High temperature resistant vacuum bag sealing adhesive tape
Technical field
The present invention relates to a kind of sealant tape, particularly a kind of high temperature resistant vacuum bag sealing adhesive tape.
Background technology
In the manufacturing processed of fan blade and aircraft, between vacuum bag and making mould, need sealing.Vacuum bag also claims decompression packing, according to atmosphere principle, carry out, the Main Function of vacuum bag is deoxygenation, in the manufacturing processed of fan blade and aircraft, between vacuum bag and mould, need when vacuumizing, seal, this just needs the adhesive tape of favorable sealing property to seal.
In the manufacturing processed of fan blade and aircraft, all to use resin, as unsaturated polyester or epoxy resin and fiber, as glass fibre or carbon fiber pass through mould molding, manufacturing processed will be used vacuum bag sealing to vacuumize, be vacuum bag and make between mould and need adhesive tape to seal between vacuum bag and vacuum bag, can there are some problems in the sealant tape of prior art: (1) high thermal resistance is poor: because material resin is to vacuumize while heating in moulding process, so be to have very high requirement to the high temperature resistant of sealant tape, the sealant tape resistance to elevated temperatures of prior art is low, (2) spatter property of the demoulding: for convenient construction, many manufacturerss require the sealant tape demoulding to facilitate, and have not allowed any cull to stay on mould, and this is also prior art cannot meet a bit.
Summary of the invention
Technical problem to be solved by this invention is to provide a kind of high temperature resistant vacuum bag sealing adhesive tape for the existing problem of prior art, and its maximum operation (service) temperature can reach 180 ℃, and depart from making mould is not have cull to be trapped on mould simultaneously.
Technical problem to be solved by this invention can be achieved through the following technical solutions:
A high temperature resistant vacuum bag sealing adhesive tape, is characterized in that, by raw material extrusion moulding after being uniformly mixed of following weight part:
Isoprene-isobutylene rubber: 8-10 part;
Chloroprene rubber: 10-12 part;
Cardanol Modified PF Resin: 1.5-2.5 part;
Nano-calcium carbonate: 30-35 part;
Glass fibre 3-6 part, length is 5-6mm;
Superfine talcum powder 25-30 part;
Zinc oxide 1.6-2.0 part;
Stearic acid 0.5-1.2 part;
Tackifying resin 2.0-2.5 part;
Titanium dioxide: 1.0-1.5 part;
Dioctyl phthalate (DOP) 1.0-1.4 part.
Beneficial effect of the present invention is: in the manufacturing processed of fan blade and aircraft, air tight while vacuumizing, maximum operation (service) temperature can reach 180 ℃, and depart from making mould is not have cull to be trapped on mould simultaneously.
Embodiment
Below in conjunction with embodiment, the present invention will be further described.All embodiment are parts by weight below.
Embodiment 1
8 parts of isoprene-isobutylene rubbers, 10 parts of chloroprene rubbers, 1.5 parts of Cardanol Modified PF Resins, 30 parts of nano-calcium carbonates, 3 parts, glass fibre, length is 5mm, 25 parts of superfine talcum powders, 1.6 parts, zinc oxide, 0.5 part of stearic acid, 2.0 parts of tackifying resins, 1.0 parts of titanium dioxides, 1.0 parts of dioctyl phthalate (DOP)s.
Preparation method is: by the extrusion moulding after being uniformly mixed of above-mentioned each component.
Embodiment 2
9 parts of isoprene-isobutylene rubbers, 11 parts of chloroprene rubbers, 2.0 parts of Cardanol Modified PF Resins, 32 parts of nano-calcium carbonates, 4 parts, glass fibre, length is 5.5mm, 28 parts of superfine talcum powders, 1.8 parts, zinc oxide, 1.0 parts of stearic acid, 2.3 parts of tackifying resins, 1.2 parts of titanium dioxides, 1.2 parts of dioctyl phthalate (DOP)s.
Preparation method is: by the extrusion moulding after being uniformly mixed of above-mentioned each component.
Embodiment 3
10 parts of isoprene-isobutylene rubbers, 12 parts of chloroprene rubbers, 2.5 parts of Cardanol Modified PF Resins, 35 parts of nano-calcium carbonates, 6 parts, glass fibre, length is 6mm, 30 parts of superfine talcum powders, 2.0 parts, zinc oxide, 1.2 parts of stearic acid, 2.5 parts of tackifying resins, 1.5 parts of titanium dioxides, 1.4 parts of dioctyl phthalate (DOP)s.
Preparation method is: by the extrusion moulding after being uniformly mixed of above-mentioned each component.
Table 1 has reflected resistance to elevated temperatures and the demolding performace of above-described embodiment.
Table 1
Project |
Embodiment 1 |
Embodiment 2 |
Embodiment 3 |
Maximum operation (service) temperature ℃ |
390 |
410 |
425 |
Demolding performace |
Without cull |
Without cull |
Without cull |