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Aircraft Apu
THE AIRCRAFT APU (Auxiliary Power Unit)

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ABSTRACT
The Auxiliary Power Unit is a system designed to provide a secondary source of energy to a particular plant or craft. In aviation, this system has evolved to become as essential system in today’s commercial transport aircraft. This report provides an analysis of the history, functionality and future development of the aircraft Auxiliary Power Unit. It covers the technological evolution of the APU with reference to specific makes and models, and their direct impact on the aviation industry. The report also details the main components of Auxiliary Power Units, and highlights their impact on the aircraft’s flight controls. The report concludes with a summary of the impact of APU’s on global aviation, and their development into the future.

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CONTENTS

TITLIE PAGE ABSTRACT CONTENTS HISTORY APU SYSTEM COMPONENTS AND FUNCTIONS APU REDUNDANCIES - The RAT FUTURE APU SYSTEMS – The Fuel Cell SUMMARY REFERENCES

1 2 3 4 7 10 11 12 13

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HISTORY
The development of an aircraft Auxiliary Power Unit was first undertaken by British aircraft designer and manufacturer Noel Pemberton Billing in 1916 (Andrews & Morgan, 1987). His P.B.31.E prototype “Nighthawk”, was a quadruplane designed to hunt German airships at night during WW1. For that purpose, it was equipped with a nose-mounted searchlight powered by a 5 horsepower, 2stroke gasoline piston engine, courtesy of the All British Engine Company (ABC) (Andrews & Morgan, 1987). Although the Nighthawk never entered service, it has achieved historical significance as the first ever example of an APU equipped aircraft.
Fig 1: Early ABC APU (ABC and other aero auxiliary engines , 2002)

During WW2, the All British Engine Company once again took up manufacturing of APU systems for military aircraft. ABC APU’s were installed in a variety of aircraft, primarily providing secondary electrical power to various electronic systems (Andrews & Morgan,



References: ABC and other aero auxiliary engines . (2002, 5 14). Retrieved 5 26, 2011, from http://homeand-garden.webshots.com/album/38000561qzQZLj Airbus internal studies. (2008). Case study: Scenario analysis for hydrogen and fuel cells. Airbus. Andrews, C., & Morgan, E. (1987). Supermarine Aircraft since 1914. London: Putnam. ATSB. (2010). Aviation safety investigation number 200401353 . Canberra, ACT: ATSB. Bachtel, B. (2003, 10 22). ETOPS, Extended Operations and En Route Alternate Airports. Retrieved 5 28, 2011, from http://www.boeing.com/commercial/airports/faqs/etopseropsenroutealt.pdf Bentley, D. (2011). BPS 3509 Jet engines - Aircraft General Knowledge Sect 2.3 [lecture slides]. Retrieved 5 29, 2011, from https://learning.secure.griffith.edu.au/@@703577C61004ACBFAB5BD63D984E0618/courses/1/350 9BPS_3111_NA/content/_1639191_1/2011%20BPS%203509%20Turbine%20Engines-Final.ppt Bradley, C. (2007). The Boeing Technical Guide. Classic Aviation Adds: Rover APU 1959. (2008, 10 15). Retrieved 5 26, 2011, from Avitaion Ancestry: http://www.aviationancestry.com/Engines/Rover/ Daggett, D. (2003). Commercial Aeroplanes Fuel Cell Overview. Boeing. Darling, K. (2007). RAF Illustrated Arvo Vulcan Part 1. Big Bird Aviation Publications. F-16.net Media gallery. (2005, 6 21). Retrieved 6 2, 2011, from F-16.net: http://www.f16.net/gallery.html Federal Aviation Administration. (2008). Advisary Circular AC 120-42B. US Department of Transportation. Green, W. (1962). War planes of the Second World War - Flying Boats, Volume 5. Garden City, New York: Doubleday and Company. Honeywell Aerospace. (2010). Honeywell Aerospace. Retrieved 4 15, 2011, from Honeywell International Inc: http://www.honeywell.com/sites/aero/Phoenix_Repair_Overhaul3_C5D5EB8A76730-18D1-F595-53107B90D5DA_HAF4748F3-42EF-F1E6-0E4B-B3C77023F099.htm Jackson, A. (1987). De Havilland Aircraft since 1909. London, England: Putnam. Middleton, G. (2010). Boeing 757 RAT . Retrieved from Biggles software: http://www.bigglessoftware.com/software/757_tech/hydraulics/rat.htm Navaroo, X. (2008, 2 20). Airbus successfuly tests fuel cells in civilian aircraft. Retrieved 6 2, 2011, from The Load Compressor section supplies the aircraft with pneumatic energy (service air). P a g e | 14 NMIT. (n.d.). AME608 Turbine engines - Lubrication system. Retrieved 6 2, 2011, from MNIT online: http://ecampus.nmit.ac.nz/moodle/mod/book/print.php?id=51630 Sabc. (2009, 11 7). Jet fuel starter. Retrieved 6 2, 2011, from http://www.scribd.com/doc/28700771/Jet-Fuel-Starter Schiller, G. (2005). SOFC development for Aircraft Application. Quebec city: German Aerospace Center. Smith, M. A. (1955, August 29). Flight and Aircraft Engineer. no 2588, Vol 74. , pp. 353, 354. Suggs, H. J., Luskus, L. J., Kilian, H. J., & Morkey, J. W. (1979). Exhaust gas composition of the F-16 emergency power unit. Brooks Airforce Base, Texas: USAF school of aerospace medicine. Tapper, O. (1988). Armstrong Whithworth Aircraft since 1913. London, England: Putnam. Tristar L-1011 . (2011). Retrieved 6 2, 2011, from Tristar 500.net: http://www.tristar500.net/features.htm

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