>Date: Wed, 11 Feb 1998 12:00:34 +0100
>To: "Miller, Michael W" <Mike.Miller3@PSS.Boeing.com>, "'RP Mail List'"
<rp-ml@bart.lpt.fi>
>From: Matteo Righini <m.righini@democenter.it>
>Subject: Re: Sibco LOM material
>In-Reply-To:
<816A0A914A8BD01181A900805F31E0B2011C475B@xch-sea-06.ca.boeing.com>
>
>At 09.59 10/02/98 -0800, Miller, Michael W wrote:
>>I'm going to try out Sibco's paper on our 2030. I had never heard of
>>this alternate material option before yesterday. Any opinions (good and
>>bad) or advice on this material would be welcome. Thanks,
>>Michael W Miller (Mike.Miller3@PSS.Boeing.com)
>>The Boeing Company MS 17-PE B-XT62
>>Propulsion Experimental Hardware 206-655-3289
>>Rapid Prototyping 655-4366 Lab 655-4365
>>
>>For more information about the rp-ml, see http://ltk.hut.fi/rp-ml/
>>
>>
Dear Michael
We have a LOM 1015 and we are trying Sibco's paper now.
I think it's more resistant than Helisys paper but it's more difficult to
manage the process building.
Precisely during the process the surface temperature of part must remain in
a particular window to optimize the sticking of different layers (50°C-57°C
or 122°F-135°F).
So you must regulate the heater velocity accordingly and check the surface
temperature during the building process.
I think that with LOM 2030 there are more problems but i don't know precisely.
Kind Regards
Eng. Matteo Righini
Rapid Prototyping Service Manager
DemoCenter
Via Virgilio, 55
41100 Modena, Italy
Phone: ++39 59 848810
Fax: ++39 59 848630
For more information about the rp-ml, see http://ltk.hut.fi/rp-ml/
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