Test piece for determining I type fracture energy of compound propellant/coating layer bonding interface
A coating layer and propellant technology, applied in the field of composite propellant/coating layer bonding interface I-type fracture energy measurement specimens, can solve end deflection, affect experimental accuracy, and not suitable for stiffness/weight ratio and other issues to achieve the effect of easy disassembly and increased rigidity
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment
[0019] A composite propellant / coating layer adhesive interface type I fracture energy measurement specimen, including a loading block 1, an aluminum support beam, a composite propellant layer 3, a grating 4, an adhesive layer 5 and a coating layer 6, wherein, The composite propellant layer 3 and the cladding layer 6 are bonded through the adhesive layer 5, and the two ends are aligned, and one end is not bonded, leaving a prefabricated crack, pushing the composite propellant layer 3, the adhesive layer 5 and the cladding layer 6 in the middle of the sides A grating 4 is pasted on the position, the initial scale of the grating 4 corresponds to the tip of the prefabricated crack, and the corresponding surfaces of the bonding surfaces of the composite propellant layer 3 and the cladding layer 6 are respectively bonded with aluminum support beams, and the aluminum support beams One end is aligned with the end of composite propellant layer 3, adhesive layer 5 and cladding layer 6 wi...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 