1H-Pyrrole-2,5-Dione, 1,1'-((1-Methylethylidene)Bis(4,1-Phenyleneoxy-4,1-Phenylene))Bis-

1H-Pyrrole-2,5-Dione, 1,1'-((1-Methylethylidene)Bis(4,1-Phenyleneoxy-4,1-Phenylene))Bis-


    • Product Name 1H-Pyrrole-2,5-Dione, 1,1'-((1-Methylethylidene)Bis(4,1-Phenyleneoxy-4,1-Phenylene))Bis-
    • Alias Bisphenol A bismaleimide
    • Einecs 500-1207-0
    • Mininmum Order 1g
    • Factory Site West Ujimqin Banner, Xilingol League, Inner Mongolia, China
    • Price Inquiry sales9@bouling-chem.com
    • Manufacturer Bouling Chemical Co., Limited
    • CONTACT NOW
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    Specifications

    HS Code

    778636

    Chemical Formula C36H28N2O6
    Molar Mass 600.62 g/mol
    Appearance Typically a solid (description may vary)
    Physical State At Room Temp Solid
    Solubility In Water Low solubility (qualitative, exact data may vary)
    Solubility In Organic Solvents May dissolve in some organic solvents like dichloromethane, details vary
    Melting Point Data may vary, requires experimental determination
    Stability Stable under normal conditions, may decompose under extreme conditions

    As an accredited 1H-Pyrrole-2,5-Dione, 1,1'-((1-Methylethylidene)Bis(4,1-Phenyleneoxy-4,1-Phenylene))Bis- factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing 1 kg of 1H - Pyrrole - 2,5 - Dione compound packaged in a sealed chemical - grade container.
    Shipping The chemical "1H - Pyrrole - 2,5 - Dione, 1,1'-((1 - Methylethylidene)bis(4,1 - Phenyleneoxy - 4,1 - Phenylene))bis-" should be shipped in properly sealed, corrosion - resistant containers, following all hazardous chemical shipping regulations to ensure safety during transit.
    Storage 1,1'-((1 - Methylethylidene)bis(4,1 - phenyleneoxy - 4,1 - phenylene))bis - 1H - pyrrole - 2,5 - dione should be stored in a cool, dry place, away from direct sunlight. Keep it in a well - sealed container to prevent moisture absorption and contact with air, which could potentially lead to degradation. Store it separately from incompatible substances, such as strong oxidizing agents.
    Application of 1H-Pyrrole-2,5-Dione, 1,1'-((1-Methylethylidene)Bis(4,1-Phenyleneoxy-4,1-Phenylene))Bis-

    What Limits Signal Integrity in Millimeter-Wave Substrates Beyond 30 GHz?

    The propagation velocity of a signal through a laminate is irreversibly degraded by dielectric loss factors exceeding 0.005 at 10 GHz, a threshold that disqualifies conventional FR-4 and many mid-range epoxies from 5G New Radio and automotive radar platforms. The bismaleimide monomer 2,2-bis[4-(4-maleimidophenoxy)phenyl]propane functions as a hard-modifier in cyanate ester and BT (bismaleimide-triazine) resin matrices, where its sterically rigid bisphenol-A bridged diphenoxy architecture suppresses dipole relaxation without introducing the excessive moisture uptake observed in unmodified cyanate esters. In a typical low-loss laminate formulation, the BMI constituent represents 15–40 wt% of the total resin solids, blended with bisphenol-A dicyanate at a mass ratio between 80:20 and 50:50, and further loaded with fused silica filler at 30–60% by weight to reduce the coefficient of thermal expansion below 40 ppm/°C in the z-axis. Varnish mixing is executed in dimethylformamide or methyl ethyl ketone at 25–35% non-volatile content, followed by vertical treater impregnation of 1078 or 2116 E-glass fabric; forward velocity and zone temperatures are calibrated such that B-stage resin advancement reaches a pre-cure conversion of 15–25% as measured by differential scanning calorimetry (ISO 11357-5:2013), with residual volatile content held below 0.5 wt%. Stack-up assembly of eight-ply or ten-ply layups proceeds under cleanroom Class 10,000 conditions before the book is transferred to a multi-opening hydraulic press where a stepped thermal lamination cycle is applied: ramp at 3–5 K/min to 200 °C under contact pressure, dwell for 60 min with a specific pressure of 2.5–4.0 MPa (hydraulic gauge), then post-baked unrestrained in an air-circulating oven at 240 °C for 120 min to complete oxazoline-to-triazine ring formation and drive residual maleimide homopolymerization beyond 95% conversion. The cured laminate must satisfy IPC-4101E /99 or /102 slash sheet requirements, with qualification testing per IPC-TM-650 2.5.5.9 (relative permittivity and loss tangent at 10 GHz via split-post dielectric resonator) yielding a Dk of 3.0–3.4 and a Df of 0.0025–0.0045. When such laminates are paired with ultra-low-profile electrodeposited copper foil and processed into PCB inner-layers through a subtractive etch regime, the finished substrate is specified for phased-array antenna boards operating in the 28 GHz and 39 GHz bands defined by 3GPP Release 17, where circuit impedance tolerance must remain within ±5% of nominal across the -40 to +125 °C operating envelope.
    Comparative Dielectric Data for Resin Systems in Millimeter-Wave Laminates (Typical Qualification Values at 10 GHz, IPC-TM-650 2.5.5.9)
    Resin SystemDkDfMoisture Absorption (ASTM D570, %)
    BMI-Cyanate Ester (30 wt% BMI)3.20.00350.6
    BT Resin (unfilled)3.50.00420.8
    High-Tg FR-4 (180 °C Tg)4.20.0151.5
    PTFE-Ceramic Composite2.80.00200.1
    The injection of a one-part bismaleimide resin formulation into a heated closed mold containing a near-net-shape carbon fiber preform demands a viscosity window of 0.1–1.0 Pa·s sustained for ≥45 min at injection temperatures between 90 °C and 120 °C, a constraint that excludes high-molecular-weight polyimide precursors and forces reliance on the low melt enthalpy of 2,2-bis[4-(4-maleimidophenoxy)phenyl]propane when co-reacted with a reactive diluent such as o,o′-diallyl bisphenol A (DABPA) at a stoichiometric ratio of 1.0:0.8 mol/mol maleimide to allyl functionality. The mixed resin is degassed under 5 mbar vacuum prior to transfer into the pressure pot of a twin-component RTM injection unit, where it is forced at 0.3–0.7 MPa injection pressure through a heated static mixer and a distribution runner into a tool cavity preheated to 160–180 °C; the tooling incorporates peripheral vacuum ports that maintain 10–20 mbar absolute pressure during the fill phase to prevent void nucleation. The preform, composed of 12K high-strength carbon fiber tows conforming to the fiber architecture specified in SAE AMS 3961/3, is compacted to a fiber volume fraction of 57±3% and held under controlled cavity pressure during the fill-bleed cycle so that the advancing flow front is monitored by in-mold dielectric sensors triggering a pressure-lock when the fill reaches the predefined vent line. After gelation at 180 °C for 60 min, the integrally cured part is demolded directly into a free-standing post-cure rack where the laminate undergoes a ramped thermal program: 200 °C/2 h + 230 °C/2 h + 260 °C/4 h in a nitrogen-purged oven with a ≤2 % oxygen atmosphere to avoid oxidative surface degradation. Compliance with ASTM D3531/D3531M-16 for carbon fiber-reinforced plastic cure characterization is required, and finished components must pass ultrasonic C-scan inspection per ASTM E2580-17 with a ≤0.5% void content acceptance criterion. Failure mode analysis on production tools has shown that preform edge racetracking channels exceeding 1.5 mm width induce dry-spot formation because the resin front bypasses the main compaction zone; this necessitates tooling rework after 300–500 injection cycles on aluminum tools. The post-cured composite is then machined into outer bypass duct segments for high-bypass turbofan engines, where the continuous service temperature of 260 °C and the thermo-oxidative stability limit of 280 °C (defined by a 5% mass loss in 500 h per ASTM E1877-21) place the component outside the flight envelope of aluminum and standard-epoxy alternatives.

    BMI-Modified Phenolic Compounds in Wet Friction Clutches

    When automatic transmission fluid (ATF) temperatures reach 140 °C during repeated engagement cycles, the methylol bridges in unmodified phenolic binders undergo progressive hydrolysis that reduces the friction interface cohesion and shifts the dynamic-to-static friction ratio µds below 0.95, triggering shudder. The addition of 2,2-bis[4-(4-maleimidophenoxy)phenyl]propane powder to a novolac or resole phenolic at 10–25 phr (parts per hundred resin) establishes a semi-interpenetrating network during hot pressing because the maleimide ring opens at 170–200 °C and reacts with residual phenolic hydroxyls and free formaldehyde, forming thermally stable benzoxazine-like linkages and maleimide homopolymer domains that delay the onset of thermal degradation to above 320 °C as verified by thermogravimetric analysis under nitrogen per ASTM E1131. Compounding is performed in a plow mixer in which bismaleimide powder with a median particle size D50 of 15–25 µm is dry-blended with phenolic resin, aramid pulp, graphite, and friction modifiers for 20–30 min; the mixture is then dispersed onto a copper alloy core plate, cold compacted at 8–12 MPa, and hot pressed at 170 °C and 15–18 MPa for 90 s to achieve the final groove-patterned friction lining. The finished plate is subjected to an SAE J2488 high-energy friction test sequence in Dexron VI ATF, where the mid-cycle µ-coefficient must stay within a ±7% band of the target 0.130 set point, and the integrated shudder index per SAE J2490 must not exceed 150 N·s/m for typical 6-speed automatic transmission clutch packs. Post-mortem analysis of linings that survived 10,000 engagement cycles without delamination demonstrates that bismaleimide domains inhibit the propagation of binder-phase microcracks that would otherwise coalesce under the shear stress of 0.8–1.2 MPa present at the paper-to-steel interface.Capillary underfill encapsulants based on bismaleimide-modified epoxy matrices address a stress-relaxation gap that emerges in fine-pitch flip-chip assemblies when the glass transition temperature (Tg) of a conventional anhydride-cured epoxy falls below 125 °C, permitting rapid μBump fatigue during MSL3 reflow cycles. Pre-dispersion of 5–15 wt% of 2,2-bis[4-(4-maleimidophenoxy)phenyl]propane into a bisphenol-F diglycidyl ether monomer, followed by catalytic imidazole-level initiation prior to the addition of a methylhexahydrophthalic anhydride hardener, yields a single-component formulation that retains a flow viscosity of 2–6 Pa·s at 80 °C (measured per ASTM D3236 at 10 s⁻¹) for 8 hours of pot life. Application onto a bumped die with a 40 µm stand-off height is performed through a precision jet dispenser operating at a shot rate of 200 dots/s and a target fillet width of 1.8–2.2 mm; the assembly then passes through a multi-zone reflow oven where underfill cure is integrated into the reflow profile, with a hold step at 110 °C for 20 min followed by a ramp to 165 °C for 60 min. The resulting network exhibits a Tg of 155–170 °C by thermomechanical analysis (IPC-TM-650 2.4.24.4) and a coefficient of thermal expansion below 30 ppm/°C below Tg and 80 ppm/°C above Tg, which keeps the under-bump shear stress within acceptable limits when the package is subjected to 1,000 cycles of -55/+125 °C thermal shock per JEDEC JESD22-A106B. Qualification requires compliance with IPC-CC-830B for conformal coating material compatibility, and the void-free underfill fillet must pass C-mode scanning acoustic microscopy with a void area rejection threshold of 2%. The finished devices are ball-grid-array (BGA) packages in glass-fabric coreless substrates designed for automotive advanced driver-assistance system (ADAS) processors, where the junction temperature can briefly approach 150 °C during full-load operation and the underfill must not delaminate from the passivation layer after reflow at 260 °C peak.

    When Jet Engine Connector Housings Require Retention of Tensile Strength After 20,000 Hours at 300 °C

    Polyimide (PI) compression moldings based on PMR-15 formulations suffer from microcracking sensitivity because the nadic end-cap curing creates a crosslink density that leaves the network excessively brittle at strain levels below 1.5%; introducing 20–40 phr of a thermoplastic-like BMI phase via the melt blending of 2,2-bis[4-(4-maleimidophenoxy)phenyl]propane with a stoichiometrically imbalance PI oligomer (molecular weight Mn targeted at 1,500 g/mol) introduces a dispersed domain morphology that absorbs crack-tip energy without substantial depression of the heat deflection temperature. Compounding proceeds in a co-rotating twin-screw extruder (L/D 40, screw diameter 25 mm) with barrel zone temperatures rising from 310 °C at the feed throat to 370 °C at the die; a vacuum vent at −0.08 MPa removes volatile imidization by-products. Pelletized alloy is injection molded into connector inserts and bushings using a mold temperature of 180–210 °C and an injection pressure of 140–170 MPa, with holding pressure profiles adjusted for the non-Newtonian power-law behavior of the melt. The molded components achieve a tensile strength retention of ≥70% after 20,000 h isothermal aging at 300 °C in air, as evaluated per ASTM D3045-18, and must demonstrate no visible surface crazing under 20× magnification when cross-sectioned after the same exposure. Thermogravimetric analysis per ASTM E1131 under nitrogen shows a 5% mass loss temperature of 520–540 °C for the alloy, compared to 490 °C for the unmodified PI control. Qualification for engine nacelle applications is benchmarked against the electrical insulation retention criteria of SAE AS81044 and the flammability index of ≤35 per ASTM D2863 at 28% oxygen concentration for the finished insulation sleeves.
    Key Qualification Standards for BMI-Containing Polyimide Alloy Connector Components
    TestStandardRequirement
    Isothermal TGA (air, 300 °C)ASTM E1877-21≤5% mass loss at 20,000 h
    Tensile strength after heat agingASTM D3045-18≥70% retention at 20,000 h
    Dielectric strength (short-time)ASTM D149-2015 kV/mm
    Flammability (limiting oxygen index)ASTM D2863-19LOI ≥28%
    Dimensional stability (linear shrinkage)ASTM D5516-180.1% after 2,000 h at 300 °C
    Outgassing (TML/CVCM)ASTM E595-15TML ≤1.0%, CVCM ≤0.1%
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    Certification & Compliance
    More Introduction

    Designated as BisM-BPAE-02 in commercial catalogues, 1H-Pyrrole-2,5-Dione, 1,1'-((1-Methylethylidene)bis(4,1-phenyleneoxy-4,1-phenylene))bis- is a bismaleimide monomer whose molecular backbone incorporates a bisphenol A-derived aromatic diether bridge. The empirical formula yields a molecular weight of 568.6 g/mol. The product is released as a crystalline powder with a faint yellow-to-amber hue, a melting range of 95–105 °C (differential scanning calorimetry, 10 °C/min under nitrogen), and a typical assay of ≥97% (HPLC area%, internal method aligned with ISO 13885). Residual solvent content is controlled below 0.3 wt%. The monomer is stabilized against spontaneous radical polymerization during transit through the inclusion of a proprietary free-radical inhibitor; consequently, storage at a controlled temperature of <25 °C in sealed, moisture-proof packaging is mandated. Pre-drying under vacuum at 50–60 °C for a minimum of 4 h is required whenever the product has been exposed to an ambient relative humidity exceeding 60%, as adsorbed moisture can accelerate premature gelation during subsequent thermal processing.

    Supplied as a micro-granulated powder in 25-kg high-density polyethylene pails containing integrated desiccant pouches, the material must be re-sealed under nitrogen after each withdrawal to prevent humidity ingress. A certificate of analysis is provided with each batch declaring the melt enthalpy, HPLC purity, and ash content (target <0.05%) per internal release specifications.

    What Structural Features Distinguish This Bismaleimide from MDABMI?

    4,4′-Bismaleimidodiphenylmethane (MDABMI) derives rigidity and a high melting point (156–158 °C) from two terminal maleimide rings directly coupled to a methylene-bridged diphenyl core. In BisM-BPAE-02, each maleimide is separated from the central isopropylidene unit by a flexible phenyleneoxy spacer. The extended ether linkages lower the rotational energy barrier, reducing the crystalline melting point by approximately 50–60 °C and dramatically improving solubility in common polar aprotic and ketone solvents. The cured network retains a stoichiometric maleimide density sufficient for high-temperature performance yet exhibits a measurable reduction in crosslink density, which translates into toughness gains relative to rigid MDABMI systems. A comparative data set is provided in Table 1. The values represent laboratory-characterized neat resin specimens cured with 2 wt% dicumyl peroxide (98% purity) under a standard cycle of 180 °C/2 h + 220 °C/4 h, unless otherwise noted.

    Table 1 — Comparative property summary for BisM-BPAE-02 and standard MDABMI.
    PropertyBisM-BPAE-02MDABMI
    Melting point (DSC peak, °C)95–105156–158
    Melt viscosity at 130 °C (ASTM D4440, Pa·s)0.5–2.0>10 (extrapolated)
    Solubility in acetone at 25 °C (wt%)>30<5
    Glass transition temperature after cure (ASTM E1640, DMA tan delta peak, °C)230–250290–310
    Fracture toughness KIC (ASTM D5045, MPa·m1/2)0.9–1.20.5–0.7

    Processing Parameters and Risk of Premature Gelation

    The monomer undergoes free-radical homopolymerization upon heating above approximately 140 °C, with the exothermic onset recorded by differential scanning calorimetry (ASTM E2041) typically falling between 160 °C and 180 °C at a ramp rate of 10 °C/min. The total reaction enthalpy exceeds 200 J/g, requiring careful thermal management in large-scale mixing equipment. Parallel-plate rheometry (ASTM D4440) reveals a deep melt-viscosity minimum of 0.15–0.4 Pa·s in the region of 110–130 °C; however, the processing window between full melting and the onset of irreversible viscosity rise is narrow—typically 8–12 min at 150 °C before the complex viscosity surpasses 10⁴ Pa·s. On a twin-screw extruder with an L/D ratio of 20:1, barrel temperatures must be profiled to maintain the melt temperature within ±3 °C of the set point; excursions beyond this band generate high-molecular-weight fractions that can cause pressure spikes at the die and visible surface defects in the extrudate. For hot-melt prepreg impregnation, the melt is maintained under a vacuum of less than 10 mbar to eliminate entrapped volatiles without triggering premature advancement. Use of primary or secondary amine-based curatives must be avoided: nucleophilic attack on the maleimide double bond leads to uncontrolled Michael-addition crosslinking that completely collapses the thermal latency of the formulation. Peroxide initiators such as dicumyl peroxide at 1–3 phr are preferred for controlled chain-extension prior to gelation.

    When Post-Cure Cycles Exceed 250 °C in Air

    The inherent oxidative stability of the bismaleimide network is sufficient to deliver a 5% weight-loss temperature of 380 °C when characterized by thermogravimetric analysis in air (ASTM E1131, 20 °C/min). However, sustained exposure to temperatures beyond 250 °C in an oxygen-containing environment initiates surface carbonyl formation and microcracking, particularly in unreinforced resin plaques. Accelerated aging tests conducted at 260 °C over 1000 h show a progressive increase in the intensity of the 1715 cm⁻¹ carbonyl band as monitored by attenuated total reflectance FTIR spectroscopy. Incorporation of a hindered phenolic antioxidant at 0.5 phr has been demonstrated on analogous bismaleimide ether systems to extend the onset of oxidative embrittlement by approximately 40% under identical conditions (ISO 11358 guidelines followed for isothermal TGA). The flexural modulus retention after 500 h at 250 °C in circulating air, measured per ASTM D790, drops below 80% for unstabilised castings, whereas a stabilised formulation maintains values above 92%. Consequently, any application demanding continuous service above 250 °C in an oxidative atmosphere must incorporate an antioxidant package validated for the specific part geometry and air-flow exposure.

    Adhesive Formulations for Titanium Honeycomb Panels

    BisM-BPAE-02 is utilized as the primary resinous component in high-temperature structural film adhesives intended for titanium honeycomb sandwich assemblies in aerospace thrust-reverser structures. The monomer is blended with a low-viscosity diallylbisphenol A comonomer and a free-radical initiator to produce a B-staged film that exhibits controlled flow during cure. Lap shear specimens bonded to Ti-6Al-4V adherends prepared by chromic acid anodization, and cured under vacuum-bag pressure at 180 °C for 2 h followed by a free-standing post-cure at 220 °C for 4 h, generate single-lap shear strength values of 22–26 MPa at 23 °C (ASTM D1002). After thermal aging for 1000 h at 232 °C in circulating air, the retained lap shear strength remains above 70%, with cohesive failure observed in the adhesive layer rather than interfacial debonding. Film areal weights between 150 g/m² and 300 g/m² are achievable using solvent-cast deposition on release paper, and the tack-and-drape characteristics remain adequate for hand lay-up of complex core geometries provided the film is stored at −18 °C until use. Pre-bond moisture conditioning at 50 °C/95% RH for 72 h results in a less than 10% reduction in hot-wet lap shear strength at 180 °C, which meets the service requirements of major airframe original equipment manufacturers.

    Rheokinetic Modelling of Minimum Viscosity Window

    Isothermal curing kinetics of BisM-BPAE-02 can be described by the Kamal-Sourour autocatalytic model, requiring parameters obtained from multi-heating-rate DSC scans over a range of 140–200 °C. The kinetic triplet—activation energy of approximately 80–85 kJ/mol, pre-exponential factor, and reaction orders m and n—derived for closely related bismaleimide ether systems is applicable as a first approximation, though published data for this specific monomer remains limited. Coupling the kinetic expression with the Castro-Macosko chemorheological model permits a prediction of the isothermal viscosity profile once the monomer’s zero-shear viscosity Arrhenius coefficients are determined (typical flow activation energy 55–65 kJ/mol). Under a standard isothermal molding condition of 150 °C, the predicted gel point (defined as the time at which the complex viscosity reaches 10⁴ Pa·s) falls within a 10–14 min envelope, aligning with the rheometric observations. These models are implemented in proprietary process simulation software to define the permissible injection window for resin transfer molding (RTM) tools. A sensitivity analysis reveals that a 2 °C increase in tool temperature shortens the gel time by approximately 1.5 min, underscoring the necessity of active multi-zone temperature control on RTM presses. The narrow processing latitude effectively excludes this monomer from low-cost open-mold processes where thermal gradients routinely exceed 5 °C across the part.