Author: Wendy Lin
Publisher:
ISBN:
Category :
Languages : en
Pages : 442
Book Description
Induction Heating Model for High Frequency Induction Joining and Repair of Complex-shape Graphite Fiber/polymer Matrix Composites
Induction Heating Model for High Frequency Induction Joining and Repair of Complex-shape Graphite Fiber
Scientific and Technical Aerospace Reports
Dissertation Abstracts International
Author:
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 816
Book Description
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 816
Book Description
American Doctoral Dissertations
Author:
Publisher:
ISBN:
Category : Dissertation abstracts
Languages : en
Pages : 796
Book Description
Publisher:
ISBN:
Category : Dissertation abstracts
Languages : en
Pages : 796
Book Description
Thirty-third Annual Report on Materials Research at Stanford University, January 1, 1993 - December 31, 1993
Author: Stanford University. Center for Materials Research
Publisher:
ISBN:
Category :
Languages : en
Pages : 176
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 176
Book Description
Conference Proceedings
Author: Society of Plastics Engineers. Technical Conference
Publisher:
ISBN:
Category : Plastics
Languages : en
Pages : 964
Book Description
Publisher:
ISBN:
Category : Plastics
Languages : en
Pages : 964
Book Description
Utilization of Induction Bonding for Automated Fabrication of Tigr
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781723907616
Category :
Languages : en
Pages : 46
Book Description
A laboratory study of magnetic induction heat bonding of titanium foil and graphite fiber reinforced polymer prepreg tape, TiGr, demonstrated that the process is a viable candidate for low cost fabrication of aircraft structure made of this new material form. Data were obtained on weld bonding of PIXA and PETI-5 prepreg to titanium. Both the foil and honeycomb forms of titanium were investigated. The process relies on magnetic susceptor heating of titanium, not on high frequency heating of graphite fiber. The experiments showed that with a toroid magnet configuration, good weld bonds might be obtained with heating times of a few seconds. These results suggest the potential is good for the induction heating process to achieve acceptable commercial production rates.Hinkley, Jeffrey A. and Johnston, Norman J. and Hulcher, A. Bruce and Marchello, Joseph M. and Messier, Bernadette C.Langley Research CenterTITANIUM; WELDING; FOILS (MATERIALS); HONEYCOMB STRUCTURES; GRAPHITE-POLYIMIDE COMPOSITES; RESEARCH; LABORATORIES; TECHNOLOGY UTILIZATION; TOROIDS; PREPREGS; METAL-METAL BONDING; MAGNETIC INDUCTION; LOW COST; INDUCTION HEATING; HIGH FREQUENCIES; HEATING; FIBER COMPOSITES; FABRICATION; AIRCRAFT STRUCTURES
Publisher: Independently Published
ISBN: 9781723907616
Category :
Languages : en
Pages : 46
Book Description
A laboratory study of magnetic induction heat bonding of titanium foil and graphite fiber reinforced polymer prepreg tape, TiGr, demonstrated that the process is a viable candidate for low cost fabrication of aircraft structure made of this new material form. Data were obtained on weld bonding of PIXA and PETI-5 prepreg to titanium. Both the foil and honeycomb forms of titanium were investigated. The process relies on magnetic susceptor heating of titanium, not on high frequency heating of graphite fiber. The experiments showed that with a toroid magnet configuration, good weld bonds might be obtained with heating times of a few seconds. These results suggest the potential is good for the induction heating process to achieve acceptable commercial production rates.Hinkley, Jeffrey A. and Johnston, Norman J. and Hulcher, A. Bruce and Marchello, Joseph M. and Messier, Bernadette C.Langley Research CenterTITANIUM; WELDING; FOILS (MATERIALS); HONEYCOMB STRUCTURES; GRAPHITE-POLYIMIDE COMPOSITES; RESEARCH; LABORATORIES; TECHNOLOGY UTILIZATION; TOROIDS; PREPREGS; METAL-METAL BONDING; MAGNETIC INDUCTION; LOW COST; INDUCTION HEATING; HIGH FREQUENCIES; HEATING; FIBER COMPOSITES; FABRICATION; AIRCRAFT STRUCTURES
Induction Heating Advances
Author: A. F. Leatherman
Publisher:
ISBN:
Category : Induction heating
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Induction heating
Languages : en
Pages : 56
Book Description
Induction Heating of Carbon-Fiber Composites: Thermal Generation Model
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
Book Description
A theory of local and global mechanisms of heat generation and distribution in carbon-fiber-based composites subjected to an alternating magnetic field has been proposed. A model that predicts the strength and distribution of thermal generation through the thickness of carbon-fiber-based laminated composites has been developed. Earlier work has established the distribution of point voltages in the plane of the laminate that exist in the form of potential differences between fibers in adjacent plies in a cross-ply or angle-ply laminate system. In this work a capacitive-layer microstructure that models the actual fiber-reinforced-polymer microstructure from a square-packing assumption to a series of conductive parallel plates is formulated. An effective parameter of heating, gamma, that establishes the distribution of heating through the thickness is defined. Extreme gradients in this thermal source can exist with peaks occurring at the interfaces of ply-ply orientation changes. An optimization study establishes the effect of various microstructural and macrostructural parameters on the heating parameter, gamma. Several parametric studies are performed on the computer algorithm, which calculates gamma to further analyze these effects.
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
Book Description
A theory of local and global mechanisms of heat generation and distribution in carbon-fiber-based composites subjected to an alternating magnetic field has been proposed. A model that predicts the strength and distribution of thermal generation through the thickness of carbon-fiber-based laminated composites has been developed. Earlier work has established the distribution of point voltages in the plane of the laminate that exist in the form of potential differences between fibers in adjacent plies in a cross-ply or angle-ply laminate system. In this work a capacitive-layer microstructure that models the actual fiber-reinforced-polymer microstructure from a square-packing assumption to a series of conductive parallel plates is formulated. An effective parameter of heating, gamma, that establishes the distribution of heating through the thickness is defined. Extreme gradients in this thermal source can exist with peaks occurring at the interfaces of ply-ply orientation changes. An optimization study establishes the effect of various microstructural and macrostructural parameters on the heating parameter, gamma. Several parametric studies are performed on the computer algorithm, which calculates gamma to further analyze these effects.