Ultrahigh-Pressure Waterjets for Coke Removal in Jet Engine Fuel Tubes, with Laser-Optic Inspection

1996 ◽  
Author(s):  
D. E. Steele ◽  
J. L. Doyle ◽  
D. O. Monserud ◽  
P. J. Miles
2008 ◽  
Vol 74 (746) ◽  
pp. 2213-2220
Author(s):  
Takahiro TAMURA ◽  
Mikiya ARAKI ◽  
Hideshi YAMADA ◽  
Seiichi SHIGA ◽  
Shigeru HAYASHI ◽  
...  

2020 ◽  
Vol 20 (5) ◽  
pp. 1470-1478
Author(s):  
Mirko Sgambetterra ◽  
Guido Zucca ◽  
Vincenzo di Francesco ◽  
Fabrizio De Paolis ◽  
Manuele Bernabei
Keyword(s):  

2011 ◽  
Vol 19 (3) ◽  
pp. 996-1006 ◽  
Author(s):  
Morteza Montazeri-Gh ◽  
Mostafa Nasiri ◽  
Soheil Jafari

2010 ◽  
Vol 83 (7) ◽  
pp. 1265-1269
Author(s):  
Kh. D. Ibragimov ◽  
E. G. Ismailov ◽  
G. S. Martynova ◽  
N. R. Bektashi ◽  
Z. M. Ibragimova ◽  
...  

Author(s):  
Ewen Marechal ◽  
Sofiane Khelladi ◽  
Florent Ravelet ◽  
Farid Bakir ◽  
Olivier Delepierre-Massue Snecma

1967 ◽  
Author(s):  
Jay C. Harris ◽  
E. A. Steinmetz
Keyword(s):  

2009 ◽  
Vol 2009.3 (0) ◽  
pp. 115-116
Author(s):  
Nobuaki MOTEGI ◽  
Mikiya ARAKI ◽  
Hideshi YAMADA ◽  
Hisao NAKAMURA ◽  
Seiichi SHIGA

2014 ◽  
Vol 136 (04) ◽  
pp. 54-58
Author(s):  
Lee S. Langston

This article explains various technical aspects of the boundary layer ingestion (BLI) concept. Using BLI, airliner designs featuring close-coupled, rear-mounted turbofans are being considered, with a fuselage sculpted to sweep a large part of the fuselage boundary layer into engine inlets for reduced fuel consumption. With an engine array fuselage-centered, rather than splayed out on wings, reduced rudder control is needed in the event of a single engine outage. This reduces the size of a BLI tail assembly, saving weight and reducing drag. A near-future goal of the BLI studies is to determine if modern engine front-mounted fans can be designed to operate efficiently and stably under BLI inlet conditions. The D8 design is aimed at the huge single-aisle, narrow-body market, now dominated by the Boeing 737 and Airbus 320 families. Airframe and engine designers strive to achieve 'clean' inlet flow conditions for jet engines.


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