CA1118948A - Intumescent fireretardant composites - Google Patents

Intumescent fireretardant composites

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Publication number
CA1118948A
CA1118948A CA000301095A CA301095A CA1118948A CA 1118948 A CA1118948 A CA 1118948A CA 000301095 A CA000301095 A CA 000301095A CA 301095 A CA301095 A CA 301095A CA 1118948 A CA1118948 A CA 1118948A
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Canada
Prior art keywords
weight percent
sodium silicate
filler
fire retardant
composite material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA000301095A
Other languages
French (fr)
Inventor
Roger L. Langer
Richard R. Licht
Alan J. Marlor
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
3M Co
Original Assignee
Minnesota Mining and Manufacturing Co
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Filing date
Publication date
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Abstract

Abstract The disclosure relates to flexible heat expanding, fire retardant composite materials comprising an intumescent component in granular form, an organic binder component such as an elastomer, an organic char-forming component and fillers such as clay, silica, synthetic organic staple fibers or inorganic fiberglass or ceramic fibers. These composites when subjected to heat at about 110° C.. can intumesce up to ten times their original volume.

Description

- `
~ FN 913,565 INTUMESCENT FIRE RETARDANT COMPOSITES

Background of the Invention This invention relates to an intumescent fire retardant material, and particularly a material which has the ability to rema;n in the flexible unexpanded form, until heat, such as that produced by a fire, is applied, at which time it will expand to become a substantially rigid refractory thermal insulator.
Industry has long sought better materials to effectively fill voids left by burning or melting cable insulation as in the case of a fire in modern office buildings. Better thermal insulating coverings for walls, doors, ceilings, etc., are also needed. The materials heretofore employed provided protection for only limited periods because of poor stability at elevated temperatures ~ ;
or damage by high pressure water sprays due to low mechanical strength. They have had the ~urther disadvantage that they were not waterproof and had low volume expansions and pressure generation, particularly at low temperatures, with a resultant loss in their capacity to fill void areas or provide thermal insulation, thus allowing the spread of smoke or fire.
U.S. Patent 3,786,604 is illustrative of the prior art and discloses the concept of filling the gap between a concrete floor slab and an upright curtain wall with a urea formaldehyde resin foam which is supported in a trough made of thin resilient sheet steel. The steel trough support is required because the mechanical strength of the foam is relatively low and that of the charred foam is even lower.
U.S. Patent 3,429,836 discloses a process For producing thermal insulating coverings from organic -(polystyrene and copolymers of s~yrene) foam materials in combination with alkali metal silicates. The composition is made into rigid boards for use as thermal insulating covers on surfaces such as walls, ceilings, doors, and the like~ The foamed board-like material must be coated with a protective layer of lacquers or plastic films to render it moisture resistant.
U.S. Patent 3,983,082 relates to a silicone resin base fire retardant system having a temperature çapability to at least about 230C. and combines intumescent character-istics with a crusting and charring capability. These materials are intended primarily for use in aircraft gas turbine engines and they are most effective at relatively high temperatures on the order of 1000C. or higher.

Summary of the Invention The present invention relates to flexible heat expanding, fire retardant composite materials which have the capability of expanding up to ten times their original volume when exposed to heat. The composite materials are applied in sheet or putty form and remain in their flexible unexpanded state until such time as they are subjected to heat on the order of 100C., as in a burning building.
When thus heated, the composite materials read;ly intumesce to seal voids caused by burn;ng or melting material and provide seals against smoke, vapors, water, steam pressure and due to its refractoriness, protects against spread of fire from one area to another or from floor to floor. An added advantage provided by the unexpanded flexible fire retardant composites of the present invention, particularly in paste or putty form, resides in the provision of an elastomeric seal against vapors, smoke and even water , ., , ~ ,...... . . .. .

The invention may be generally defined as a dense, solid, flexible, heat expandable, fire retardant composite material capable of subsisting substantially indefinitely in sheet or putty form and having increased thermal insulating and sealing efficiency when exposed to temperatures above about 110C., and capable of expand-ing at least up to two times its original volume. The material consists essentially of about 15 to 80 weight percent of sodium silicate in granular form as the intumescent component, the individual sodium silicate granules each enlarging solely upon the application of heat; about 15 to 40 weight percent of a polychloroprene binder component; up to about 40 weight percent of a phenol-formaldehyde organic char-forming resin; and up to about 50 weight percent filler, said filler comprising up to about 20 weight percent active filler and up to about 40 weight percent inactive filler.

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Detailed Descriptlon of the Inventlon -The flexible heat expanding, fire retardant composite materials of ~he present invention can range from a soft putty-like consistency up to a hard rubber. This range of "hardness" is achieved by selectively varying the individllal components of the intumescent composite materials.
Useful materials are compounded to include, by weight, about 15 to 80% of an intumescent component such as a hydrated alkali metal silicate, 15 to ~0% of an organic binder component such as an elastomer which may also be a char-forming component,up to ~0% of an organic char-forming component such as a phenolic resin and up to 50% fillers such as granular inorganic materials, organic or inorganic fibers, vulcanization aids, plasticizers, etc.
The fillers utilized in the present invention can be classified as "active" and "inactive". The active fillers are either chemically and/or phys;cally reactive components and contribute to the "green" state characteristics of the intumescent composite materials of the present invention and include those fillers such as the plasticizers, vulcanization aids, blowing agents and solvents. The inactive fillers are inert materials, and include "active" fillers which may be present in excess, which are chemically unreactive and function during or after a fire as a refractory or endothermic material. The active fillers can comprise up to 20% by weight of the composite material and the inactive f;llers can be present up to 40% by weight, provided, however, that the total filler content of the composite materials does not exceed 50% by weight.
It has been found that an especially preferred alkali metal silicate is granular sodium silicate with particle sizes of from 0.2 r,~m. to 2.0 mm., i.e., with 95%

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of the particles being greater than 0.2 mm., a moisture content of 5 to 30% and an SiO2 and Na20 ratio of 2 to 3.75:1. In this connection, we have found that as the proportion of silica to alkali in the alkali metal silicate decreases, the rate of solution of the alkali metal silicate increases. For example, i~ all other factors remain the same, a sodium silicate having an SiO2:Na20 ratio o~ 2.0 will dissolve more rapidly than a sodium silicate having a 3.75 ratio. This rapid attack by water is detrimental from a long-term environmental stability and performance stand-point. Accordingly, materials having SiO2:Na20 ratios less than 2.0 have been found to be less than satisfactory.
Additionally, as the SiO2:Na20 ratio decreases, the refractoriness of the composite material also decreases and thus results in a material lacking stability when subjected to water and water sprays during a fire. Other hydrated alkali metal silicates such as potassium silicate can also be utilized to form fire retardant compositeSof the present invention prov;ded that the silica to alkali ratio is within the contemplated range.
It has been found that when about 80% of the particle sizes of the alkali metal silicate, e.g., sodium silicate, utilized in the composite material, was less than about 0.15 mm., the composite material when subJected to heat intumesced only slightly. In a comparative test, a composite material produced with sodium silicate having about 95% of the particle sizes greater than 0.2 mm. expanded to twice its original volume and the composite material produced with sodium silicate particle slzes less than 0.15 mm. had a volume expansion of only 0.5.

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~ ~ 8 ~ 8 Among the useful organic char-forming resins are phenolic resins, polycarbodiimide~ urea-formaldehyde and malamine formaldehyde which, when charred in combination with the other components, contribute to formation of a highly refractory composition.
Those fillers which may be added to the composites - of the present invention include quartz sand (silica), anti-oxidants, vulcanization aids, clay, fly ash, blowing agents, plasticizers, perlite~ vermiculite, inorganic fibers such as glass fibers and mineral wool and organic fibers.
Exemplary binder materials include char-forming elastomers such as chloroprene and acrylonitrile rubbers and non-char forming polymers such as chlorosul~onated polyethylene, polybutene and polysulfide polymers.
15In the examples which follow, flexible sheet mater;als as well as paste or putty-like materials were produced by standard forming procedures. These materials begin to intumesce at temperatures as low as 110C., and when heated to 600C. have volume expansions of at least
2, flexural strengths of at least 20 kg. per cm.2 and withstand temperatures greater than 1000C. In addition, these materials generate expansion pressures greater than :` 14 kg./cm.2 when tested in the Instron "Pressure Test".

Batching The following materials were prebatched by dry blending:
Ingredients Wt.%
B Neoprene W~ 25 ` Sodium Silicate -(Brites~jl H2~ 56 Phenolic Resin -~lVarcu~5485)11 Silica (Min-U-Si~ 8 ~ ` ~ tr~de r~ ks ~ 9 Compounding The above materials were charged to a Banbury mixer for compounding using the ~ollowing conditi~ns:
Step Comments 1 Charge all materials 2to a water cooled Banbury 2 Lower Ram - 3 kg./cm.
3 Raise Ram and sweep
4 Lower Ram
5 When temperature reaches 90C., raise Ram until temperature drops to 65C.
6 Lower Ram
7 Repeat steps 5-6 three times. On third time~
dump material and transfer to rubber mill.
Milling Mill material until material bands on mill. Set mill gap to desired thickness and sheet out material. The resulting sheet will be a flexible rubber like material which can be die cut to form the desired configurations.

TESTING ~.
The following tests were conducted on the above mater;al:
1. Expansion (X) at 600C. under weight where X =
Final Vol. - Int. Vol.
_ Int. Vol.
Test method: A 50 mm. diameter disk is die cut from the material and the volume and weight of the disk is determined.
The disk is set on a ceramic plate and a metal disk weighing 760 gm. is set on top of the material. The sample is then placed ;n a preheated kiln for 30 minutes at 600C. The sample is removed and weight and volume are determined.

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lllB9A~3 In addition to expansion, LOI, green bulk density, and fired bulk density are determined.
2. Low Temperature Expansion A sample is placed in an oven set at 120C. to determine if expansion takes place at low tempera-tures. This is a pass/fail test.
3. Strength MOR
(a) Test samples are prepared as follows:
The green material is cut into 50 mm. long x 13 mm. wide x 6 mm. thick bars. These bars are expanded under confinement at a kiln temperature of 600C. w;th a soak time of 30 minutes.
(b) The modulus of rupture is determined on an Instron strength testing machine. The method used is the MOR for a three-point load, and ~ ?
is calculated by: MOR = ~2, where P = load required to break bar L = span distance between outer supports b = width of bar d = depth of bar 4. Refractory Test Samples of the above material, 25 mm. x 50 mm. x 6 mm. are placed in a kiln at lO90~C. The samples ;~
are monitored for three hours. Failure is deter-mined by melting of the material within three hours.
5. Pressure Generation The pressure generated kg./cm.2 during expansion is determined by use of a free piston device. The piston is rested on a test sample which is heated.
The device was loaded at room temperature and placed in an Instron tester. The sample was heated to 230C. slowly, allowing the sample to generate pressure. Piston clearance is maintained to allow expansion gases to escape. Sample size was chosen to allow direct readout of kg./cm.2 on the Instron tester.
6. In addition to the above tests, the following standard tests were also performed:
NEL-PIA/MAERP Standard Method of Fire Test ASTM D-395 Compression Set-Method B
22 Hours at Room Temperature TEST RESULTS

Actual Test TEST Range All Compositions Results Expansion - X 2 - 10 2.46 LOI - % 20 - 60 30.9 r~
Green Density - gm./cc.1.0 - 1.65 ls48 Fired Density - gm.lcc. .05 - .5 .34 MOR - kg./cm.2 28 - 84 40 20 Refractory Pass/Fail Pass Pressure Generatîon kg./cm.2 >14 18 Low Temperature ExpansionPass/Fail Pass ASTM E-119-73 Pass/Fail Pass NEL-PIA/MAERP Pass/Fail Pass ASTM D-395 - X compression10 - 80 70 Shore "A" Durometer 35 - 95 83 A simulated firedoor test was ~nducted with ~he intumescent material of the example. A 17 guage steel ~rame measuring about 180 mm. x 215 mm. x 25 mm. was loaded with test material and set into a refractory brick assembly, then -B

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subjected to 815~C. produced by a propane burner. The first test (A) used two 20 mm. skyrofoam test panels. The second test (B) used two 20 mm~ styro~oam panels sandwiched between two 1.6 mm. Flexible firestop sheets. Temperatures were recorded on the hot and cold side using Chromel-Alumel thermocouples attached to the center of the frame and are shown below.
Time Minutes Hot Temperature (C.) Cold Temperature (C.) A B A B
8 690 760 100 65 Examination after 30 minutes revealed that the styrofoam panels ;
had been completely consumed whereas the intumescent fire retardant sheets had expanded and hardened into a rigid :
insulating material.

The following materials were batched and compounded according to the procedures of Example 1:
Ingredients Wt.%
Neoprene W 24.2 Sodium Silicate (Britesil H-24) 54.2 Phenolic Resin (Varcum 5485) 10.6 *Silica (Min-U-Sil) 7.7 **Zinc Oxide 1.3 **Magnesia 1.0 **Sulfur - ~ Y .24 . ~ **Tetramethythirum Monosulfide (Thionex ~ .32 . ~ **N-Phenyl-A7pha-Napthylamine (Neozone A) .44 *Inactive Filler **Active Filler ~ ra~ ks.

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After normal processing, the above material was heat treated at 85C.9 in a forced air oven for 24 hours. The material, when tested as in Example 1, exhibited the following test results.
Test Test Result Expansion - X 7.6 LOI - % 36.5 Green Density - g./cc. 1.48 Fired Density - g./cc. Ooll MOR - kg./cm.2 42 Refractory Pass Pressure Generation - kg./cm. 20 ASTM-E-119-73 Pass ASTM D-395 Method B - % compression 23 Low Temp. Expansion Pass Shore "A" Durometer 94 An intumescent putty-like composition was formulated from the following materials:
Material Wt.%
Polybutene (Oronite~ 32) 28.6 Phenolic resin (Reichold Varcum Type 5416) 21.4 Sodium Sil;cate (Britesil H-24) 3806 Fiberglass (Owens-Corning 799AB 1/4" chopped) 6.0 Sil;ca - (Min-U-Sil) 5.4 The ~iber, sodium silicate, and phenolic resin were mogul mixed into the polybutene. The composite had the consistency of a caulking putty. When fired at 600C. for ten m;nutes, the material expanded 2.1X.
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~ll B~f~8 In these examples, intumescent fire retardant composite materials with the indicated components (weight percent) were formulated according to the compounding procedure of Example l, (4-16) and Example 3 (17-20) and were also tested in the manner set forth in Example l.

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EXA_PLES 21 - 25 In these examples, intumescent ~ire retardant composite mater;als with the indicated components (weight percent) were formulated according to the compounding procedure of Example 1 and were also tested in the manner set forth in Example 1.
Examples Components 21 22 23 24 25 Neoprene W 20.3 22.0 20.0 20 23.4 10 Britesil - H-24 45.4 40.0 35.0 25 52.4 Phenolic Resin 8.0 8.0 5 5 5.5 B (a)Agerite~Stalite S O.37 0.4 0.39 0.39 0.46 (a)Dioctyl Phthalate 8.3 8.35 10 10 8.26 (a)Unads ~ 1.04 1.1 1.03 1.03 1.21 15 (a)Sulfur 0.05 0.05 0.05 0.05 0.06 - (a)Red Lead Oxide 1.04 1.1 1.03 1.03 1.21 (b)Silica 14.6 19.0 27.5 37.5 7.5 (a) Active filler 10.8 11 12.5 12.5 11.2 (b) Inactive filler 14.6 19 27.5 37.5 7.5 20 Expansion (x) 6.4 5.2 5.5 5.7 8.7 LOI % 33.4 37 47.4 47.5 26.5 Green Density (gms/cc) 1.4 1.37 1.37 1.39 1.4 Fired Density (gms/cc~ .14 .17 .13 .13 00118 MOR kg./cm.2 Not measured 25 Refractory pass/fail Pass Pass Pass Pass Pass Low Temperature Ex Expansion Pass Pass Pass Pass Pass Shore "A" Durometer 50 50 45 45 55 ,` '':.` ~t-~e ~a~ks 1 :

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Claims (4)

FN 913,565 THE EMBODIMENTS OF THE INVENTION IN
WHICH AN EXCLUSIVE PROPERTY OR PRIVILEGE
IS CLAIMED ARE DEFINED AS FOLLOWS:
1. Dense, solid, flexible, heat expandable, fire retardant composite material capable of subsisting substan-tially indefinitely in sheet or putty form and having in-creased thermal insulating and sealing efficiency when ex-posed to temperatures above about 110° C., and capable of expanding at least up to two times its original volume consisting essentially of about 15 to 80 weight percent of sodium silicate in granular form as the intumescent compon-ent, the individual sodium silicate granules each enlarging solely upon the application of heat, about 15 to 40 weight percent of a polychloroprene binder component, up to about 40 weight percent of a phenol-formaldehyde organic char-forming resin and up to about 50 weight percent filler com-prising up to about 20 weight percent active filler and up to about 40 weight percent inactive filler.
2. Fire retardant composite material of claim l wherein said granular sodium silicate has particle sizes of from about 0.2 to about 2.0 mm., a moisture content of about 5 to about 30 percent and a SiO2 to Na2o ratio of 2 to 3.75:1.
3. Fire retardant composite material of claim 2 having a Shore "A" durometer of from about 35 to about 95.
4. Dense, solid, flexible, heat expandable, fire retardant composite material capable of subsisting substan-tially indefinitely in sheet or putty form and having in-creased thermal insulating and sealing efficiency when ex-posed to temperatures above about 110° C., and capable of expanding to about ten times its original volume consisting essentially of about 52 weight percent of granular sodium silicate, 95 weight percent of the particles being greater than 0.2 mm., said particles each enlarging solely upon the application of heat, said sodium silicate having a moisture content of about 19 percent, about 23 weight percent of a polychloroprene rubber, about 6 weight percent of powdered phenol-formaldehyde resin, and about 19 weight percent of a filler about 11 weight percent of active filler and about 8 weight percent of inactive filler.
CA000301095A 1977-05-11 1978-04-13 Intumescent fireretardant composites Expired CA1118948A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US79593677A 1977-05-11 1977-05-11
US795,936 1977-05-11
US89139778A 1978-03-31 1978-03-31
US891,397 1978-03-31

Publications (1)

Publication Number Publication Date
CA1118948A true CA1118948A (en) 1982-02-23

Family

ID=27121671

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000301095A Expired CA1118948A (en) 1977-05-11 1978-04-13 Intumescent fireretardant composites

Country Status (1)

Country Link
CA (1) CA1118948A (en)

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