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The IPM GROUP Farmington Hills, Michigan

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Title: Weight Reduction Initiative Proposal Author: Bombardier Aerospace Last modified by: BD Created Date: 5/3/2004 7:07:00 PM Document presentation format – PowerPoint PPT presentation

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Title: The IPM GROUP Farmington Hills, Michigan


1
The IPM GROUPFarmington Hills,
Michigan
2
Contact us
  • Beni Dror
  • 27003 Hills Tech Drive
  • Farmington Hills, MI 48331
  • Tel 248 489 9490,
  • Fax 248 479 0771
  • e-mail bdror_at_ipmworld.com
  • Web www.ipmworld.com
  • Mail Address P.O.Box 252223
  • West Bloofield, MI 48325

3
Tactical Wheeled Vehicle Weight Reduction
Initiative
  • May, 2004
  • By
  • International Projects Management (I.P.M) LLC
  • Phone 248 489 94 90

4
Preamble
  • The attached are Examples of an on going weight
    reduction initiative for the HUMVEE.

5
PROGRAM
  • Selected Components were analyzed to
    re-engineered to reduction weight by 15-20
  • Brackets, Brackets Supports Transmission
    Supports.

6
Potential
  • Additional Components Under consideration
  • Alternator support bracket
  • Chassis beams
  • Engine components

7
Material and Manufacturing Method Selection
  • Selecting the most appropriate material and
    manufacturing methods according to the part
    loading and stiffness.
  • Special welding processes of high strength steel
    sheet
  • More Accurate Casting process to reduce tolerances

8
Using FEA methods
  • Using Finite Element Analysis enables us to
    refine the stress distribution under more
    realistic load application and attachment
    conditions, eliminating the inherent conservatism
    present in the original calculations.
  • Material lightly loaded can then be safely
    trimmed from the original part.

9
Examples of FEA used for weight reduction.
  • Part No. 12338191- Spring Seat
  • from 10.9 lbs to 9.4 lbs
  • Part No. 12469497- Alternator Support
  • from 25.3 lbs to 21 lbs
  • Part No. 12469498- Compressor Bracket
  • from 9.8 lbs to 8.1 lbs

10
Stress Report AbstractPart No. 12338191
  • Compiled
  • Name J. Hornstein
  • Title Stress Engineer
  • Checked
  • Name J. Hornstein
  • Title Stress Engineer
  • Approved
  • Name Dr Fredy H. Ornath
  • Title CEO Materials Systems

11
  • 1 Subject Spring Seat, Front, Stress Analysis
  • Scope
  • The scope of this report is to compare the
    strength of the proposed-design to the current
    design of the subject part under the same
    stipulated set of external loads. Currently the
    part is a low alloy, steel sheet (Ftu 60 ksi)
    welding assembly while the new design is a
    casting made of ductile iron of higher strength
    (Ftu 100 ksi).
  • Abstract
  • A coarse FEM of the current (welded) part was
    created and subjected to the stipulated set of
    applied loads.
  • The internal loads, (reactions at the rail
    attachment and the part displacements and
    stresses) were calculated.
  • The geometry of this model was then modified to
    represent the proposed design, retaining the
    loading and reaction system and the internal
    loads were calculated again.
  • A strength comparison was then performed
    considering both internal loads and material
    properties and a safety factor for the proposed
    part was calculated when applicable.
  • Conclusions and Recommendations
  • The maximum calculated stresses in the current
    part are exceeding the UTS of the material in the
    attachment flanges, which is attributable to the
    inherent conservatism of the analysis. On the
    assumption that the part had passed the
    certification tests this should not be a matter
    of concern.
  • While the strength of the proposed part is
    exceeding the strength of the current part,
    because of the materials low elongation (3 vs.
    22 for the current design) it is recommended to
    eliminate hot spots of tensile stresses above
    100000 psi by extending the lower bosses all the
    way to the horizontal flanges (see Figure 2.1.1
    on the next page)
  • References

12
Current 12338191 image
13
Current 12338191 - welding
14
New 12338191 - casting
15
12338191 Welding FE Model plot
16
12338191 Casting FE Model plot
17
12338191 Welding FE Results plot
18
12338191 Casting FE Stress plot
19
Part No. 12338191
  • Stress Report
  • Open 12338191_Stress_Report_Abstract.doc

20
12469497(R) and 12469498(L)
21
Stress Report AbstractPart No. 12469498
  • Compiled
  • Name J. Hornstein
  • Title Stress Engineer
  • Checked
  • Name J. Hornstein
  • Title Stress Engineer
  • Approved
  • Name Dr Fredy H. Ornath
  • Title CEO Materials Systems

22
12469498 Original part
New Part Weight reduction accomplished by
opening cutouts in original part
23
12469498 Original - FEM
24
12469498 Redesigned - FEM
25
Part No. 12469498
  • Stress Report
  • Open 12469498_Stress_Report_Abstract.doc
  • NoteAluminium Cast Alloy (e.g. 300 Series
    Aluminium Cast Alloy, MIL-HDBK-5G chapter 3.9)
    could offer acceptable strength, while reducing
    the part weight to a third of the current 9.8 lbs

26
Stress Report AbstractPart No. 12469497
  • Compiled
  • Name J. Hornstein
  • Title Stress Engineer
  • Checked
  • Name J. Hornstein
  • Title Stress Engineer
  • Approved
  • Name Dr Fredy H. Ornath
  • Title CEO Materials Systems

27
12469497 Redesigned part
Weight reduction accomplished by opening cutouts
in original part
28
12469497 Redesigned - FEM
29
Part No. 12469497
  • Stress Report
  • Open 12469497_Stress_Report_Abstract.doc
  • NoteAluminium Cast Alloy (e.g. 300 Series
    Aluminium Cast Alloy, MIL-HDBK-5G chapter 3.9)
    could offer acceptable strength, while reducing
    the part weight to a third of the current 25.3 lbs
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