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As fire doors are passive fire protection parts, the doors have to be certified through standard fire tests. It is usual practice to perform the standard fire testing on the components which require the fire certification. However, some gas turbine enclosure doors are too large to test at the test facility and hence the fire resistance test is practically not possible. The purpose of this paper is to develop a reliable finite element model, validate the model using the specimen door test results and extend the method to actual gas turbine enclosure doors to support the fire certification.

First, the standard fire testing on enclosure door test specimen was carried out. Second, the finite element analysis model was built and tuned to match the standard fire test deflections, and finally, the same modelling technique was extended to model the actual gas turbine enclosure door to verify the results for fire certification process.

Gap analysis, a method of post processing is suggested for result analysis. It was found suitable to verify the gap openings which are required for A0 rated fire certification according to fire test procedure code and also to check the mechanical integrity of the enclosure door frame assembly.

The method presented in this work could be used as support information along with the test specimen results for A0 class fire rating certification of the doors according to International Maritime Organization Resolution MSC.307 (88) Annexure 1: Part 3.

The aero gas turbine has been in commercial service now for a little over 30 years. Pioneering experience on the Dart/Viscount and Ghost/ Comet led to transatlantic commercial turbojet operation in late 1958—just over a quarter of a century ago. Over this period of time, the fuel usage per seat mile for typical long range operation has been reduced by no less than two‐thirds (Figure 1).

While the hot‐end of a gas turbine, with its high thermal stresses and vulnerability to excessive exhaust gas temperatures, tends to attract most attention from the aircraft engineer, it is the compressor which is the dominant factor in aircraft gas turbine performance. This is particularly true of smaller types of engine and older designs. In these gas turbines any reduction in compressor efficiency can have a substantial effect on the thermal efficiency and service life of an engine. Between overhauls the turbine will be running in relatively clean combustion gases, but the compressor, from the moment it enters service, will be subject to continuous fouling.

An aeroplane wing including a fixed forward portion, a flap, a slot controller between the forward portion and the flap, a spoiler on the slot controller, control means on the fixed wing portion and connected with the spoiler for operating the spoiler independently of the slot controller.

An accumulator bladder adapted to be positioned within and secured at one end to an accumulator shell and comprising a moulded bag having two portions each made from a material of different compound from the other, one of the portions being formed and being made of a relatively stiff compound in order to follow the contour of said shell and the other portion being made of a relatively flexible compound in order to telescope into said stiff portion.

The Presidential Address to the Liverpool Engineering Society by Mr. Farthing (the salient points of which are reproduced in this issue) has particular bearing upon lubrication and especially on young lubrication engineers. Mr. Farthing stressed the very wide field open to young engineers and the difficulties associated with training in order to cover as wide a field as may be necessary. It is usually so important to gain a wide knowledge before one can specialise and this is certainly the case with lubrication engineers. One cannot begin to fully appreciate the intricacies of a lubrication system with all its accessory components lubricating and guarding, for example, a large motive power plant or rolling mill, until one has more than a mere working knowledge of the plant itself, the duties it must perform, how it performs them and the snags that arise which might be overcome by correct lubrication. In view of the fact that lubrication systems are just as important in a textile mill as in a power station or a large brick works, the almost impossible‐to‐achieve‐range of knowledge that would simplify the work of a lubrication engineer is very obvious. Fortunately, lubricating principles apply to most cases and knowing how to apply one's knowledge from basic principles is the key to success in this difficult profession.

Surface preparation of a number of major components used in the latest versions of the Rolls‐Royce RB211 gas turbine aero‐engine, prior to bonding and painting operations, has been radically streamlined with the recent installation at the company's Parkside plant of a specially‐designed Vacu‐Blast programme‐controlled dry blasting machine, costing some £94,000. (Vacu‐Blast is part of the BTR Group.)

IN the two years since the last Farnborough Air Show was held by the Society of British Aerospace Companies the aircraft industry has achieved an almost complete metamorphosis from the body blows in the form of major programme cancellations that almost felled it in 1965 to the very healthy position that it holds today.

As part of the V.10 F programme financed by Service Technique de la Production Aeronautique (STPA), AEROSPATIALE and DASSAULT — BREGUET have joined forces to produce a single Falcon 10 wing entirely made of carbon fibre. This wing has just been sent from the AEROSPATIALE Company's Nantes factory to the Toulouse Aernautic Testing Centre. A second wing will also be built, but this time, by DASSAULT‐BREGUET Biarritz plant. The two wings will be used for static fatigue testing. The programme calls for another pair of wings, one to be made by each of the same firms. They will later be mounted to a Falcon 10 for flight testing.

Fire protection has several components: prevention, containment, detection, and suppression. While building codes and inspectors generally do not require special construction techniques or fire protection systems for computer rooms, economic and service factors may dictate that special protection be given such facilities. This article discusses emergency planning, the various types of fire detection and suppression systems, and future options, with particular attention given to halon and possiblehalon‐replacements.