| Created: 10/24/95 |
Updated: 8/18/98 |
Project Number: C95-18
Use of Electronic Hardware at Elevated Temperature
Point of Contact: Dr. Yogi Joshi
email: yogi@calce.umd.edu
Phone: (301) 405-5428
Fax: (301) 314-9269
Objective
Describe effects that limit the use of electronic hardware at elevated
temperatures up to 200° C.
Background
Limiting operation to temperatures below the traditional barrier of 85°
C can be extremely costly for electronics used for sensing and control
in such environments as automotive underhood, aerospace, chemical processing
and well logging. The costs are associated with the price, size, weight,
and reliability limitations of cooling systems and/or the hardware associated
with remote placement of the electronics. This is particularly true for
avionic systems where the allowable weight and volume are severely constrained.
Developments in the design and manufacture of electronic components indicate
that the presently accepted temperature limits may be unduly restrictive,
particularly when compared to the actual benefit realized. Many systems
should be able to perform adequately up to 200° C with no changes,
and others may require only minor materials or design alterations. Knowledge
of the effects of elevated temperatures and strategies to accommodate these
temperatures can be useful to engineers, allowing them to make informed
design tradeoffs based on the actual costs and benefits involved in operation
at elevated temperatures.
Work Accomplished
This project consisted of a feasibility study of six candidate electronic
modules to determine the technical challenges to their operation under
the desired high temperature conditions. It involved the collection and
analysis of material data for temperatures up to 200° C, including
mechanical, electrical, and thermal properties of materials, and their
relationship to temperature within that range and the application of this
information to the design analysis. Design information on each module was
provided by the member companies, including block diagrams and parts lists,
as well as information on the use environments. The following are the key
deliverables:
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A document describing generic materials-related limitations to the use
of electronics at elevated temperatures up to 200° C. These reports
include tables of maximum use temperatures for electronic materials along
with relevant mechanical, electrical, and thermal properties of these materials
and their relationship to temperature. Materials were characterized from
many elements of packaging, including but not limited to the
-
semiconductor die
-
die attach
-
leadframe/substrate
-
case
-
first-level interconnect
-
boards
-
solders
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connectors
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boxes
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Reports were generated for each of the six representative electronic modules
listed below:
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A proposed subsonic flight control product.
-
A proposed supersonic engine control.
-
An existing cockpit lamp dimmer.
-
An existing ARINC 629 SIM.
-
A point-of-use power supply for aircraft.
-
An existing automotive engine controller.
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These reports identify the technical challenges to be met in the temperature
ranges of interest, the risks involved, and potential solutions to those
challenges.
-
A book on high temperature electronics has been published based on contributions
from experts in the field.