HB 7709-2002 in English

VALID

Design requirements of mechanically fastened joint of composite structure for airplane

Issued on:2002-11-20
Implemented on:2003-02-01
File Format:PDF
Delivery:Via email within 1~3 business days

Price(USD)： $120.00
$117.00

Standard No:	HB 7709-2002
Document status:	VALID
Title in English:	Design requirements of mechanically fastened joint of composite structure for airplane
Title in Chinese:	飞机复合材料结构机械连接设计要求
Language:	English
File Format:	Electronic (PDF)
Delivery:	Via email within 1~3 business days
Issued on:	2002-11-20
Implemented on:	2003-02-01
Chinese Classification:	V22-Mechanical gadgets and components
Professional Classification:	HB-Aviation
Related Keywords:	composite structures composite structure fiber/lipid-based composite structures similar composite structures design requirements
Related Topics:	material structure mechanical design iec material structure copper mechanical connection Institutional Mergers and Institutions mechanical connection aircraft mechanical parts Structural Analysis of Organic Materials composite structure mechanical connection hb7709 composite structure Materials, structures, electronics Composite connection composite material Xifei composite material preparation Aircraft composite material requirements Composite aircraft structure certification Composite cabin section connection ring

Scope

This standard specifies the design requirements for mechanical connections of aircraft composite structures. This standard is applicable to the mechanical connection of various reinforced fiber/lipid-based composite structures of aircraft and the mechanical connection of metal and composite structures; the mechanical connection of similar composite structures on helicopters can be used as a reference.

More samples: GB 50021-2001(2009) GB 18306-2015 DL/T 368-2010

Sample only — not a preview of HB 7709-2002

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