HB 7491-1997 in English

VALID

Verification Requirements for Composite Material Structure Strength of Military Aircraft

Issued on:1997-09-23
Implemented on:1997-10-01
File Format:PDF
Delivery:Via email within 5 business days

Price(USD)： $790.00
$767.00

Standard No:	HB 7491-1997
Document status:	VALID
Title in English:	Verification Requirements for Composite Material Structure Strength of Military Aircraft
Title in Chinese:	军用飞机复合材料结构强度验证要求
Language:	English
File Format:	Electronic (PDF)
Delivery:	Via email within 5 business days
Issued on:	1997-09-23
Implemented on:	1997-10-01
ICS Classification:	49.025-Materials for aerospace construction
Chinese Classification:	V15-Composite materials and solid fuels
Professional Classification:	HB-Aviation
Related Keywords:	military aircraft verification requirements composite material structure strength military aircraft scopethis standard power-driven manned military aircraft
Related Topics:	material structure hb7491 material structure Composite Strength hb 7491-1997 hb+7491 Composite Strength Alloy structural steel for military use table binding strength Structural Analysis of Organic Materials Composite particle size Material Validation Analysis Composite material Composite Materials and Structures Composite material verification requirements composite structure Composites flexural strength Composites flexural strength Material Validation Analysis table binding strength complex parsing structure Structural strength composite structure HB1997- composite material Composites for military ships Mechanical Properties of Military Composite Materials General requirements for military aircraft painting Xifei composite material preparation Aircraft composite material requirements Interfacial bonding strength between composite layers Interlayer bonding strength of composite materials Composite aircraft structure certification Aircraft Strength Test Design Chinese military aircraft strength Common military aircraft friction materials Retest requirements for chemical retest period General principles for strength and stiffness specifications for military aircraft verify Analytical method validation repeatability requirements Composite material bonding strength

Scope

This standard specifies the verification requirements and verification methods for strength, stiffness, durability and damage tolerance necessary for the structural integrity of military aircraft composite materials. This standard applies to the ordering, design and verification of composite structures for power-driven manned military aircraft with fixed wings or variable swept wings; it also applies to similar structures on manned military helicopters and vertical/short-moment take-off and landing aircraft. Ordering, design and verification of structural properties of composite structures.

More samples: GB 18306-2015 DL/T 5154-2012 JC/T 2453-2018

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