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PRESSURE FILTER
The pressure oil filter housing contains a wire-wound or mesh, Paper or felt elements and incorporates a by-pass valve. The filter housing can be drained independently of the main oil system. This is done through a drain valve in the housing base. When drained, the filter can be removed for examination, servicing, or replacement, as necessary, without disturbing the rest of the system. Typical pressure filters are illustrated in figure.
Filters are usually fitted with an impending by-pass indicator. This is usually a red pop out indicator which will pop out and stay out it the differential pressure across the filter element exceeds a predetermined value. This value will be less than the by-pass valve value, to allow the filter to be replaced before the filter goes into by-pass. The pop out usually has a thermal lock on it, which prevents the pop out extending when the oil is cold and thick.
Damage Limits and Repair Minor damage to compressor and fan blades may be repaired provided the damage is within the allowable limits established by the manufacturer in the AMM
Ideal intake conditions: For air to flow smoothly through a compressor, its velocity should be about 0.5 mach at the compressor inlet; this includes aircraft flying faster than
The figure below compares the discrete solution with the exact analytical solution The error is largest at the right boundary where it is equal to solution. The error is largest at
Inlet duct arrangement in Aircraft Engine: Wherever the APU is located, ducting will be required to bring air to the APU inlet. In figure 18.9. we can see that the inlet duct
the amount of cold working a metal can withstand
Controller Requirements The requirements for the stability and performance of fight control systems are specified in the certi-fication requirements for U.S. civilian aircraft
Heat conduction problem in hollow cylinder There are a lot of researches for calculating the temperature field in various shapes using different boundary and initial cond
Replacement Analysis In the previous chapter we have compared various investment alternatives. Two scenarios were considered: single alternative and a set of mutually exclusive
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).
You are required to undertake the following tasks: 1. Problem Identification Download the dataset assigned to you from the module Blackboard site. Read the data description
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