Detailed Investigation of Heat Flux Measurements Made in a Standard Propane-Air Fire-Certification Burner Compared to Levels Derived From a Low-Temperature Analog Burner

Author:

Abu Talib Abd. Rahim1,Neely Andrew J.2,Ireland Peter T.3,Mullender Andrew J.4

Affiliation:

1. Universiti Putra Malaysia, Department of Aerospace Engineering, Faculty of Engineering, 43400 Selangor, Malaysia

2. University of New South Wales, School of Aerospace and Mechanical Engineering, Australian Defense Force Academy, Northcott Drive, Canberra ACT 2600, Australia

3. University of Oxford, Department of Engineering Science, Parks Road, Oxford OX1 3PJ, UK

4. Rolls-Royce plc., Fire Precautions Group, P.O. Box 31, Derby, DE24 8Bj, UK

Abstract

This paper presents detailed heat flux measurements on a flat plate subjected to the ISO2685 [The International Organization for Standardization (ISO), 1992, “Aircraft—Environmental Conditions and Test Procedures for Airborne Equipment—Resistance to Fire in Designated Fire Zones,” ISO2685:1992(E)] standard, propane fueled burner used throughout the industry in aero-engine fire-certification. The authors have developed a custom-built heat transfer gauge to measure the heat flux from the burner under isothermal wall conditions. The heat flux from the standard burner is normally calibrated using either a water-cooled copper tube or a Gardon gauge, each sited at a single position in the flame. There are no reports in the literature of a detailed survey of heat flux distribution for the burner and the results are of considerable interest to engineers involved in fire-certification. The reported measurements constitute the first, detailed distribution of heat flux from the actual burner flame during a fire test. These measurements provided benchmark data which allowed the heat flux distribution from the ISO burner to be compared to levels derived from the low-temperature analog burner developed by the authors. The analog burner uses liquid crystals to measure heat transfer coefficient and adiabatic wall temperature on scale models of engine components and provides key data to facilitate the successful design of components used in fire zones. The objective of this paper is to further validate the low-temperature analog burner technique developed by the authors which simulates the standard large propane-air burner for fire-certification in aero engine.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference29 articles.

1. The International Organization for Standardization (ISO), 1992, “Aircraft—Environmental Conditions and Test Procedures for Airborne Equipment— Resistance to Fire in Designated Fire Zones,” ISO2685:1992(E).

2. Federal Aviation Administration (FAA), 1990, “Draft Advisory Circular, Powerplant Installation and Propulsion System Component Fire Protection Test Methods, Standards and Criteria,” U.S. Department of Transportation, Advisory Circular No: 20-135.

3. Neely, A. J., Ireland, P. T., and Mullender, A. J., 1999, “Pilot Study to Investigate Novel Experimental and Theoretical Fire-Event Modelling Techniques,” Proceedings, 37th Aerospace Science Meeting, Reno, Nevada, USA. (AIAA-99-09-0326).

4. Schultz, D. L., and Jones, T. V., 1973, “Heat Transfer Measurements in Short Duration Hypersonic Facilities,” AGARD-AG-165, Advisory Group for Aerospace Research and Development (AGARD).

5. Jones, T. V., 1977, “Heat Transfer, Skin Friction, Total Temperature and Concentration Measurements,” Measurement of Unsteady Fluid Dynamic Phenomena, von Karman Institute for Fluid Dynamics.

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