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  1. #1
    Join Date
    Jun 2008
    Posts
    11

    RFQ : 5/8" cubes (6061 alum.) 100/1000/5000 pcs

    I am looking for a quote of 100, 1000, and 5000 cubes of aluminum (6061 or similar) 5/8" x 5/8" x 5/8". If raw 5/8" square stock is used, then the 3rd dimension should match the stock (EG - .630 x .630 x .630 ). Tolerance I would prefer would be +/-.001", but consistency of the 3 dimensions to each other is the most critical thing.

    I assume the best way to do this is to pull and part the stock. If that is the case and parting gives both sides a nice finish that is square within .001" consistently no face off is necessary (a very slight nub could be acceptable. Quote it in both faced front/parted back and just parted finish on both sides if you can.

    Thanks for your interest,

    dukejavelin

  2. #2
    Join Date
    Jan 2012
    Posts
    43
    Pm sent.

  3. #3
    Join Date
    Nov 2012
    Posts
    55

    Aero-Technologies West

    PM sent. Thanks for your consideration!

  4. #4
    Join Date
    Jul 2012
    Posts
    56
    PM sent. Thank you

  5. #5
    Join Date
    Jan 2008
    Posts
    449
    You probably need to clarify the parts use and tolerances for flatness and squareness. Obviously running from 12 foot bars on a lathe with a puller or pusher is going to be the quickest and cheapest way. The back and front faces will be parallel. Unfortunately unfinished extruded stock can very greatly in width, straightness (slight twists), flatness, and the corners aren't all 90 degrees, and are rounded off.

  6. #6
    Join Date
    Aug 2010
    Posts
    128
    Thanks dualkit. I was hoping you were going to chime in

  7. #7
    Join Date
    Mar 2010
    Posts
    1852
    Very curious as to why you would need a tolerance of + or - .001" on these. After all the bars could vary + or - .009" per advertised specifications.

    Not to lecture just to inform, so please don't take this wrong, but I did a lot of stuff for Boeing aircraft. There were areas on their parts that needed precision and I did some to + or - .0002", but if it was not needed the other tolerances of that same part might be + or - 1/16". Boeing knew one thing, precision costs money. .001" is about 1/4 to 1/3 the thickness of a human hair.

    Just letting you know just in case.



    Mike
    Two Haas VF-2's, Haas HA5C, Haas HRT-9, Hardinge CHNC 1, Bother HS-300 Wire EDM, BobCAD V23, BobCAD V28

  8. #8
    Join Date
    Jun 2008
    Posts
    11
    Thanks for the advice..... twist shouldn't matter over 5/8" i wouldn't think. I definitely hear you on the variation but the test bar i got from msc that i sawed then mill faced never varied from end to end by more than. 0015" either way from .629... but maybe i got lucky....;-) as far as rounded off corners it is desirable....i will be tumbling, sandblasting, etc on them so the fresh cut corners will eventually be radiused as well.

  9. #9
    Join Date
    Jun 2008
    Posts
    11
    Thanks for the advice..... twist shouldn't matter over 5/8" i wouldn't think. I definitely hear you on the variation but the test bar i got from msc that i sawed then mill faced never varied from end to end by more than. 0015" either way from .629... but maybe i got lucky....;-)

  10. #10
    Join Date
    Feb 2013
    Posts
    0
    PM sent with quote info.

  11. #11
    Join Date
    Jun 2012
    Posts
    514
    is this rfq still open? if so shoot me a pm
    Big Chipin, spreading tha cheese, I be Big Chipin for days!

  12. #12
    Join Date
    Jun 2008
    Posts
    11
    I have accepted a bid. Thanks for responding everyone!

    -Duke

  13. #13
    I am starting to think that may be my problem...

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