| HS Code | 110531 |
| Backingmaterial | Glass cloth |
| Adhesivetype | Silicone |
| Tapetype | Pressure sensitive |
| Totalthickness | 10 mil |
| Color | White |
| Tensilestrength | 100 lb/in |
| Elongation | 10% |
| Adhesiontosteel | 45 oz/in |
| Dielectricstrength | 500 V/mil |
| Operatingtemperaturerange | -100°F to 500°F |
| Flameretardant | Yes |
| Length | 36 yd |
| Corediameter | 3 in |
As an accredited Saint-Gobain CHR 2915-10 Glass Cloth Backing Silicone Adhesive Pressure Sensitive Tape factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Saint-Gobain CHR 2915-10 tape is supplied on 36-yard rolls, individually packaged, with 12 rolls per carton. |
| Container Loading (20′ FCL) | 20′ FCL loaded with Saint-Gobain CHR 2915-10 glass cloth backing silicone adhesive pressure-sensitive tape, palletized and secured for transport. |
| Shipping | Saint-Gobain CHR 2915-10 Glass Cloth Backing Silicone Adhesive Pressure Sensitive Tape is non-hazardous and not regulated for transport by DOT, IATA, or IMDG. Ship via standard ground, air, or ocean freight in sealed cartons. Store dry, away from extreme temperatures and contamination. No special labels or placards required. |
| Storage | Store in a cool, dry, well-ventilated area away from direct sunlight, heat, ignition sources, and oxidizing materials. Keep in original sealed packaging, upright, and clean. Maintain temperatures between 15–27°C (59–80°F) and relative humidity around 40–60%. Avoid moisture, dust, and heavy stacking. Rotate stock using FIFO to preserve shelf life. |
| Shelf Life | Shelf life is 18 months from date of manufacture when stored in original packaging at 70°F (21°C) and 50% relative humidity. |
Saint-Gobain CHR 2915-10 is applied as a single-ply mask on threaded bores, machined bearing shoulders, and masked datum edges before electrostatic deposition in conveyorized powder coating lines for architectural aluminium extrusions and automotive steel brackets. Tape add-on coverage is calculated at 1.2× the feature surface area for circular bores and 3 mm peripheral bleed allowance for flat flanges, with adjacent strips overlapped 50% to create an effective 0.508 mm double layer at the seam. The downstream process includes a phosphate pretreatment stage, a drying oven at 120 °C, an electrostatic spray booth operating at 60–80 kV, and a gas-fired convection cure oven held at 200 °C for 15 min. Removal is initiated only after the part surface cools to 70 °C, and the tape is pulled at a 180° peel angle to minimise cohesive splitting of the silicone adhesive. Industry compliance for the coated article is verified against Qualicoat 3.0 and AAMA 2605-20 film performance requirements, while tape residue is evaluated by visual inspection under 1000 lux lighting and, where specified, by cross-cut adhesion testing according to ISO 2409:2020. Terminal products include architectural aluminium profiles, automotive engine brackets, electrical enclosure panels, and construction hardware. Published data for this specific configuration is limited because the rate of silicone adhesive transfer depends on substrate finish, oven residence time, and powder chemistry.
Turbine blade shroud refurbishment places the glass cloth/silicone tape at the boundary between the dovetail cooling-passage land and the plasma-sprayed surface. Saint-Gobain CHR 2915-10 is applied as 10 mm perimeter strips, with a 50% overlap at the corners; this yields an add-on ratio of 0.508 mm effective thickness at corner transitions, while flat runs remain single-ply 0.254 mm. The critical process conflict is that the tape edge must resist mechanical lift from rebound of 60 mesh brown fused alumina blasted at 0.4 MPa, yet the same edge must separate without cohesive adhesive failure when the yttria-stabilized zirconia topcoat has cooled to 50 °C. Grit-blast preconditioning is followed by a NiCrAlY bond coat and a YSZ topcoat applied with an automated plasma gun at particle velocities exceeding 600 m/s and bond-coat preheat temperatures near 150 °C. The glass cloth backing is specified because it does not generate brittle char that can contaminate the spray booth, but char-free removal is verified after each cycle. Surface preparation quality is controlled under ISO 8503-2:2012 for grit profile and ISO 14922-1:1999 for thermal spray quality management; some overhaul shops add SAE AMS 2447 coating requirements. Terminal products include turbine blades, combustion liners, nozzle guide vanes, and industrial gas turbine seal housings. Published data for edge-lift behaviour at blast angles above 30° from the surface normal remains limited, so production validation with the exact robot torch path is required.| Application segment | Primary standard | Measured property | Exposure or test condition |
| Powder coating mask | AAMA 2605-20, ISO 2409:2020 | Film performance, cross-cut adhesion after tape removal | 200 °C, 15 min cure; removal at 70 °C |
| Thermal spray mask | ISO 8503-2:2012, ISO 14922-1:1999 | Grit profile, thermal spray quality management | 0.4 MPa alumina blast; plasma plume velocity |
| Electrical coil taping | ASTM D1000-10, IEEE 43-2013, UL 510 | Tape physical properties, insulation resistance, flame resistance | 150–180 °C VPI cure |
| Web splicing | ISO 29862:2018, PSTC-101 | Peel adhesion on steel | 150 °C, 300 m/min line speed |
| Engine harness protection | SAE AS50881 | Harness installation and retention | 180 °C, 60 min oven |
| Composite tool masking | ISO 2409:2020, ASTM D2734-23 | Tool cross-cut, cured part void content | 180 °C, 0.7 MPa, 2 h autoclave |
Half-lap taped end windings in traction motor and generator repair are subjected to vacuum-pressure impregnation after Saint-Gobain CHR 2915-10 is applied over mica paper and varnish-treated coil surfaces. The tape add-on structure is a half-lap winding at 50% overlap, producing 0.508 mm effective double-layer thickness; application tension is kept at 2–4 N/cm width to avoid cutting into the mica paper and to maintain a uniform resin path during epoxy impregnation. The downstream process includes oven preheat at 80 °C, vacuum draw below 5 mbar, epoxy resin transfer, and cure at 150–180 °C for 6–10 h. Because the silicone adhesive can release low-molecular-weight siloxanes during preheat, compatibility with the epoxy VPI resin must be confirmed by a representative coupon test before production; this limitation is particularly relevant for encapsulated stators where siloxane contamination on the slot wall may reduce resin adhesion. Industry compliance is anchored to ASTM D1000-10 for tape physical properties, IEEE 43-2013 for insulation resistance of the finished coil, and UL 510 for flame resistance of the tape; thermal endurance follows IEC 60034-18-1. Terminal products include traction motors, alternators, mining haul-truck generators, and industrial servo motors. Published data for partial discharge inception in this specific tape-wound configuration is limited and is strongly influenced by void content in the VPI resin rather than by the tape itself.
When a roll change splice must survive a three-zone hot-air drying oven at 150 °C and line speeds up to 300 m/min, Saint-Gobain CHR 2915-10 is applied as a butt splice with a single 25 mm wide strip, giving 12.5 mm bonding width on each web end. Splice area add-on is therefore one tape layer 0.254 mm thick, with the web butt joint centred under the tape. The downstream process includes core-splice preparation on an automatic festoon splice table, web tension maintained at 150 N/m, and passage through a three-zone hot-air oven where the silicone adhesive must not soften enough to allow web slippage at the highest zone temperature. Peel adhesion of the tape is evaluated according to ISO 29862:2018, and unwind and adhesion characteristics are compared under PSTC-101. Terminal products include silicone release papers, double-sided adhesive label stock, coated films, and abrasive sheet backing. Published data for this specific splice configuration is limited to line trial results because spliced web behaviour depends on web tension, oven air impingement, and roller wrap angle.| Scenario | Tape add-on structure | Peak process temperature | Removal temperature | Principal limitation |
| Powder coating mask | 50% seam overlap; 0.508 mm double layer at seams | 200 °C | 70 °C | Adhesive transfer on zinc-phosphate steel |
| Thermal spray mask | 10 mm perimeter strips; 0.508 mm at corners | 150 °C preheat plus plasma plume | 50 °C | Edge lift under grit rebound |
| Electrical coil taping | 50% half-lap; effective 0.508 mm | 150–180 °C VPI cure | Not removed | Siloxane compatibility with epoxy |
| Web splicing | 25 mm single strip; 12.5 mm per web end | 150 °C oven zone | Not removed | Web slippage at high tension |
| Engine harness protection | 50% spiral wrap; effective 0.508 mm | 180 °C paint oven; 260 °C local heat gun | 60 °C after cooling | Silicone transfer to polyester sleeving |
| Composite tool masking | Single ply 0.254 mm; 0.508 mm at corner overlaps | 180 °C, 0.7 MPa, 2 h | 60 °C | Resin bleed under vacuum bag |
Masking engine harness bundles and hydraulic hoses during paint touch-up and thermal deburring requires a tape that does not shrink, delaminate, or transfer silicone to braided polyester sleeving. Saint-Gobain CHR 2915-10 is applied in a spiral wrap with 50% overlap, yielding an effective double layer of 0.508 mm and a tie-wrap retention interval of 100 mm along the bundle. Downstream, harness assemblies pass through a paint booth and a forced-air cure oven at 180 °C for 60 min, then are subjected to airflow from a manually operated heat gun at 260 °C for localised thermal deburring. The tape must remain dimensionally stable and must not leave adhesive residue after the harness cools to 60 °C. Compliance for harness installation is evaluated under SAE AS50881, and removal residue is checked by tactile and visual inspection under 1000 lux magnification before final acceptance. Terminal products include engine harness assemblies, landing gear cable bundles, and fuselage wireway mock-ups. Published data for this exact masking configuration is limited, particularly for adhesion retention after cyclic exposure to solvent-based paint overspray and oven air flow.
Carbon-fibre-reinforced polymer part fabrication uses Saint-Gobain CHR 2915-10 on tool flanges and vacuum bag sealing surfaces to prevent epoxy resin bleed from bridging the tool edge and the bag seal. The tape is laid as a single ply along the flange, with 50% overlap at corners and a 3 mm setback from the part boundary; this creates an add-on barrier of 0.254 mm on flat flange runs and 0.508 mm at corner overlaps. Downstream, the tool is placed into an autoclave and cured at 180 °C and 0.7 MPa for 2 h; the silicone adhesive remains in contact with aluminium or invar tooling during the cure, and the tape is removed after the part cools to 60 °C. The glass cloth backing resists autoclave pressurisation and does not generate fibrous debris that might be trapped in the vacuum-bagged layup. Industry compliance for the tooling surface is verified by ISO 2409:2020 cross-cut before tool release agent application, and cured part porosity is assessed under ASTM D2734-23; the tape itself is not part of the final component. Terminal products include CFRP spars, fan cowl panels, and propeller blades. Published data for this specific tooling mask is limited because resin bleed behaviour depends on tool geometry, bag-side bleeder configuration, and release agent selection.
Competitive Saint-Gobain CHR 2915-10 Glass Cloth Backing Silicone Adhesive Pressure Sensitive Tape prices that fit your budget—flexible terms and customized quotes for every order.
For samples, pricing, or more information, please contact us at +8618005193850 or mail to sales8@ascent-chem.com.
We will respond to you as soon as possible.
Tel: +8618005193850
Email: sales8@ascent-chem.com
Flexible payment, competitive price, premium service - Inquire now!
Saint-Gobain CHR 2915-10 Glass Cloth Backing Silicone Adhesive Pressure Sensitive Tape is a single-sided, high-temperature electrical insulation tape in which a woven electrical-grade glass cloth carrier is coated with a cured silicone pressure-sensitive adhesive. The product code suffix “-10” corresponds to a nominal total thickness of 0.254 mm (0.010 in) within the CHR 2915 series. The tape is supplied as a self-wound log roll; standard widths range from 6.35 mm (0.25 in) to 914 mm (36 in), and the standard roll length is 32.9 m (36 yd). Because the backing is woven fabric rather than cast film, edge tear resistance and conformability over slot edges and lead break-outs are higher than for film-backed pressure-sensitive tapes. The silicone adhesive extends the upper continuous operating temperature to 200 °C, with intermittent exposure tolerance to 260 °C for short dwell cycles. Thermal failure is governed by oxidative embrittlement of the silicone mass and possible degradation of the glass sizing rather than by melting of the carrier. Published data for this specific configuration is limited to the manufacturer’s technical data sheet; values reproduced here are representative of the CHR 2915 series and should be confirmed against the batch certificate of analysis.
Within the CHR 2915 series, the 0.010 in (0.254 mm) build differs from CHR 2915-5 primarily in dielectric and mechanical reserve. The heavier glass cloth raises machine-direction tensile strength to approximately 30.7 N/mm (175 lb/in) and dielectric breakdown to approximately 4,000 V when tested in air according to ASTM D149-20. CHR 2915-5, at nominally 0.127 mm (0.005 in), is preferred where space claim is restricted or where lower bending stiffness is required; it provides proportionally lower voltage withstand and tensile strength. Selection between the two is therefore determined by slot fill, voltage margin, and abrasion load, not solely by adhesive performance.
The silicone pressure-sensitive adhesive on CHR 2915-10 retains a measurable fraction of room-temperature peel strength after short-dwell exposure at 200 °C, whereas conventional acrylic PSAs generally lose adhesion and become brittle above 120–150 °C after repeated cycling. This distinction is critical in motor coil and transformer lead-out wrapping where the tape must survive baking or impregnation without lifting at the overlap. Polyimide-film silicone tapes offer higher dielectric strength per unit thickness and a smoother surface, but their thin film is more easily punctured by sharp core steel edges. Glass cloth gives CHR 2915-10 higher tensile strength and abrasion resistance at equal total thickness, with better conformability over irregular coil surfaces. Rubber-adhesive glass cloth tapes may provide higher room-temperature tack, but they are not suitable for continuous service above 105 °C. Silicone adhesive also releases more consistently from copper and steel after thermal exposure, although initial tack on low-surface-energy substrates is lower than rubber or acrylic systems.
| Property | Test method | Representative value |
|---|---|---|
| Total tape thickness | ASTM D3652-16 | 0.254 mm (0.010 in) |
| Backing | — | Woven electrical-grade glass cloth |
| Adhesive | — | Cured silicone pressure-sensitive adhesive |
| Adhesion to steel | ASTM D3330 / D3330M-04 | 2.7 N/10 mm (25 oz/in) |
| Machine-direction tensile strength | ASTM D3759 / D3759M-05 | 30.7 N/mm (175 lb/in) |
| Elongation at break | ASTM D3759 / D3759M-05 | 7% |
| Dielectric breakdown in air | ASTM D149-20 | 4,000 V |
| Maximum continuous service temperature | Manufacturer thermal rating | 200 °C |
| Intermittent exposure | Manufacturer thermal rating | 260 °C |
The adhesion value is a 180° peel measurement on stainless steel at 23 °C and 50% relative humidity after a 24 h dwell. Tensile and elongation values are machine-direction data; cross-machine values may be lower because of fabric anisotropy. The single-layer dielectric breakdown value should not be used as a design withstand for wrapped coils. Partial discharge, creepage distance, and layer-to-layer voltage grading dominate in high-voltage insulation systems.
On production-scale motor coil taping lines, CHR 2915-10 is applied as a containment wrap before vacuum-pressure impregnation. Taping heads are typically equipped with closed-loop tension spindles set at 2–4 N per 25 mm width. If unwind tension exceeds 4 N, the glass weave can neck down and the adhesive can flow out at the slit edge. Application is normally half-lap or butt-lap, with overlap held to 0.5–1.0 mm on straight sections. The wrapped coil enters an epoxy or unsaturated polyester VPI process at 60–80 °C and 3–5 bar; during resin gelation, the tape functions as a mechanical constraint, not as the primary groundwall insulation. Successful processing requires that underlying mica, enamel, or steel surfaces be free of silicone oil, plasticizer, and amine-based release agents. Low-molecular-weight amines can alter the cure state of the silicone pressure-sensitive adhesive at the bond line and reduce tack; this is a frequently observed field failure mode when amine-containing mold release agents are used upstream.
In high-voltage coil end-winding consolidation, CHR 2915-10 is used as an overwrap over mica tape layers. The dielectric grading system relies on the mica groundwall; the glass cloth tape contributes mechanical restraint and moderate dielectric strength but is not a substitute for the mica insulation. The single-layer dielectric strength is measured in air; when multiple half-lap layers are wound over an end-winding, withstand voltage does not scale linearly because of entrapped air pockets and field enhancement at each overlap edge.
Peel adhesion of CHR 2915-10 to stainless steel is typically 2.7 N/10 mm (25 oz/in) when measured by ASTM D3330. On low-surface-energy substrates below 30 mN/m, such as untreated polypropylene or silicone rubber, initial peel strength can fall below 1.0 N/10 mm unless the surface is prepared. Wiping with isopropyl alcohol or naphtha removes plasticizer bloom but does not increase surface energy; corona or plasma treatment to 40–50 mN/m is required for thermoplastic films. For silicone rubber, the silicone adhesive can build bond strength over time, but residual silicone oils from processed gaskets must be removed by wiping with a 70:30 isopropanol/water mixture and drying at 60 °C for 10 min. On copper, the alkalinity of certain oxide passivation baths can attack the silicone adhesive during long dwell times; the tape should not be left as a temporary wrap on bare copper for more than 30 days at elevated humidity.
Converting CHR 2915-10 from master rolls to slit rolls requires shear-cut equipment rather than razor slitting when edge quality is critical. The glass fibers are abrasive; tungsten carbide or ceramic-edged shear blades are specified to hold a burr level below 0.025 mm per edge. Rotary slitting speeds of 50–100 m/min are used for woven glass cloth silicone tapes, with web tension held between 3–5 N per 25 mm width. Higher tension causes the fabric to distort and creates a curved tape that will not lay flat on a coil slot. On taping heads with a 25 mm wide roll, the unwind brake should be set to 2–4 N to maintain fiber alignment. Published production-scale data for this specific configuration is limited; the stated parameters are representative of silicone adhesive woven glass cloth behavior and should be confirmed by a converting trial on the target slitter.
In powder coating operations, CHR 2915-10 is used to mask threaded holes, bearing seats, and electrical contact areas through cure ovens operating at 180–220 °C for 15–30 min. A single cure cycle typically leaves no carbonized adhesive residue when the tape is removed below 80 °C; removal at elevated temperature increases cohesive failure risk and can transfer silicone residue. Multiple cycles above 200 °C progressively harden the adhesive and shorten clean removal life. In plasma spray booths where surface temperatures can exceed 260 °C, the glass cloth may survive short exposure, but adhesive degradation and fuming limit the product to temporary masking rather than continuous operation.
Compared with PTFE-coated glass cloth tapes, CHR 2915-10 does not provide a low-friction release surface for sliding contact or mold release. The silicone adhesive is the exposed functional layer in the assembled form, whereas PTFE-coated glass cloth is commonly used as a facing or separator. Selection therefore depends on whether the application demands adhesion to the substrate or release from process media. In heat-sealing jaw wraps, a non-adhesive PTFE-coated glass cloth is generally preferred; CHR 2915-10 is used where the tape must remain adhered to the coil, bar, or harness under vibration.
This product is not recommended for immersion in toluene, xylene, chlorinated solvents, or gasoline, because the silicone mass swells and loses peel strength. If solvent wiping is required before application, use isopropyl alcohol or naphtha in a ventilated area and allow the surface to dry completely. Storage should be maintained at 20–25 °C and 45–55% relative humidity with the roll suspended on its core; prolonged side pressure or high humidity can cause the glass cloth to absorb moisture and reduce dielectric margin before application.