ISBN 9798672787107 is currently unpriced. Please contact us for pricing.
Available options are listed below:
Available options are listed below:
Intelligent Engine Systems
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/06/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
A high bypass jet engine fan case represents one of the largest, heaviest single components in an engine. In addition to supporting the inlet and providing the fan flowpath, the most critical function is the containment of a failed fan blade. In this development program, a lightweight, low-cost composite containment case with diagnostic capabilities was developed, fabricated, and tested. The fan case design, containment methods, and diagnostic concepts evaluated in the initial Propulsion 21 program were improved and scaled up to a full case design. Xie, Ming Glenn Research Center NASA/CR-2008-215233, E-16523 NAS3-01135; WBS 984754.02.07.03.11.03 FABRICATION; FAN BLADES; GAS TURBINE ENGINES; AIRCRAFT FUEL SYSTEMS; AIRCRAFT ENGINES; SYSTEMS ENGINEERING; MECHANICAL PROPERTIES; LOW COST; COMPRESSORS; CONTAINMENT; PROPULSION SYSTEM PERFORMANCE; FLOW DISTRIBUTION; NANOTECHNOLOGY; CARBON NANOTUBES; PANELS
Show More
Product Format
Product Details
ISBN-13:
9798672787107
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
38
Carton Quantity:
108
Product Dimensions:
8.50 x 0.08 x 11.02 inches
Weight:
0.25 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
A high bypass jet engine fan case represents one of the largest, heaviest single components in an engine. In addition to supporting the inlet and providing the fan flowpath, the most critical function is the containment of a failed fan blade. In this development program, a lightweight, low-cost composite containment case with diagnostic capabilities was developed, fabricated, and tested. The fan case design, containment methods, and diagnostic concepts evaluated in the initial Propulsion 21 program were improved and scaled up to a full case design. Xie, Ming Glenn Research Center NASA/CR-2008-215233, E-16523 NAS3-01135; WBS 984754.02.07.03.11.03 FABRICATION; FAN BLADES; GAS TURBINE ENGINES; AIRCRAFT FUEL SYSTEMS; AIRCRAFT ENGINES; SYSTEMS ENGINEERING; MECHANICAL PROPERTIES; LOW COST; COMPRESSORS; CONTAINMENT; PROPULSION SYSTEM PERFORMANCE; FLOW DISTRIBUTION; NANOTECHNOLOGY; CARBON NANOTUBES; PANELS
Show More