Aircraft part as compound product

• Main Author: JULIAN NORLEY
• Format: Patent
• Language: Chinese; English
• Published: 16.07.2014
• Subjects: AEROPLANES; AIRCRAFT; AMMUNITION; AVIATION; BLASTING; CHEMISTRY; COMPOSITIONS BASED THEREON; COMPOSITIONS OF MACROMOLECULAR COMPOUNDS; COSMONAUTICS; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; HEATING; HELICOPTERS; LAYERED PRODUCTS; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM; LIGHTING; MECHANICAL ENGINEERING; METALLURGY; ORGANIC MACROMOLECULAR COMPOUNDS; PERFORMING OPERATIONS; TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION; TECHNICAL SUBJECTS COVERED BY FORMER USPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS; THEIR PREPARATION OR CHEMICAL WORKING-UP; TRANSPORTING; USE OF INORGANIC OR NON-MACROMOLECULAR ORGANIC SUBSTANCES ASCOMPOUNDING INGREDIENTS; WEAPONS

The utility model relates to thermal management of an aircraft compound material and particularly relates to a compound product. The compound product comprises a fiber reinforced resin compound material with an inner part as well as inner and outer surfaces and a hot product formed by an anisotropic graphite flake. The graphite flake has a thermal-machine design constant of at least 10mm-W/m*K. The hot product is arranged in the inner part of the fiber reinforced resin compound material. The thermal-machine design constant is defined as follows: heat conductivity coefficient of the material multiplies average thickness.