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It’s funny to think about ancient traffic jams, but that was why the Tower Bridge in London, England was built. By the end of the 19th century, the development of the eastern part of London caused such a load on the London Bridge that the city decided to build a new bridge.

AIRCRAFT GAS TURBINE ENGINES

 

 

Introduction

 

 

Most of modern passenger and military aircraft are powered by gas turbine engines, which are also called jet engines. There are several types of jet engines, but all jet engines have some parts in common . Aircraft gas turbine engines can be classified according to (1) the type of compressor used and (2) power usage produces by the engine.
Compressor types are as follows:
    1. Centrifugal flow
    2. Axial flow
    3. Centrifugal-Axial flow.
Power usage produced are as follows:
   1. Turbojet engines
   2. Turbofan engines.
   3. Turboshaft engines.

 

 

Centrifugal Compressor Engines
Centrifugal flow engines are compress the air by accelerating air outward perpendicular to the longitudinal axis of the machine. Centrifugal compressor engines are divided into Single-Stage and Two-Stage compressor. The amount of thrust is limited because the maximum compression ratio.

 

   

 

 

Principal Adventages of Centrifugal Compressor
1. Light Weight
2. Simplicity
3. Low cost.

 

 

Axial Flow Compressor Engines
Axial flow compressor engines may incorporate one , two , or three spools (Spool is defined as a group of compressor stages rotating at the same speed) . Two spool engine , the two rotors operate independently of one another. The turbine assembly for the low pressure compressor is the rear turbine unit . This set of turbines is connected to the forward , low pressure compressor by a shaft that passes through the hollow center of the high pressure compressor and turbine drive shaft.

 

 

  

 

 

Adventages and Disadventages
Adventages: Most of the larger turbine engines use this type of compressor because of its ability to handle large volumes of airflow and high pressure ratio.
Disadventages: More susceptable to foreign object damage , Expensive to manufacture , and It is very heavy in comparision to the centrifugal compressor with the same compression ratio.

 

 

Axial-Centrifugal Compressor Engine
Centrifugal compressor engine were used in many early jet engines , the efficiency level of single stage centrifugal compressor is relatively low . The multi-stage compressors are some what better , but still do not match with axial flow compressors. Some small modern turbo-prop and turbo-shaft engines achieve good results by using a combination axial flow and centrifugal compressor such as PT6 Pratt and Whitney of canada which very popular in the market today and T53 Lycoming engine.

 

 

 

  

 

 

Characteristics and Applications

 

 

The turbojet engine : Turbojet engine derives its thrust by highly accelerating a mass of air , all of which goes through the engine. Since a high ” jet ” velocity is required to obtain an acceptable of thrust, the turbine of turbo jet is designed to extract only enough power from the hot gas stream to drive the compressor and accessories . All of the propulsive force (100% of thrust ) produced by a jet engine derived from exhaust gas.

The turboprop engine : Turboprop engine derives its propulsion by the conversion of the majority of gas stream energy into mechanical power to drive the compressor , accessories , and the propeller load. The shaft on which the turbine is mounted drives the propeller through the propeller reduction gear system . Approximately 90% of thrust comes from propeller and about only 10% comes from exhaust gas. The turbofan engine : Turbofan engine has a duct enclosed fan mounted at the front of the engine and driven either mechanically at the same speed as the compressor , or by an independent turbine located to the rear of the compressor drive turbine . The fan air can exit seperately from the primary engine air , or it can be ducted back to mix with the primary’s air at the rear . Approximately morethan 75% of thrust comes from fan and less than 25% comes from exhaust gas.

The turboshaft engine : Turboshaft engine derives its propulsion by the conversion of the majority of gas stream energy into mechanical power to drive the compressor , accessories , just like the turboprop engine but The shaft on which the turbine is mounted drives something other than an aircraft propeller such as the rotor of a helicopter through the reduction gearbox . The engine is called turboshaft.

Aircraft types for charter

 

                      Helicopters
A helicopter is one of the most convenient and timesaving ways to transfer between the city and airport, alternatively an easy way to reach remote destinations.

 

 

                      Twin Pistons
A economical aircraft range suitable for short distance flights. Aircraft seating capacity ranging from 3 to 8 passengers.

 

 

                   Turboprops
A wide range of aircraft suitable for short and medium distance flights with a duration of up to 2-4 hours. Aircraft seating capacity ranging from 4 to 70 passengers.

 

 

                  Executive Jets
An Executive Jet is the most time efficient way of travel, suitable for medium or long distance flights. Aircraft seating capacity ranging from 4 to 16 passengers.

 

 

   Airliners
Large jet aircraft suitable for all kinds of flights. Aircraft seating capacity ranging from 50 to 400 passengers.

 

 

                  Cargo Aircraft
Any type of cargo. Ranging from short notice flights carrying vital spare parts up to large cargo aircraft that can transport any volumnious goods.