摘要:
The present disclosure provides a method for bonding parts, comprising the following steps (a) Providing a two-component adhesive composition precursor, comprising Part (A) comprising at least one first dye and at least one epoxy curing agent; Part (B) at least one second dye different from first dye and at least one epoxy resin; (b) Mixing part (A) and part (B) of the two-component adhesive composition precursor to obtain an adhesive composition; (c) Applying the adhesive composition onto a first part; (d) Applying a second part onto the adhesive composition applied to the first part; (e) Perform a first curing step at a first temperature, wherein the adhesive composition undergoes a first colour change; Perform a second curing step at a second temperature higher than the first temperature, thereby fully curing the adhesive composition so as to obtain a structural adhesive bond between the first and second parts, wherein the adhesive composition undergoes a second colour change.
摘要:
The present disclosure is directed to a precursor composition for a curable adhesive, the precursor comprising: a) a part (A) comprising: i. a first epoxy curing agent comprising at least one polyether amine and having an amine equivalent weight of at least 45 grams per mole of amine equivalents; ii. a second epoxy curing agent distinct from the first epoxy curing agent; iii. a metal nitrate catalyst; iv. optionally, a metal triflate catalyst; and b) a part (B) comprising: i. an epoxy resin; ii. a filler material; iii. an epoxy-based reactive diluent; and iv. optionally, a core-shell polymer toughening agent; and wherein the amount of filler material is selected such as to provide the part (B) with a hysteresis area of at least 30 Pa x 1/s, when measured at 23°C according to the test method described in the experimental section. The compositions of the present disclosure are particularly suitable for use in structural bonding applications, in particular for adhesively bonding small parts in manufacturing operations in aeronautic and aerospace industries. The present disclosure also relates to method of using such epoxy resin based curable compositions.
摘要:
In one aspect of the present disclosure, there is provided an adhesive precursor, comprising a first part (A) comprising: a first epoxy curing agent comprising at least one polyether amine and having an amine equivalent weight of at least 55 grams per mole of amine equivalents; a second epoxy curing agent distinct from the first epoxy curing agent and/or a secondary curative; a metal salt catalyst; a toughening agent; optionally, at least one phosphorous-based first flame retardant; optionally, at least one second flame retardant distinct from the at least one first flame retardant; and
a second part (B) comprising: a first epoxy resin; and/or a second epoxy-based resin distinct from the first epoxy resin; at least one phosphorous-based first flame retardant; optionally, at least one second flame-retardant distinct from the at least one first flame retardant; an epoxy-based reactive diluent; a core-shell polymer toughening agent; and optionally, a filler material;
wherein the total amount of flame retardant is lower than 50 wt.-% of the total curable adhesive precursor.
摘要:
In one aspect of the present disclosure, there is provided a sealant precursor, comprising a first part (A) comprising (a1) an epoxy curing agent having an amine equivalent weight of at least 150 grams per mole of amine equivalents; (b1) a first epoxy curative;
a second part (B) comprising (a2) a blend of epoxy resins comprising at least one bisphenol A epoxy resins and at least one bisphenol F epoxy resin; (b2) at least one silicone-based resin comprising epoxy functionalities; (c2) optionally, a toughener.
摘要:
In one aspect of the present disclosure, there is provided an adhesive precursor, comprising a first part (A) comprising: a first epoxy curing agent comprising at least one polyether amine and having an amine equivalent weight of at least 55 grams per mole of amine equivalents; a second epoxy curing agent distinct from the first epoxy curing agent or a secondary curative; a metal salt catalyst; and optionally, a toughening agent;
a second part (B) comprising: a first epoxy resin; a second epoxy-based resin distinct from the first epoxy resin; at least one phosphorous-based first flame retardant; a core-shell polymer toughening agent; optionally an epoxy-based reactive diluent; and optionally, a filler material;
wherein the total amount of the flame retardant system is lower than 25 wt.-% of the total curable adhesive precursor.