Structural component and method for producing a structural component
作者： Memis Tiryaki , Michael Sauer
DOI:
关键词: Spacecraft 、 Stiffening 、 Engineering 、 Structural engineering 、 Section (archaeology) 、 Fuselage 、 Integrally closed 、 Structural component
摘要: A structural component for reinforcing the fuselage of an aircraft or spacecraft is integrally formed and segmented into surface-like stiffening sections, whereby at least one section as a rigid mesh section, solid section.
lens.org 参考文章(18)
Ulrich Bieling, Memis Tiryaki, System and method for interconnecting composite structures ,(2013)
Tobias Stroehlein, Paul Joern, Markus Kleineberg, Christian Huehne, Steffen Niemann, Markus Mueller, Method and a device for the manufacturing of a lightweight structure, and also a lightweight structure ,(2013)
Hermann Benthien, Barbara Kern, Coupling for joining two frame segments ,(2009)
Gopal P. Mathur, Multifunctional nano-skin articles and methods ,(2010)
Simon D. Senibi, Barry P. Van West, Douglas A. McCarville, Juan Carlos Guzman, Daniel M. Rotter, Method of forming a reinforced foam-filled composite stringer ,(2013)
Steven E. Pearson, Douglas G. Marciniak, Martin G. Andrews, Matthew M. Whitmer, Kenneth D. Cominsky, Rebecca M. Dixon, Jason L. Firko, Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same ,(2013)
Bruce K. Keough, Diane C. Rawlings, Wide area lightning diverter overlay ,(2005)
William G. Roeseler, David B. Christman, Apparatuses and methods for joining structural members, such as composite structural members ,(2005)
Dominique Micheaux, Raymond J. Palmer, Integral woven reinforcement for structural components ,(1982)
James L. Bullen, James W. Love, David M. Keicher, Mark E. Smith, Kevin J. Dullea, Pierrette H. Gorman, Forming structures from CAD solid models ,(2001)