Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Uwe Beier"'
Publikováno v:
Zeitschrift Kunststofftechnik. 1:146-173
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f3fd239be4d74b5a412864d146594a4
https://doi.org/10.3139/o999.02012018
https://doi.org/10.3139/o999.02012018
Publikováno v:
Journal of Thermoplastic Composite Materials. 31:1587-1608
The increasing content of thermoplastic composites in the aerospace industry requires the application of new joining technologies. Their main assembly advantage is rivetless joining, which needs to be examined in greater detail in order to compensate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea8c0b9f93f62cfdee3b625b6232841d
https://doi.org/10.1177/0892705717738390
https://doi.org/10.1177/0892705717738390
Autor:
Uwe Beier, Antje Helbig
Publikováno v:
WSI-Mitteilungen. 69:386-389
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b50a4d3025b74030a781091fefa702a
https://doi.org/10.5771/0342-300x-2016-5-386
https://doi.org/10.5771/0342-300x-2016-5-386
Autor:
Uwe Beier, Oliver Schieler
Publikováno v:
KMUTNB International Journal of Applied Science and Technology. :27-36
With the increasing requirements on aircrafts with respect to performance and costs, there is a need for a systematical use of the advantages of different materials and innovative joining technologies. This necessitates inter alia the use of thermopl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7acd470ade380b91a3b02c57b4fb7e52
https://doi.org/10.14416/j.ijast.2015.10.005
https://doi.org/10.14416/j.ijast.2015.10.005
Simulation and experimental validation of gaps and bridging in the automated fiber placement process
Publikováno v:
Science and Engineering of Composite Materials, Vol 22, Iss 2, Pp 131-148 (2015)
With the increasing demand for carbon fiber-reinforced parts in the aerospace industry, automated manufacturing methods such as automated fiber placement (AFP) are being established. To utilize AFP’s strong potential on multiple-curved surfaces suc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b8ade85408bbe7136e7cb89f808a4665
https://doi.org/10.1515/secm-2013-0158
https://doi.org/10.1515/secm-2013-0158
Publikováno v:
Key Engineering Materials. :465-471
Presenting interesting aspects such as a high strength-to-weight ratio, Carbon Fibre Reinforced Plastic components are frequently used in the aerospace industry. The forming step, which conforms the reinforcement to a specific geometry, is a sensitiv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2bcb8dc9853e02aab870e36e8f07360
https://doi.org/10.4028/www.scientific.net/kem.554-557.465
https://doi.org/10.4028/www.scientific.net/kem.554-557.465
Autor:
Jan K.W. Sandler, Wolfgang Buchs, Volker Altstädt, Christian Weimer, Uwe Beier, Hermann Spanner, Frank Fischer
Publikováno v:
Composites Part A: Applied Science and Manufacturing. 39:705-711
A comparative assessment of the influence of assembly seams based on two different thermoplastic yarn types on key in-plane and interlaminar properties of carbon fibre-reinforced epoxy composite is presented. Non-crimped fabric (NCF) composites prepa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2578f560d5cfdcc66cb1757373a477d0
https://doi.org/10.1016/j.compositesa.2008.02.011
https://doi.org/10.1016/j.compositesa.2008.02.011
Autor:
Volker Altstädt, Jan K.W. Sandler, Wolfgang Buchs, Frank Fischer, Christian Weimer, Uwe Beier
Publikováno v:
Composites Part A: Applied Science and Manufacturing. 38:1655-1663
A comparative assessment of the influence of pure assembly seams based on a thin (11 tex) polyester yarn in a zigzag geometry on the resulting mechanical performance of a non-crimped fabric (NCF) carbon fibre-reinforced epoxy composite manufactured b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f79827d3d2ce8f788c698176631ab4a9
https://doi.org/10.1016/j.compositesa.2007.02.007
https://doi.org/10.1016/j.compositesa.2007.02.007
Publikováno v:
Science and Engineering of Composite Materials, Vol 18, Iss 4, Pp 209-215 (2011)
The present study describes the results of a detailed investigation of the fracture toughness and fatigue crack growth behaviour of epoxy resins used for aeronautic applications. More specifically, the influence of incorporating thermoplastic or trib
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::49b3686065f4ed4b8f3a5db03c407dc3
https://doi.org/10.1515/secm.2011.042
https://doi.org/10.1515/secm.2011.042