document is considered proprietary in nature by the author(s) and any disclosure is subject

    to the restrictions under Public Laws and supporting regulations governing this program. Use or disclosure outside of the U.S.

    Government of any information contained within this document without the expressed written consent of the author(s) is hereby

    prohibited. Further, release or disclosure of any information within the U.S. Government is restricted to that necessary to support the

    expressed purposes of the SBIR program. This restriction is to be retained with any and all parts of this document that are so

    distributed.

    Dielectric Measuring Tool forRadome Checkout:

    Prototype DevelopmentTexas Research Institute POC:

    Russell Austin

    (512) 263-2101

    amntlPOC:

    Reza Zoughi, Ph.D.

    (573) 341-4656

    OC-ALC COTR/TPOC:

    Todd Bayles

    (405) 662-7384

    OC-ALC FFR Manager

    Jess Phillips

    (405) 734-0229

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Background Repaired Radomes Inspected with Moisture Meter

    & Tap Testing

    Inspection Requires 4 Passes over the Radome

    Moisture Meter & Tap Testing

    Interior & Exterior Skins Tap Testing:

    May Not Accurately Determine Boundaries of Debond

    Operator Dependant Potential for Larger Repair Than Required

    Moisture Meter Not Always Accurate

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Relationship Between FFR & Repair Repaired Radomes sent to Far Field Range (FFR)

    to Test Radar Performance Approximately 40% of Repaired Radomes Fail

    FFR

    However: FFR Radar Performance Results cannot accurately

    determine location, extent or type of imperfectioncausing a performance failure

    Radar Performance Problems not Always Related to a

    Discrete Physical Flaw

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Return to Repair Facility Radome is Returned to Repair Facility after FFR

    Failure Current inspection methods available to repair

    personnel:

    provide no quantitative measurements cannot estimate if a radome will pass FFR tests

    only detect discrete flaws, not radar problems

    Repair Personnel Have no Guidance on How toAlter the Radome so it will Pass FFR

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    TRI/amntl Solution Show feasibility of millimeter wave reflectometry

    to solve radome problems detect presence of various flaws of interest

    detects flaws regardless of depth

    locates flaw edges fast, simple

    detects transmission problems even if no discreteflaw exists

    more complex quantitative measurements canmeasure phase and amplitude of reflections

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Samples with Known Flaws Manufactured by Applied Aerospace

    Structures Corp (AASC) Air Force radome manufacturer

    Fiberglass skins (6 layers top, 4 layers bottom)

    Honeycomb core (0.75 thick phenolic with 0.25diameter cells)

    Debonds & Delaminations Crushed Core

    Core Thickness Variations

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Sample Design Flaws:

    Debonds at BothSkin/Core interfaces

    Delams in Both Skins

    Crushed Core & Core

    Thickness Variations Water Ingress

    Thickness: 8 to 20

    mils Cross Section: 0.25

    to 1

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Sample Construction

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Basis of Method Finite Energy

    All incident energy willhave some reflectionand some transmission

    Change intransmission causes achange in reflection

    Quantifying reflected signals phase andmagnitude allows quantification of transmissionproblems

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Microwave Image 24 Flaws Obvious

    4 Flaws NotObvious

    3 in middle of lowerskin (12 mils thick)

    1 is 0.008 thickcrushed core nearlower skin

    Appears to showadditional features

    Excess adhesive?

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Higher Resolution Image All Flaws Detected

    More ComplexEquipment thanPrevious Image

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Water Ingress 0.1 cc water injected

    into a single cell of thehoneycomb

    First 6 images made

    over 2 days Final image made after

    emptying cell of water

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Hand Scans Video

    Technique is simple and real time Accurately detects radar performance anomalies

    & locates flaw edges (independent of flaw depth)

    Output is Simple DC Voltage could power needle gauge or light LEDs (green, yellow, red)

    proper analysis can provide quantitative phase and

    magnitude data COTS camcorder battery runs it for a week

    Cost Comparable to Other Flaw Detectors

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Correlate Test Data to Flaws Edges of all flaws located accurately regardless of

    flaw type or depth

    no need for complex signal analysis nor operatorinterpretation of data

    No ambiguity in locations of flaws

    Simple Equipment:

    All flaws except 8 mil core crush at far face anddebonds embedded in middle of far face detected

    Complex Equipment:

    All flaws detected

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Small B-52 Radome Sample

    Two Previous Repairs

    Build Up of Radome Coatings

    Radar Performance Unknown

    Note Center of Circular Repair and Large Repair

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Small Sample Results No NDI Indication:

    Various Coatings Large Repair

    Smaller Circular

    Repair

    Large Indication

    Joint of LargeRepair andCircular Repair

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Large B-52 Radome Sample

    Three Previous Repairs (two through wall, one exterioronly)

    Passed Radar Performance Testing

    No NDI Indications (Even where Repairs Overlap)

    Video of B-52 Radome Inspections Available

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Highlights So far, no False Positives

    Not radome specific - can be applied to radomes at allthree ALCs

    Detect Radar Anomalies, even if not caused by a discreteflaw

    Accurately determine size of radar anomaly regardless ofdepth

    Requires little operator training/data interpretation

    Quantitative phase and amplitude data can be used topredict FFR performance

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Cost/Cycle Time Reduction Depots currently go over each radome four times.

    This technology will require one time inspection labor reduced 75%

    B-52 Nose Radome Cycle Time

    44 days 6 days for inspection

    Millimeter Wave Inspection Reduce Cycle Time by 4.5Days

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Major Savings Current FFR failure rate for repaired radomes is

    ~40% Each Rebuild Costs $20k

    OC-ALC Rebuilds about Three Dozen B-52 Nose

    Radomes per Year B-52 Repair Facility Savings: $288k per year

    FFR Savings: testing fewer radomes that will fail

    Savings for More Numerous Aircraft (130, 135etc) Scales

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Current Status Field Prototype Development Started

    Develop handheld sensor for detecting and sizingflaws:

    crushed core, delams, fluid ingress, thicknessvariations

    radar anomalies

    Implement Two Reflectometers Built AroundSensor

    Handheld go/no go

    Quantitative measurement of phase and amplitude

    data can be used to predict FFR performance

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Go/No Go Prototype Handheld Probe:

    battery powered rugged enclosure

    audible/visual alarm (e.g. buzzer, LED, needle deflection)

    adjustable amplifier adjustable alarm trigger

    Calibration:

    known good section look at several places on radome and assume smallest

    signal is good

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Quantitative Version Essentially Similar Hardware as Go/No Go

    Electronics in Handheld Unit AutomaticallyDisplays Quantitative Phase and AmplitudeMeasurements

    Quantitative Data Used by FFR Personnel toDetermine Location and Severity of RadarAnomalies

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Most Important Result Determining if a

    Radar Window WillPass FFR TestingWithout Expenseand Effort of FFRTesting

    Allowing FieldPersonnel to QualifyRadome Repairs

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)

    program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Both Prototypes Tested on Existing Samples from Phase I

    Field tests at OC-ALC, WR-ALC andcommercial facilities

    B-1

    B-52

    E-3

    Provide Automated Prototypes with UserManual

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    Information disclosed on this page was developed under the U.S. Government Sma ll Business Innova tion Research (SBIR)

    program. The informa tion conta ined on this page is considered proprietary in nature by the author(s) and any disclosure is

    subject to the restrictions as stated in the cover sheet of this document.

    Contact InformationRussell Austin

    Texas Research Institute

    415 Crystal Creek Dr.Austin, TX 78746

    (512) 263 - 2101

    [email protected]

    Reza Zoughi, Ph.D.Applied Microwave NDT Lab

    University of Missouri Rolla

    224 Emerson Electric Co. Hall

    Rolla, MO 65409

    (573) 341-4656

    [email protected]

    Jess Phillips76 CMXG/MXCPATinker AFBVoice: 405-734-0229

    [email protected]