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After installation of a propeller, the engine must be ground run in order to check the propeller for correct function and operation. Aircraft propeller installations vary considerably, and no set testing procedure would be satisfactory for all aircraft. It is imperative, therefore, that any particular installation should be tested in accordance with the approved AMM procedure, which will normally include the following general requirements:
Note: If vibration was experienced during the engine run, the hub retaining nut should be re-tightened after the engine shaft has cooled down.
Nozzle Guide Vane Inspection: Inspection of the NGVs is possible using a strong light source and mirror, it is more probable however that a boroscope inspection will be require
On a typical aerofoil, a point exists about which the resultant aerodynamic pitching moment M is independent of incidence. This special point is called the Aerodynamic Centre (AC).
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Lifting wing FP was run at the conditions corresponding to AGARD WG07 TEST CASE 11, namely M∞ = 0.84,α= 3.06 deg. The ‘final step' values of the partially-conservative paramete
Terminal cash flows Salvage value Salvage value (SV) is the most common example of terminal cash flows. Salvage value may be defined as the market price of an investment at the
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Process of fire risk assessment: In the UK, the process for the FRA came out of the process for a general risk assessment. In a general risk assessment hazards are identif
To achieve successful results in powder metallurgy the metallic powder must be thoroughly homogenized. The term blending and mixing are both used in this content. Blending refers t
Turbine engines cooling : Turbine engines are designed to convert heat energy into mechanical energy. The combustion process is continuous and, therefore, heat is produced. On
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