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Handbook of Turbomachinery Second Edition Revised - Ventech!

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pressures at critical points. These data may be obtained during<br />

certification tests as well.<br />

Engine vibration survey.<br />

Bird ingestion or foreign object damage (FOD) tests.<br />

Bird ingestion tests are performed to determine the robustness <strong>of</strong> the<br />

engine components to withstand the effects <strong>of</strong> ingestion <strong>of</strong> foreign objects<br />

such as a bird (1 to 4 lbm), piece <strong>of</strong> tire tread, sand, gravel or water, ice and<br />

hail. According to FAA regulations, the engine is required to demonstrate<br />

that the ingestion <strong>of</strong> a bird 4 lbm in weight, fired at the engine at a maximum<br />

climb speed <strong>of</strong> 250 knots (273 miles/hr), should cause no fire, fan or rotor<br />

burst, or loss in shutdown capability. The regulations stipulate further that a<br />

1 lbm bird fired several times at the engine at an initial climb speed <strong>of</strong> 150<br />

knots (173 miles/hr) should cause less than 25% thrust loss with no<br />

shutdown. (A certain minimum number <strong>of</strong> test firings proportional to the<br />

area based on the engine inlet flange diameter is required.) This test is more<br />

severe in its effects than the 4-lbm bird ingestion test. The ingestion <strong>of</strong> water,<br />

ice, or hail should cause no thrust loss or shutdown <strong>of</strong> the engine.<br />

FAA Certification Tests and Military Quality Tests. Figure 18 shows the<br />

engine cycle for FAA accelerated mission test, which specifies variations in<br />

power level plotted against time. Each cycle shown lasts 26.4 min. The total<br />

duration <strong>of</strong> the test is 150 hr. The engine is expected to operate satisfactorily<br />

over the whole period with no deterioration in performance. At the end <strong>of</strong><br />

the test, inspection should indicate no signs <strong>of</strong> distress at any <strong>of</strong> the<br />

components.<br />

Future <strong>of</strong> Mechanical and Thermal Design<br />

As seen in the foregoing, improved materials, better analytical techniques<br />

including unsteady flow prediction capability, and better experimental<br />

methods to understand the local effects <strong>of</strong> stress and heat transfer are<br />

necessary to improve the capabilities for design. These improvements may<br />

be expected to permit the design <strong>of</strong> more durable machines with improved<br />

performance. The following paragraphs provide a very limited sample <strong>of</strong><br />

some <strong>of</strong> the areas that are showing signs <strong>of</strong> promise for future developments.<br />

Improved Materials<br />

Ceramics for Airfoils and Turbine Disks. Ceramics have certain<br />

characteristics that make them admirably suited for use in hightemperature<br />

applications. These are<br />

Copyright © 2003 Marcel Dekker, Inc.

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