Industry University Crosstalk Dan Adams University of Utah - - PowerPoint PPT Presentation

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Industry University Crosstalk Dan Adams University of Utah - - PowerPoint PPT Presentation

Industry University Crosstalk Dan Adams University of Utah adams@mech.utah.edu (801) 5859807 1 Nov Nov 2107 2107 My My Backgr Background ound 20 Years as Mechanical Engineering Professor at the Univ. of Utah 3 Years in Utah


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SLIDE 1

Industry‐University Crosstalk

Dan Adams

University of Utah

adams@mech.utah.edu (801) 585‐9807 1 Nov Nov 2107 2107

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SLIDE 2

My My Backgr Background

  • und
  • 20 Years as Mechanical Engineering Professor at the Univ. of Utah
  • 3 Years in Utah Composites Industry
  • Hercules Inc. Composites Design and Analysis, 1983‐1986
  • Total of 37 years of experience in composite materials
  • Vice‐Chair, ASTM Committee D30 on Composites
  • Co‐Chair Composite Materials Handbook (CMH‐17) Testing Working Group
  • Design and Testing Columnist for CompositesWorld Magazine
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SLIDE 3

Je Jeff Ke Kessler

  • 11 Years as Composites Lab Manager at the
  • Univ. of Utah
  • 2 Years in Utah Composites Industry
  • Hercules Inc. Test Engineer, 1984‐1986
  • 7 Years as Composites Lab Manager at the

University of Wyoming

  • 20+ years of composites testing experience
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SLIDE 4

Re Research Sum Summary: ary:

Composi Composite Te Test Met Method Dev Developm pmen ent

  • Composite Wedge Test for Adhesive Durability Assessment
  • Flat‐Coupon Crush Test for Composite Laminates
  • Combined‐Loading Shear (CLS) Test for Composite Laminates
  • Sandwich Composite Mode I Single Cantilever Beam (SCB) Test
  • Sandwich Composite Compression After Impact (CAI) Test
  • Sandwich Composite 4‐Point Flexure After Impact (4FAI) Test
  • Sandwich Composite Open Hole Compression (OHC) Test
  • Sandwich Composite Open Hole Flexure (OHF) Test

(All in process of ASTM standardization)

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SLIDE 5

Re Research Sum Summary: ary:

Composi Composite Te Test Met Method Dev Developm pmen ent

  • Composite Wedge Test for Adhesive Durability Assessment
  • Flat‐Coupon Crush Test for Composite Laminates
  • Combined‐Loading Shear (CLS) Test for Composite Laminates
  • Sandwich Composite Mode I Single Cantilever Beam (SCB) Test
  • Sandwich Composite Compression After Impact (CAI) Test
  • Sandwich Composite 4‐Point Flexure After Impact (4FAI) Test
  • Sandwich Composite Open Hole Compression (OHC) Test
  • Sandwich Composite Open Hole Flexure (OHF) Test

(All in process of ASTM standardization)

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SLIDE 6

Composi Composite Te Test Met Method

  • d Dev

Developmen pment: t:

Fla Flat‐Coupon Coupon Crush Crush Te Test

Sponsor Sponsors: Departm Departmen ent of

  • f Ener

Energy gy (D (DOE) Fe Federa ral Av Aviation Adm Adminis nistration

  • n (F

(FAA)

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SLIDE 7

Composi Composite Te Test Met Method

  • d Dev

Developmen pment: t:

Fla Flat‐Coupon Coupon Crush Crush Te Test

Unsupported Testing For Flat Sections Pin-Supported Testing For Curved Sections

Design‐value development Material property evaluation

Component tests Sub‐component tests Structural elements tests Allowable development Material specification development Material screening and selection

Full‐

scale

tests

Analysis validation

Courtesy of Kevin Davis, Boeing

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SLIDE 8

Re Research Sum Summary: ary:

Composi Composite Te Test Met Method Dev Developm pmen ent

  • Composite Wedge Test for Adhesive Durability Assessment
  • Flat‐Coupon Crush Test for Composite Laminates
  • Combined‐Loading Shear (CLS) Test for Composite Laminates
  • Sandwich Composite Mode I Single Cantilever Beam (SCB) Test
  • Sandwich Composite Compression After Impact (CAI) Test
  • Sandwich Composite 4‐Point Flexure After Impact (4FAI) Test
  • Sandwich Composite Open Hole Compression (OHC) Test
  • Sandwich Composite Open Hole Flexure (OHF) Test

(All in process of ASTM standardization)

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SLIDE 9

Composi Composite Te Test Met Method

  • d Dev

Developmen pment: t:

Mo Mode I Si Single ngle Can Cantilev ever er Beam Beam Te Test

Sponsor: Sponsor: Fe Federa ral Av Aviation Adm Adminis nistration

  • n (F

(FAA)

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SLIDE 10

Composi Composite Te Test Met Method

  • d Dev

Developmen pment: t:

Mo Mode I Si Single ngle Can Cantilev ever er Beam Beam Te Test

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SLIDE 11

Re Research Sum Summary: ary:

Structur Structural al Heal Health Mo Monitor toring ng

Sponsor Sponsors: NASA, NASA, Na National

  • nal Sci

Science nce Founda undation

  • n
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SLIDE 12

Re Research Sum Summary: ary:

Structur Structural al Heal Health Mo Monitor toring ng

In In Col Collabor aboration ion wi with Orbi Orbital AT ATK Im Impact Loc Location tion Es Estim timation tion

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SLIDE 13

Re Research Sum Summary: ary:

Structur Structural al Heal Health Mo Monitor toring ng

In In Col Collabor aboration ion wi with Orbi Orbital AT ATK Dam Damage Det Detection ction and and Cl Classific assification tion

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SLIDE 14

Uni Univer ersi sity ty‐ Indus Industr try Cr Cross

  • sstal

alk: k:

How Can Utah Composites Industry Help Us?

  • In

Internship rnships and and jo job opportuni

  • pportuniti

ties es fo for our

  • ur studen

udents

  • To

Tours of

  • f co

comp mpos

  • sites

es facilitie cilities

  • Ex

Excess/ cess/expi piri ring ng mater material als (pr (prepr preg, film film adhesi adhesive, co core re mater material als) s)

  • Opportuni

Opportuniti ties es to to collab llaborate

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SLIDE 15

Univ Univer ersity sity‐ Ind Industry ry Cr Cross

  • sstalk:

alk:

Some Thoughts on Collaborating

  • Wo

Work on

  • n get

getting re require red agr agreemen eements ts in in pl place ace in in adv advance nce

  • Service ve

versus re research when when ap applic licab able le

  • Cos

Cost, qual quality, speed speed (PICK (PICK TW TWO) O)

  • When

When possi possibl ble, e, su sufficie icient sc scope and and peri period

  • d of
  • f perf

perform

  • rmance

nce to to support support a gr gradua aduate studen udent

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SLIDE 16

Thanks for your attention! Comments/Questions?