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DYNAMIC EFFECTS ON AIRBORNE ELECTRONICS

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
GOLUEKE, CARL A., author.
Conference Name:
SAE NATIONAL AERONAUTIC MEETING
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1958
Summary:
SUMMARYAirborne electronics as used in current aircraft are normally quite fragile in relation to the environment. The gap is being bridged by the use of isolators. The state of the art in ruggedization techniques for electronics is sufficiently advanced to preclude the use of isolators, but experience indicates that this advance is not being exploited in aircraft applications. This paper presents some specific vibration levels that general airborne electronics and component parts will withstand without the benfit of vibration isolators. Because of the large scope and complexity of the electronics area, it is to be realized that these susceptibility levels are only generalized indications. Also, applicability and function of vibration isolators is briefly discussed
Notes:
Vendor supplied data
Publisher Number:
580364
Access Restriction:
Restricted for use by site license

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