The present disclosure describes one or more systems, methods, routines and/or techniques for thermal management. One or more systems, methods, routines and/or techniques may provide advice or guidance (e.g., to a repair technician) regarding how to perform a hot bond repair, for example, on an aircraft component that has been damaged. The thermal management advisor may provide advice or guidance regarding how to prepare a repair field prior to running a thermal survey. For example, thermal management advisor may recommend a particular heat blanket, a configuration of the heat blanket, placement of various temperature sensors and other preparation guidance. The thermal management advisor may provide advice or guidance regarding how to alter or manage the repair setup during a thermal survey and during the actual curing process. For example, thermal management advisor may recommend particular temperature sensors or areas of the repair field that should be insulated.
SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES
SYSTEM UND VERFAHREN ZUR REPARATUR VON FLUGZEUGSTRUKTUREN AUS VERBUNDWERKSTOFF
SYSTÈME ET PROCÉDÉ DE RÉPARATION DES STRUCTURES COMPOSITES D'AVION
2017-02-01
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS |
SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES
European Patent Office | 2018
|SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES
European Patent Office | 2015
|System and method for repairing composite aircraft structures
European Patent Office | 2017
|SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES
European Patent Office | 2019
Repairing Commercial Aircraft Jet Engine Nacelle Composite Structures
SAE Technical Papers | 1984
|