SYSTEMS AND METHODS FOR AIRCRAFT INTEGRATED COMPOSITE FRAMES
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United States of America Patent
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Issued Date -
Nov 15, 2018
app pub date -
May 10, 2017
filing date -
May 10, 2017
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Abstract
Systems and methods are provided for a variable web height aircraft composite structural beam. The variable web height aircraft composite structural beam can include a variable height web, a first flange located on an outer portion of the web, and a second flange located on an inner portion of the web. The variable height web is a first height in a first portion of the variable web height aircraft composite structural beam and a second height in a second portion thereof. The variable web height aircraft composite structural beam can be a structural beam of an aircraft.
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