Connecting method of connected part
A connection method and a technology of connectors, which are applied in the field of materials, can solve problems such as poor fatigue life gain and lower structural static strength, and achieve the effects of increasing reliability and tightness, improving joint strength, and improving fatigue life
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2015-02-04
- Estimated Expiration
- Not applicable · inactive patent
Abstract
Description
technical field
[0001] The invention relates to the field of material technology, in particular to a connection method for connected parts. Background technique
[0002] Resin-based composite materials have unique advantages such as high specific strength and specific modulus, strong designability, and good fatigue resistance, and are widely used in the aerospace field. In applications, resin-based composite materials are often connected with traditional metal skeletons, and the connection forms are mostly openings and rivets. The opening of the hole cuts the fiber reinforcement in the composite material, and at the same time forms a high-stress area at the edge of the hole. After the hole is opened, the composite material is generally mechanically connected together by aluminum alloy or titanium alloy rivets. The impact effect, and the anisotropy of the composite material plate makes the edge area of the hole produce peeling stress due to the edge effect when impacted, w...
Examples
Embodiment Construction
[0015] In order to make the purpose, technical solutions and advantages of the present invention clearer, the following technical solutions in the present invention are clearly and completely described. Obviously, the described embodiments are some embodiments of the present invention, rather than all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative work all belong to the protection scope of the present invention.
[0016] The TiNiNb memory alloy and TiNi alloy that the present invention selects for use, wherein TiNiNb composition mainly is Ti 45-X Ni 46+X Nb9at% (x=0~5), its martensitic transformation initiation temperature can be adjusted at -60~-20°C. TiNi alloy composition is mainly Ti 51.5-X Ni 48.5+X (x=0~3), the martensitic transformation initiation temperature can be adjusted at -40~-20°C. The raw materials used for TiNiNb alloy and TiNi alloy are 0-grade industri...