Abstract
We get the load and the work stress of aircraft accessory gearbox shell based on every starting and flying conditions of plane. By analyzing the stress level and stress distribution of the shell ,we assessed the shell structure validity and then proposed improving method .The study shows , the strength of the bearing mounting holes and its supporting stiffeners of the shell is lower than else structure part, and the starting condition is strength weak condition of the shell, so the study results supplies a theory reference to the design and improve method of aircraft accessory gearbox shell structure.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
