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Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006
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Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Dec 22, 2015

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Page 1: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Aircraft Fuel Systems

AIAA Team 1 (Shelley Biagi & Curtis Black)

A/C Design Class

Tuesday, September 19, 2006

Page 2: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Business and Commercial Aviation Magazine

“An aircraft's fuel system has a more profound effect on aircraft performance than any other airframe system. Without fuel, the mission inevitably comes to an abrupt stop and, unless the flight crew is very, very lucky, the ensuing forced landing will cause severe or catastrophic aircraft damage.” ~ Fred George, 6/20/06 http://www.avweek.com/avnow/news/channel_bca_story.jsp?id=news/fuel0606.xml

Page 3: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Fuel Types

Civilian Jet A Jet A-1 Jet B

Military JP-4 JP-5 JP-8

Page 4: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Typical Fuel Tanks

Integral Rigid Removable Bladder Rule of Thumb for max. fuel volume: 85% for wing

tanks and 92% for fuselage tanks, measured to the external skin surface (exception: bladder tanks, 77% and 83%, respectively)

External

Page 5: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Components

Main Tanks

Header Tank (separate from main tanks, holds enough fuel for engines to run during complicated maneuvers)

Gravity Feed (small aircraft only)

Electric/Engine-driven Fuel Pumps

Page 6: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Fuel distributed around center of gravity

Page 7: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Fuel Dumping Systems

Needed to meet landing weight limits of landing gear or runway length

System of fuel pumps and valves Usually ejected from wingtips Sometimes from aft-most point of fuselage Usually designed to allow the plane to go

from max take-off weight to max landing weight in 15 minutes or less.

Page 8: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

777 Fuel Dumping http://www.aerospaceweb.org/question/planes/q0245b.shtml

Page 9: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

http://www.centennialofflight.gov/essay/Evolution_of_Technology/refueling/Tech22G5.htm

Page 10: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

In-Flight Refueling

Original motivation: endurance records Currently used only in the military sector Two main types:

Boom and Receptacle Probe and Drogue

http://www.answers.com/topic/aerial-refueling

Page 11: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

References

Ask A Scientist http://www.newton.dep.anl.gov/askasci/eng99/eng99417.htm

Aerospaceweb.org http://www.aerospaceweb.org/question/planes/q0245b.shtml

Refueling http://www.centennialofflight.gov/essay/Evolution_of_Technology/refueling/Tech22G5.htm

PBS http://www.pbs.org/wgbh/nova/concorde/anat-nf.html Wikipedia http://en.wikipedia.org/wiki/Fuel_tank Raymer Aircraft Design: A Conceptual Approach 4th ed.

By Daniel Raymer George, Fred Business and Commercial Aviation Magazine,

June 2006 issue. http://www.avweek.com/avnow/news/channel_bca_story.jsp?id=news/fuel0606.xml

Page 12: Aircraft Fuel Systems AIAA Team 1 (Shelley Biagi & Curtis Black) A/C Design Class Tuesday, September 19, 2006.

Any Questions?