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787 Passes Wing Bend Test


By Guy Norris This e-mail address is being protected from spambots. You need JavaScript enabled to view it
Los Angeles 
March 2010 
 
Boeing completed the ultimate load test on the static test 787 airframe, ZY997, at Everett on March 28. The test – officially dubbed Condition 18b - evaluated the ability of the wing-body structure to sustain loads equal to 150% of the design limit load, and represents the most extreme forces ever expected to be seen in service. Its clearance also marks the passing of a significant hurdle on the way to FAA certification.

During the test, which occurred with the fuselage pressurized to 14.9 psi, the wingtips were deflected upwards by approximately 25 ft. The test was also a key evaluation of the strengthened side-of-body modification which was instigated in June 2009 after initial load tests revealed potential weaknesses in the wing-root join.

The deflection of the higher-aspect-ratio composite wing was greater than that of the metallic 777 wing, the last major primary structure to undergo “wing ultimate up-bending” tests in Boeing’s sprawling Everett site more than 15 years ago. The 777 wing failed at 154%, having deflected 24 ft.

Although an apparent success, the company is sounding a note of caution before declaring victory. “The initial results of the ultimate-load test are positive. More extensive analysis and review are required before the test can be deemed a success,” says Boeing. The static test is an important milestone not only for further flight testing, but as a key structural verification of the design predictions. Stress and loads data from the test will also be used to determine the final design of the stretched 787-9 variant. 
 
READ MORE:    AviatiionWeek.com 
 
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