CERTIFICATE OF FIRE APPROVAL

Transcription

1 LR CERTIFICATE OF FIRE APPROVAL This is to certify that The product(s) detailed below will be accepted for compliance with the applicable Lloyd s Register Rules and Regulations for use on offshore installations classed with Lloyd s Register, and for use on offshore installations when authorised by contracting governments to issue the relevant certificates, licences, permits etc. Manufacturer Address Type Equipment Description Specified Standard Morgan Advanced Materials Thermal Ceramics Tebay Road Bromborough Wirral Merseyside, CH62 3PH United Kingdom (UK) STRUCTURAL STEEL JET FIRE PROTECTION SYSTEM Structural Tubular Steel Sections, Cylindrical Vessels or Pipes protected with a Jet Fire Protection Jacket System Type: FIREMASTER MARINE PLUS BLANKET, for Jet Fires up to 60 mins exposure International Standard ISO Determination of the Resistance to Jet Fires of Passive Fire Protection Materials, Part : General Requirements The attached Design Appraisal Document forms part of this certificate. This certificate remains valid unless cancelled or revoked, provided the conditions in the attached Design Appraisal Document are complied with and the equipment remains satisfactory in service. of issue 20 May 204 Expiry date 9 May 209 Certificate No. SAS F4030 Signed Lloyd's Register EMEA Marine Technology and Engineering Services, London Office Sheet No of 6 Name M. Farrier Surveyor to A Member of the Lloyd s Register Group Note: This certificate is not valid for equipment, the design or manufacture of which has been varied or modified from the specimen tested. The manufacturer should notify Lloyd s Register of any modification or changes to the equipment in order to obtain a valid Certificate. Lloyd's Register Group Limited, its affiliates and subsidiaries and their respective officers, employees or agents are, individually and collectively, referred to in this clause as the 'Lloyd's Register'. Lloyd's Register assumes no responsibility and shall not be liable to any person for any loss, damage or expense caused by reliance on the information or advice in this document or howsoever provided, unless that person has signed a contract with the relevant Lloyd's Register entity for the provision of this information or advice and in that case any responsibility or liability is exclusively on the terms and conditions set out in that contract.

2 7 Fenchurch Street, London, EC3M 4BS Telephone Fax of 6 SAS F4030 DESIGN APPRAISAL DOCUMENT 20 May 204 MTES/SFS/TA/WP ATTACHMENT TO CERTIFICATE OF TYPE APPROVAL No. SAS F4030 This Design Appraisal Document forms part of the Certificate. APPROVAL DOCUMENTATION GL Noble Denton, Spadeadam Test Site, Cumbria, United Kingdom, Fire Test Report Nos. 3956, Issue 3, dated 24 July 203 and 3406, Issue 4, dated 22 February 203, both for Tubular Jet Fire Tests. BRE Global, Watford, United Kingdom, Fire Test Report No , dated July 202 and Assessment Report No. CC 28408, dated 7 August 202, hydrocarbon fire testing of tubular members. Manufacturers drawing No. FM CAD 4.0 PJ, FireMaster Marine Plus Jet Fire Pipe Protection System General Arrangement. A Surveyor from Lloyd s Register s Liverpool Office witnessed the two jet fire tests of tubular sections. CONDITIONS OF CERTIFICATION. Applications to be based on two 60 minute jet fire exposure tests performed on a 29.mm OD, 6mm thick and a 93.7mm OD, 5mm thick, Tubular Sections (Hp/A s of 65 m ¹ & 205 m ¹), both fitted with a FireMaster Marine Plus Blanket (28kg/m³ density) jet fire protection system (26mm and 75mm nominal thickness respectively). The system insulation must consist of at least two layers of insulation, with staggered overlap joints, all covered with 0.6mm thick stainless steel cladding secured with stainless steel securing bands and self-tapping screws. 2. Suitably approved insulation is to be applied to any other part of the protected fire exposed surfaces not covered by this system, in all cases. In particular, attention is to be paid to means of securing jacket boundaries and the prevention of heat bridging; an overlap of at least 50mm should be provided between the two systems. 3. May be considered for applications on tubular steel sections, pipes or cylindrical vessels of up to 500mm diameter, but not with corners or edge features and not exceeding an Hp/A factor of 205 m ¹. (Where Hp is the outside circumference and A is the cross-sectional area). 4. The thickness of a Firemaster Marine Plus Blanket system for jet fire exposures up to 60 mins duration may be determined by adding a Jet Fire Erosion Factor as shown in Table, to the thickness required by hydrocarbon testing (as shown) and approved in a separate hydrocarbon LR Certificate of Fire Approval for steel tubular sections. The Jet Fire Erosion Factor thickness for any intermediate Section Factor (Hp/A value) between 65 m ¹ and 205m ¹ may be determined by linear interpolation of total thickness values given in Table. 5. Applications in each case to be approved by Lloyd's Register at the design stage. 6. Production items are to be manufactured in accordance with a quality control system which shall be maintained to ensure that items are of the same standard as the approved prototype.

3 DESIGN APPRAISAL DOCUMENT 7 Fenchurch Street, London, EC3M 4BS Telephone Fax of 6 SAS F May 204 MTES/SFS/TA/WP ATTACHMENT TO CERTIFICATE OF TYPE APPROVAL No. SAS F4030 NOTE. The FireMaster Marine Plus Blanket insulation system may be assigned the Classifications: JF/Structural steel/400/50 - (for 75mm thick and Section Factor Hp/A = 205 m ¹) or JF/Structural steel/400/40 - (for 25mm thick and Section Factor Hp/A = 65 m ¹). The Classification depends on the particular application, Hp/A Section Factor, insulation thickness and the maximum core temperature required, in accordance with ISO :2007(E), Section 5.4, the Critical Temperature Rise for load bearing steel structures is normally 400ºC. Table : Additional Thickness (mm) of FIREMASTER MARINE PLUS BLANKET (28kg/m³ density) to be applied as a Jet Fire Erosion Factor (JFEF) at 60 min or 30 min durations, to the approved Hydrocarbon Fire Thickness at 400 C steel core temperature Jet or Hydrocarbon Fire Exposure Time (minutes) Additional thickness (mm) of insulation required as JFEF above Hydrocarbon Fire Requirements for a 400 C Steel Core Temperatures at stated exposure time (mins) for the Hp/A Factor (m ¹) of tubular 65m ¹ 00 m ¹ 35 m ¹ 70 m ¹ 205 m ¹ 60 min Hydrocarbon approved thickness min JFEF (in addition to hydrocarbon) Total Thickness* min Hydrocarbon approved thickness min JFEF (in addition to hydrocarbon) Total Thickness* *Note to Table The total Jet Fire thickness for any intermediate section factor (Hp/A value) between 65 m ¹ and 205m ¹ may also be determined by linear interpolation of Tables above and rounded up to the nearest mm. For example: an Hp/A value of 50 would require a total thickness of 39mm at 30 mins and 86mm at 60 mins.

4 DESIGN APPRAISAL DOCUMENT 7 Fenchurch Street, London, EC3M 4BS Telephone Fax of 6 SAS F May 204 MTES/SFS/TA/WP JET FIRE TEST RESULTS ATTACHMENT TO CERTIFICATE OF TYPE APPROVAL No. SAS F4030 TEST No. - TEST RESULTS FOR INSULATED TUBULAR SECTION Hp/A = 65 (26mm thick) GL Noble Denton Report No. 3956, Issue 3, dated 24 July 203 Integrity: Insulation: 60 minutes (protection remained intact for duration of test) The following maximum temperature rises were recorded on the tubular specimen at the standard ISO positions: Thermocouple No. after 5 minutes of exposure: 58.ºC Thermocouple No. 2 after 30 minutes of exposure: 303.3ºC Thermocouple No. 2 after minutes of exposure: 400ºC Thermocouple No. 2 after 45 minutes of exposure: 46.5ºC Thermocouple No. after 60 minutes of exposure: 5.4ºC TEST No. 2 - TEST RESULTS FOR INSULATED TUBULAR SECTION Hp/A = 205 (75mm thick) GL Noble Denton Report No.3406, Issue 4, dated 22 February 203 Integrity: Insulation: 60 minutes (protection remained intact for duration of test) The following maximum temperature rises were recorded on the tubular specimen at the standard ISO positions: Thermocouple No. 5 after 5 minutes of exposure: 36ºC Thermocouple No. 7 after 30 minutes of exposure: 90ºC Thermocouple No. 7 after 45 minutes of exposure: ºC Thermocouple No. 7 after minutes of exposure: 400ºC Thermocouple No. 7 after 60 minutes of exposure: 473.3ºC DESCRIPTION OF TEST SPECIMENS Two jet fire tubular tests were performed in accordance with ISO :2007. Test specimen No. 3 metre long circular steel hollow section 29mm OD/203mm ID, wall thickness: 8.0mm and a Section Factor (Hp/A) of 65m ¹; fitted with a FireMaster Marine Plus Blanket jet fire resistant insulation system with both circumferential and longitudinal joints of the insulation and the 0.6mm thick stainless steel outer cladding sheets, all secured by stainless steel securing bands 20mm wide x mm thick with screw fasteners, fitted around the jacket at 200mm centres and 00mm from circumferential joints, which were overlapped for 75mm and sealed with Dow Corning Firestop 700 mastic. The stainless steel cladding panel longitudinal joints were secured together by No.8 stainless steel selftapping screws at 00mm centres and the specimen insulation consisted of: two layers of FireMaster Marine Plus Blanket with staggered overlap joints (both 3mm thick, 28 kg/m³ density), with a total nominal thickness of 26mm.

5 DESIGN APPRAISAL DOCUMENT 7 Fenchurch Street, London, EC3M 4BS Telephone Fax of 6 SAS F May 204 MTES/SFS/TA/WP ATTACHMENT TO CERTIFICATE OF TYPE APPROVAL No. SAS F4030 Test specimen No.2 3 metre long circular steel hollow section 93.7mm OD/83.7mm ID, wall thickness: 5.0mm and a Section Factor (Hp/A) of 205m ¹; fitted with a FireMaster Marine Plus Blanket jet fire resistant insulation system with both circumferential and longitudinal joints of the insulation and the 0.6mm thick stainless steel outer cladding sheets, all secured by stainless steel securing bands 20mm wide x mm thick with screw fasteners, fitted around the jacket at 200mm centres and 00mm from circumferential joints, which were overlapped for 75mm and sealed with Dow Corning Firestop 700 mastic. The stainless steel cladding panel longitudinal joints were secured together by No.8 stainless steel selftapping screws at 00mm centres and the specimen insulation consisted of: two layers of FireMaster Marine Plus Blanket with staggered overlap joints (first layer 50mm thick and second layer 25mm thick, both 28 kg/m³ density), with a total nominal thickness of 75mm. SCOPE The test described in the procedure ISO 22899: Part is one in which some of the properties of passive fire protection materials can be determined and is designed to give an indication of how passive fire protection materials will perform in a jet fire. The dimensions of the test specimen may be smaller than typical items of structure and plant and the release of gas may be substantially less than that which might occur in a credible event. However, individual thermal and mechanical loads imparted to the passive fire protection material, from the jet fire defined in the procedure described in ISO 22899: Part, have been shown to be similar to those by large-scale jet fires resulting from high pressure releases of natural gas. Although the test method has been designed to simulate some of the conditions that occur in an actual jet fire, it cannot reproduce them all exactly and the thermal and mechanical loads do not necessarily coincide. The results of this test do not guarantee safety but may be used as elements of a fire risk assessment for structures or plant. This should also take into account all the other factors that are pertinent to an assessment of the fire hazard for a particular end use. This test is not intended to replace the hydrocarbon fire resistance test (ISO/TR 834-3/EN or equivalent) but is seen as a complimentary test. PLACES OF PRODUCTION Thermal Ceramics Thermal Ceramics Thermal Ceramics Lieu-dit Les Plantées 202 Old Savannah Road Cerrada La Paz No 0 St. Marcellin-en-Forez Augusta Fraccionamiento Industrio La Paz F GA Pachuca Hidalgo France United States of America (USA) Mexico Morganite Brazil LTDA Shinnika Thermal Ceramics Thermal Ceramics Rua Darcy Pereira Chikko-yawata-machi -3 Bookdong Distrito Industrial de Santa Cruz Sakai Non Gong Eup Rio de Janeiro-RJ Japan Dal Sung-Gun, Dae Gui-Shi, Brazil Korea

6 LR DESIGN APPRAISAL DOCUMENT 7 Fenchurch Street, London, EC3M 4BS Telephone Fax of 6 SAS F May 204 MTES/SFS/TA/WP ATTACHMENT TO CERTIFICATE OF TYPE APPROVAL No. SAS F4030 PLACES OF PRODUCTION (CONTINUED) Morgan Thermal Ceramics (Kailong) No.20- Quankou Road Jingmen City, Hubei Province, People s Republic of China Morgan Thermal Ceramics China 8, Kang an Road Kangqiao Industrial Zone Pudong Shanghai 2035 People s Republic of China M/S Murugappa Morgan Thermal Ceramics Ltd. No. 26 & 27, SIPCOT Ranipet Tamil Nadu India Lloyd's Register EMEA Marine Technology and Engineering Services, London Office Martin Farrier Lead Specialist Statutory Fire & Safety Marine Technology and Engineering Services Supplementary Type Approval Terms and Conditions This certificate and Design Appraisal Document relates to type approval, it certifies that the prototype(s) of the product(s) referred to herein has/have been found to meet the applicable design criteria for the use specified herein, it does not mean or imply approval for any other use, nor approval of any products designed or manufactured otherwise than in strict conformity with the said prototype(s).