Hostname: page-component-586b7cd67f-tf8b9 Total loading time: 0 Render date: 2024-11-23T21:29:24.018Z Has data issue: false hasContentIssue false
  • English
  • Français

Multidisciplinary optimisation framework for minimum rotorcraft fuel and air pollutants at mission level

Published online by Cambridge University Press:  27 January 2016

C. Linares ,
C. P. Lawson  and
H. Smith
C. Linares
Affiliation:
School of Engineering, Cranfield University, Cranfield, UK
C. P. Lawson*
Affiliation:
School of Engineering, Cranfield University, Cranfield, UK
H. Smith
Affiliation:
School of Engineering, Cranfield University, Cranfield, UK
*
[email protected]
Get access Rights & Permissions [Opens in a new window]

Abstract

Helicopters play a unique role in modern aviation providing a varied range of benefits to society and satisfying the need for fast mobility. However, environmental concerns associated with the operation of rotorcraft have increased due to envisaged growth of helicopter operations. New rotorcraft designs, innovative aero engines and all-electrical systems, which may take decades to be in service, are being developed in order to diminish rotorcraft footprint on environment. However, since there is a large number of polluting rotorcraft that are in use and will only gradually be replaced, in the near-term, improvements to minimise air quality degradation may also be possible from better use of existing rotorcraft by focusing on mission profile management. A multidisciplinary framework, intended to generate outputs for estimating rotorcraft block fuel burn and emissions, was developed. Outcomes generated with this tool were, subsequently, the basis to carry out a parametric study for assessment of light single-engine rotorcraft environmental impact, in terms of fuel burn and emissions. Single and multi-objective optimisation for minimum fuel consumption and air pollutant emissions was part of this research as well.

Type
Research Article
Information
The Aeronautical Journal , Volume 117 , Issue 1193 , July 2013 , pp. 749 - 767
Copyright
Copyright © Royal Aeronautical Society 2013 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Goulos, I., Mohseni, M., Pachidis, V., D’Ippolito, R. and Stevens, J. Simulation Framework Development for Helicopter Mission Analysis, in ASME Conference Proceedings (ed.), ASME Turbo Expo 2010: Power for Land, Sea, and Air (GT2010), 3, 14-18 June 2010, Glasgow, UK, ASME.Google Scholar
2. Erzberger, H. and Slater, G. Optimal Short-Range Trajectories for Helicopters, 1982, 84303, NASA, Moffett Field, CA, USA.Google Scholar
3. Wayne, J. NDARC-NASA Design and Analysis of Rotorcraft Theoretical Basis and Architecture, American Helicopter Society Aeromechanics Specialists’ Conference, 2010, NASA, 20-22 January, San Francisco, CA, USA.Google Scholar
4. Davis, S., Rosenstein, H., Stanzione, K. and Wisniewski, J. HESCOMP. The Helicopter Sizing and Performance Computer Program. User’s manual, revision 2, 1979, NASA-CR-168697, CASI, USA.Google Scholar
5. Nijland, T., Atyeo, S. and Sinha, A. A Simulation Model For Flight Performance Analysis Of Helicopter Mid-Life Upgrade Designs, 30th European Rotorcraft Forum, 14-16 September 2004, Marseille, France, National Aerospace Laboratory NLR, Amsterdam, The Netherlands.Google Scholar
6. Palmer, , Cranfeld University, 1999, The TURBOMATCH Scheme for Aero/Industrial Gas Turbine Engine Design Point/Off Design Performance Calculation (unpublished User’s Guide), UK.Google Scholar
7. Leishman, J. Principles of Helicopter Aerodynamics, 2nd ed, 2006, Cambridge University Press, Cambridge, UK.Google Scholar
8. Army Materiel Command, Alexandria, VA (1974), Engineering design handbook. Helicopter engineering, part 1: Preliminary design (for VFR operation), AD-A002007; AMCP-706-201-PT-1; Pagination 876P.Google Scholar
9. Padfield, G.D. Helicopter Flight Dynamics: The Theory and Application of Flying Qualities and Simulation Modelling, 1996, 1st ed, Blackwell Science, Cambridge, UK.Google Scholar
10. Bramwell, A.R.S., Done, G. and Balmford, D. Bramwell’s Helicopter Dynamics, 2001, 2nd ed, Butterworth-Heinemann, Oxford, UK.Google Scholar
11. Filippone, A. Flight Performance of Fixed and Rotary Wing Aircraft, 2006, 1st ed, Elsevier, Oxford, UK.Google Scholar
12. Stepniewski, W.Z. and Keys, C.N. Rotary-Wing Aerodynamics, 1984, 2nd ed, Dover, London, UK.Google Scholar
13. Linares, C. Environmental Impact Assessment of the Operation of Conventional Helicopters at Mission Level (MSc by Research thesis), 2011, Cranfeld University, UK.Google Scholar
14. Allaire, D. A Physics-Based Emissions Model for Aircraft Gas Turbine Combustors (Master of Science in Aerospace Engineering thesis), 2006, Massachusetts Institute of Technology, USA.Google Scholar
15. Rindlisbacher, T. Guidance on the Determination of Helicopter Emissions, 2009, Federal Offce of Civil Aviation, FOCA, Switzerland.Google Scholar
16. IPCC Special Report: Aviation and the Global Atmosphere, 1999, Cambridge University Press, Cambridge, UK.Google Scholar
17. Coutinho, A. Performance and Emission Optimisation of Novel Aero-Engine Concepts (MSc Thesis), 2008, Cranfeld University, UK.Google Scholar
18. Messinger, B.L. Equilibrium temperature of an unheated icing surface as a function of air speed, J Aeronautical Sciences, 1953, 20, (1), pp 29–42.Google Scholar
19. Vega, R. Analysis of an Electric Environmental Control System to Reduce the Energy Consumption of Fixed-Wing Aircraft and Rotary-Wing Aircraft (MSc by Research thesis), 2001, Cranfeld University, UK.Google Scholar
20. Newman, S.J. Methods of Calculating Helicopter Power, Fuel Consumption and Mission Performance, 2011, University of Southampton, Southampton, UK.Google Scholar
21. Hugon, N. Assessment of Novel Propulsion System Confgurations for Rotorcraft: Individual Research Project (MSc in Aerospace Vehicle Design thesis), 2011, Cranfeld University, UK.Google Scholar
22. Defense & Security Intelligence & Analysis: IHS Jane’s, 2011, Jane’s All the World’s Aircraft, available at: http://jawa.janes.com/public/jawa/index.shtml (accessed June/02).Google Scholar
23. Bell Helicopter: a Textron Company, 2010, Bell 206L4 Product Specifcations, Bell Helicopters, Canada.Google Scholar
24. Watkinson, J. The Art of the Helicopter, 2004, 1st ed, Elsevier, Oxford, UK.Google Scholar