In Situ Assembly of LDPE/PA6 Multilayer Structure by Stirring

2020 ◽  
Vol 35 (1) ◽  
pp. 58-69
Author(s):  
P. Pongmuksuwan ◽  
W. Harnnarongchai
Keyword(s):  
2021 ◽  
pp. 875608792110255
Author(s):  
M Heuser ◽  
A Zankel ◽  
C Mayrhofer ◽  
K Reincke ◽  
B Langer ◽  
...  

In this work, peel tests inside the chamber of an ESEM ( in situ peel tests) are described with heat-sealed test specimens of packaging systems made of multilayer films that simulate different flexible packaging types, according to the packaging line used. The in situ peel tests provided evidence to describe the influence of three different main aspects of the packaging process in relation to the opening behavior of the sealing packages. The investigated aspects are the peel angle, the alignment angle between the orientation of the multilayer films and the seal, and the bulge formation as a consequence of inadequate sealing parameters. In situ peel tests enabled the differentiation between peel angle and local (micro) peel angle, which results from the overall stiffness of the multilayer structure film. Alignment angles of 90° and 45° were found to produce similar opening forces. Images showing the formation of various new local micro fissures on new planes during the in situ peel test explained how the opening force can be dramatically increased during the tearing of two sealed multilayer films.


1986 ◽  
Vol 71 ◽  
Author(s):  
C. M. Gronet ◽  
C. A. King ◽  
J. F. Gibbons

AbstractSiGe/Si superlattices were grown using limited reaction processing in a chamber which allows both W-halogen and Hg arc wafer illumination. Each multilayer structure was fabricated in-situ by changing the gas composition between high temperature cycles. Commensurate SiGe alloy layers as thin as 15 nm were reproducibly deposited and were examined using transmission electron microscopy, sputtering Auger electron spectroscopy,and Rutherford backscattering. Preliminary results are presented on UV/ozone cleaning of LRP substrates to remove residual carbon contamination in-situ prior to film deposition.


1984 ◽  
Vol 75 ◽  
pp. 743-759 ◽  
Author(s):  
Kerry T. Nock

ABSTRACTA mission to rendezvous with the rings of Saturn is studied with regard to science rationale and instrumentation and engineering feasibility and design. Future detailedin situexploration of the rings of Saturn will require spacecraft systems with enormous propulsive capability. NASA is currently studying the critical technologies for just such a system, called Nuclear Electric Propulsion (NEP). Electric propulsion is the only technology which can effectively provide the required total impulse for this demanding mission. Furthermore, the power source must be nuclear because the solar energy reaching Saturn is only 1% of that at the Earth. An important aspect of this mission is the ability of the low thrust propulsion system to continuously boost the spacecraft above the ring plane as it spirals in toward Saturn, thus enabling scientific measurements of ring particles from only a few kilometers.


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