Window frame for aircraft
作者： Jens Bold
DOI:
关键词:
摘要: With a window frame (1) for installation in the exterior shell (5) of an aircraft, which comprises at least one outer flange (2), inner (3), and vertical (4) arranged perpendicular to between these flanges, is attached element (7, 8) be held. This fixed its position via plurality holder elements (10) distributed equidistance over periphery (1), being connected with (2) frame. Each base plate (11) pin (12) surface, as well downholder clip (13) that can brought into force-fit engagement (12). The surfaces are provided sawtooth-like structure, hook-shaped clamping (15) flexibly formed on ring-shaped locking (14) displaced. comprise thermoplastic material, reinforcement fibers made by die casting. Before plates adhered upon mounting, riveted aircraft.
lens.org 参考文章(49)
Michael J. Irish, Window clip for aircraft ,(1992)
Juergen Meyer, Aircraft window construction ,(1997)
Heinz Kunert, Glass pane intended direct bonding, especially automobile glass pane ,(1989)
Walter A. Stephan, Hermann Filsegger, Window unit for aircraft cabins ,(1998)
Georg Schuon, Heinz Weber, Bernd Gross, Laminates of improved edge stability ,(1991)
David Carl Allen, Patricia Burchfield Walters, Moisture seal for aircraft windows ,(1989)
Walter Leon White, Ben Redito Oani, Aircraft window escuthcheon assembly ,(1998)
John Christopher Starling, Anthony Ivan Clifford Kirk, Roberto Cruz Aquino, Thomas Edward Anthony Henson Webb, Aircraft cabin panel and insulation retainer with integrated use as a spacer-isolator ,(1987)
Domenic S. Giuntoli, Ryon Christopher Warren, William Quan, Paul Mikulencak, Michael A. Ritts, Ralph Bladt, Richard Fraker, Joseph P. Condon, Aircraft windows and associated methods for installation ,(2002)
Bernhard Nordmann, Uwe Habisreitinger, Michael Ostgathe, Method and device for producing shell-shaped plastic parts reinforced with fibre mats ,(2001)