Getting to Grips with Fuel Economy
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Aircraft Engine Performance Study Using Flight Data Recorder Archives
Aircraft Engine Performance Study Using Flight Data Recorder Archives Yashovardhan S. Chati∗ and Hamsa Balakrishnan y Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA Aircraft emissions are a significant source of pollution and are closely related to engine fuel burn. The onboard Flight Data Recorder (FDR) is an accurate source of information as it logs operational aircraft data in situ. The main objective of this paper is the visualization and exploration of data from the FDR. The Airbus A330 - 223 is used to study the variation of normalized engine performance parameters with the altitude profile in all the phases of flight. A turbofan performance analysis model is employed to calculate the theoretical thrust and it is shown to be a good qualitative match to the FDR reported thrust. The operational thrust settings and the times in mode are found to differ significantly from the ICAO standard values in the LTO cycle. This difference can lead to errors in the calculation of aircraft emission inventories. This paper is the first step towards the accurate estimation of engine performance and emissions for different aircraft and engine types, given the trajectory of an aircraft. I. Introduction Aircraft emissions depend on engine characteristics, particularly on the fuel flow rate and the thrust. It is therefore, important to accurately assess engine performance and operational fuel burn. Traditionally, the estimation of fuel burn and emissions has been done using the ICAO Aircraft Engine Emissions Databank1. However, this method is approximate and the results have been shown to deviate from the measured values of emissions from aircraft in operation2,3. -
Design and Analysis of Advanced Flight: Planning Concepts
NASA Contractor Report 4063 Design and Analysis of Advanced Flight: Planning Concepts Johri A. Sorerisen CONrRACT NAS1- 17345 MARCH 1987 NASA Contractor Report 4063 Design and Analysis of Advanced Flight Planning Concepts John .A. Sorensen Analytical Mechanics Associates, Inc. Moantain View, California Prepared for Langley Research Center under Contract NAS 1- 17345 National Aeronautics and Space Administration Scientific and Technical Information Branch 1987 F'OREWORD This continuing effort for development of concepts for generating near-optimum flight profiles that minimize fuel or direct operating costs was supported under NASA Contract No. NAS1-17345, by Langley Research Center, Hampton VA. The project Technical Monitor at Langley Research Center was Dan D. Vicroy. Technical discussion with and suggestions from Mr. Vicroy, David H. Williams, and Charles E. Knox of Langley Research Center are gratefully acknowledged. The technical information concerning the Chicago-Phoenix flight plan used as an example throughout this study was provided by courtesy of United Airlines. The weather information used to exercise the experimental flight planning program EF'PLAN developed in this study was provided by courtesy of Pacific Southwest Airlines. At AMA, Inc., the project manager was John A. Sorensen. Engineering support was provided by Tsuyoshi Goka, Kioumars Najmabadi, and Mark H, Waters. Project programming support was provided by Susan Dorsky, Ann Blake, and Casimer Lesiak. iii DESIGN AND ANALYSIS OF ADVANCED FLIGHT PLANNING CONCEPTS John A. Sorensen Analytical Mechanics Associates, Inc. SUMMARY The Objectives of this continuing effort are to develop and evaluate new algorithms and advanced concepts for flight management and flight planning. This includes the minimization of fuel or direct operating costs, the integration of the airborne flight management and ground-based flight planning processes, and the enhancement of future traffic management systems design. -
Advisory Circular (AC)
U.S. Department Advisory of Transportation Federal Aviation Administration Circular Subject: Parts 91, 121, 125, and 135 Date: 7/30/12 AC No: 120-74B Flightcrew Procedures During Taxi Initiated by: Change: Operations AFS-200/800 1. PURPOSE. This advisory circular (AC) provides guidelines for the development and implementation of standard operating procedures (SOP) for conducting safe aircraft operations during taxiing to avoid causing a runway incursion. In accordance with Federal Aviation Administration (FAA) Order 7050.1, Runway Safety Program, the definition of a runway incursion is any occurrence at an aerodrome involving the incorrect presence of an aircraft, vehicle, or person on the protected area of a surface designated for the landing and takeoff of aircraft. It is intended for use by persons operating aircraft with two or more pilots on the flight deck under Title 14 of the Code of Federal Regulations (14 CFR) parts 91, 121, 125, and 135. The FAA recommends that these guidelines become an integral part of all SOPs, flight operations manuals (FOM), and formal flightcrew member training programs. The use of flightcrew SOPs should be emphasized and employed during all phases of flight, including ground operations. Appendices 1 and 2 of this AC contain examples of SOPs that are identical or similar to some SOPs currently in use. These appendices are not directive or prescriptive in nature and do not represent a rigid FAA view of Best Practices. SOPs may vary among fleets and among certificate holders and may change over time. Operators may integrate the information contained in Appendices 1 and 2 into their fleet-specific, route-specific, and equipment-specific operations and checklists. -
CRUISE FLIGHT OPTIMIZATION of a COMMERCIAL AIRCRAFT with WINDS a Thesis Presented To
CRUISE FLIGHT OPTIMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS _______________________________________ A Thesis presented to the Faculty of the Graduate School at the University of Missouri-Columbia _______________________________________________________ In Partial Fulfillment of the Requirements for the Degree Master of Science _____________________________________________________ by STEPHEN ANSBERRY Dr. Craig Kluever, Thesis Supervisor MAY 2015 The undersigned, appointed by the dean of the Graduate School, have examined the thesis entitled CRUISE FLIGHT OPTMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS presented by Stephen Ansberry, a candidate for the degree of Master of Science, and hereby certify that, in their opinion, it is worthy of acceptance. Professor Craig Kluever Professor Roger Fales Professor Carmen Chicone ACKNOWLEDGEMENTS I would like to thank Dr. Kluever for his help and guidance through this thesis. I would like to thank my other panel professors, Dr. Chicone and Dr. Fales for their support. I would also like to thank Steve Nagel for his assistance with the engine theory and Tyler Shinn for his assistance with the computer program. ii TABLE OF CONTENTS ACKNOWLEDGEMENTS………………………………...………………………………………………ii LIST OF FIGURES………………………………………………………………………………………..iv LIST OF TABLES…………………………………………………………………………………….……v SYMBOLS....................................................................................................................................................vi ABSTRACT……………………………………………………………………………………………...viii 1. INTRODUCTION.....................................................................................................................................1 -
Estimation of Aircraft Taxi-Out Fuel Burn Using Flight Data Recorder Archives
Estimation of Aircraft Taxi-out Fuel Burn using Flight Data Recorder Archives Harshad Khadilkar∗ and Hamsa Balakrishnany Massachusetts Institute of Technology, Cambridge, MA 02139, USA The taxi-out phase of a flight accounts for a significant fraction of total fuel burn for aircraft. In addition, surface fuel burn is also a major contributor to CO2 emissions in the vicinity of airports. It is therefore desirable to have accurate estimates of fuel consumption on the ground. This paper builds a model for estimation of on-ground fuel consumption of an aircraft, given its surface trajectory. Flight Data Recorder archives are used for this purpose. The taxi-out fuel burn is modeled as a linear function of several factors including the taxi-out time, number of stops, number of turns, and number of acceleration events. The statistical significance of each potential factor is investigated. The parameters of the model are estimated using least-squares regression. Since these parameters are estimated using data from operational aircraft, they provide more accurate estimates of fuel burn than methods that use idealized physical models of fuel consumption based on aircraft velocity profiles, or the baseline fuel consumption estimates provided by the International Civil Aviation Organization. Our analysis shows that in addition to the total taxi time, the number of acceleration events is a significant factor in determining taxi fuel consumption. Nomenclature ICAO International Civil Aviation Organization FDR Flight Data Recorder MTOW Maximum TakeOff Weight Tamb Ambient absolute temperature f Total fuel consumed during taxi-out t Taxi-out time ns Number of stops nt Number of turns na Number of acceleration events I. -
May 31, 2004 5 - 1
Airports Authority of India Manual of Air Traffic Services – Part 1 CHAPTER 5 SEPARATION METHODS AND MINIMA 5.1 Provision for the separation of Whenever, as a result of failure or controlled traffic degradation of navigation, communications, altimetry, flight control or other systems, 5.1.1 Vertical or horizontal separation shall aircraft performance is degraded below the be provided: level required for the airspace in which it is a) between IFR flights in Class D and E operating, the flight crew shall advise the airspaces except when VMC climb or ATC unit concerned without delay. Where the descent is involved under the failure or degradation affects the separation conditions specified in para 5.5.6; minimum currently being employed, the b) between IFR flights and special VFR controller shall take action to establish flights; [and another appropriate type of separation or c) between special VFR flights separation minimum. 5.1.2 No clearance shall be given to execute any manoeuvre that would reduce 5.2 Reduction in separation minima the spacing between two aircraft to less than the separation minimum applicable in the 5.2.1 In the vicinity of aerodromes circumstances. In the vicinity of aerodromes, the separation 5.1.3 Larger separations than the specified minima may be reduced if: minima should be applied whenever a) adequate separation can be provided exceptional circumstances such as unlawful by the aerodrome controller when each interference or navigational difficulties call for aircraft is continuously visible to this extra precautions. This should be done with controller; or due regard to all relevant factors so as to b) each aircraft is continuously visible to avoid impeding the flow of air traffic by the flight crews of the other aircraft application of excessive separations. -
Off Airport Ops Guide
Off Airport Ops Guide TECHNIQUES FOR OFF AIRPORT OPERATIONS weight and balance limitations for your aircraft. Always file a flight plan detailing the specific locations you intend Note: This document suggests techniques and proce- to explore. Make at least 3 recon passes at different levels dures to improve the safety of off-airport operations. before attempting a landing and don’t land unless you’re It assumes that pilots have received training on those sure you have enough room to take off. techniques and procedures and is not meant to replace instruction from a qualified and experienced flight instruc- High Level: Circle the area from different directions to de- tor. termine the best possible landing site in the vicinity. Check the wind direction and speed using pools of water, drift General Considerations: Off-airport operations can be of the plane, branches, grass, dust, etc. Observe the land- extremely rewarding; transporting people and gear to lo- ing approach and departure zone for obstructions such as cations that would be difficult or impossible to reach in trees or high terrain. any other way. Operating off-airport requires high perfor- mance from pilot and aircraft and acquiring the knowledge Intermediate: Level: Make a pass in both directions along and experience to conduct these operations safely takes either side of the runway to check for obstructions and time. Learning and practicing off-airport techniques under runway length. Check for rock size. Note the location of the supervision of an experienced flight instructor will not the touchdown area and roll-out area. Associate land- only make you safer, but also save you time and expense. -
Assessment Method of Fuel Consumption and Emissions of Aircraft During Taxiing on Airport Surface Under Given Meteorological Conditions
sustainability Article Assessment Method of Fuel Consumption and Emissions of Aircraft during Taxiing on Airport Surface under Given Meteorological Conditions Ming Zhang * , Qianwen Huang, Sihan Liu and Huiying Li College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China; [email protected] (Q.H.); [email protected] (S.L.); [email protected] (H.L.) * Correspondence: [email protected] or [email protected] Received: 27 September 2019; Accepted: 31 October 2019; Published: 2 November 2019 Abstract: Reducing fuel consumption and emissions of aircrafts during taxiing on airport surfaces is crucial to decrease the operating costs of airline companies and construct green airports. At present, relevant studies have barely investigated the influences of the operation environment, such as low visibility and traffic conflict in airports, reducing the assessment accuracy of fuel consumption and emissions. Multiple aircraft ground propulsion systems on airport surfaces, especially the electric green taxiing system, have attracted wide attention in the industry. Assessing differences in fuel consumption and emissions under different taxiing modes is difficult because environmental factors were hardly considered in previous assessments. Therefore, an innovative study was conducted based on practical running data of quick access recorders and climate data: (1) Low visibility and taxiing conflict on airport surfaces were inputted into the calculation model of fuel consumption to set up a modified model of fuel consumption and emissions. (2) Fuel consumption and emissions models under full- and single-engine taxiing, external aircraft ground propulsion systems, and electric green taxiing system could accurately estimate fuel consumption and emissions under different taxiing modes based on the modified model. -
Ec-130 Employment ______Compliance with This Instruction Is Mandatory
BY ORDER OF THE COMMANDER AFSOC INSTRUCTION 11-202, VOLUME 17 AIR FORCE SPECIAL OPERATIONS COMMAND 1 JUNE 1997 Flying Operations EC-130 EMPLOYMENT ____________________________________________________________________________________ COMPLIANCE WITH THIS INSTRUCTION IS MANDATORY. This instruction implements AFPD 11-2, Flight Rules and Procedures. It establishes employment procedures for AFSOC EC-130 aircraft and aircrew. It applies to all AFSOC EC-130 aircrews. It applies to the Air National Guard (ANG) when published in the ANGIND 2. OPR: HQ AFSOC/DOVF (Capt Wallace), 193 SOW/OGV (Maj McCarthy) Certified by: HQ AFSOC/DOV (Col Garlington) Pages: 33 Distribution: F; X Chapter 1 -- E-130E Employment Procedures Paragraph Section A -- Employment Concept General .........................................................................................................................1.1 Mission .........................................................................................................................1.2 Communications and Operations Security (COMSEC and OPSEC) ...............................1.3 Crew Rest .....................................................................................................................1.4 Checklists/Inflight Guides..............................................................................................1.5 Definitions ....................................................................................................................1.6 Section B -- Mission Planning and Employment Procedures -
Automation of Taxiing Jaroslav Burs´Ik1, Jakub Kraus1*, Marek Stumperˇ 1
Czech Technical University in Prague Magazine of Aviation Development Faculty of Transportation Sciences 5(1):6-11, 2017, ISSN: 1805-7578 Department of Air Transport DOI: 10.14311/MAD.2017.01.01 Automation of Taxiing Jaroslav Burs´ık1, Jakub Kraus1*, Marek Stumperˇ 1 1Department of Air Transport, Faculty of Transportation Sciences, Czech Technical University in Prague, Prague, Czech Republic *Corresponding author: Czech Technical University in Prague, Faculty of Transportation Sciences, Department of Air Transport, Horska´ 3, 128 03 Prague, Czech Republic, Email: [email protected] Abstract The article focuses on the possibility of automation of taxiing, which is the part of a flight, which, under adverse weather conditions, greatly reduces the operational usability of an airport, and is the only part of a flight that has not been affected by automation, yet. Taxiing is currently handled manually by the pilot, who controls the airplane based on information from visual perception. The article primarily deals with possible ways of obtaining navigational information, and its automatic transfer to the controls. Analyzed wand assessed were currently available technologies such as computer vision, Light Detection and Ranging and Global Navigation Satellite System, which are useful for navigation and their general implementation into an airplane was designed. Obstacles to the implementation were identified, too. The result is a proposed combination of systems along with their installation into airplane’s systems so that it is possible to use the automated taxiing. Keywords Aircraft control — Automation — Safety — Taxiing — Taxiway 1. Introduction The use of GNSS (with or without augmentation) as a single source of navigational data, for navigating on taxiways, has certain limitations. -
Chapter 5: Airport 5: Airport Facility Facilityrequirements Requirements 75 75
LAST UPDATE JULY 2013 Acknowledgements The preparation of this document was financed in part by a grant from the Federal Aviation Administration (Project No: 3-27-0000-07-10), with the financial support of the MnDOT Office of Aeronautics. The contents do not necessarily reflect the official views or the policy of the FAA. Acceptance of this report does not in any way constitute a commitment to fund the development depicted herin. Document prepared by MnDOT Office of Aeronautics and HNTB Corporation. MINNESOTA GO STATE AVIATION SYSTEM PLAN TABLE OF CONTENTS Chapter 1: Introduction and System Goals 1 Chapter 2: Inventory 29 Chapter 3: Forecast 43 Chapter 4: Airline Service 63 ChapterChapter 5: Airport 5: Airport Facility FacilityRequirements Requirements 75 75 Chapter 6: Performance Report 97 Chapter 7: Investment Plan and System Recommendations 161 Chapter 8: A Future Vision of Aviation 195 Appendices 215 CHAPTER 5 AIRPORT FACILITY REQUIREMENTS This page intentionally left blank. MINNESOTA GO STATE AVIATION SYSTEM PLAN Chapter 5 AIRPORT FACILITY REQUIREMENTS CHAPTER 5 AIRPORT FACILITY REQUIREMENTS PAGE 75 This page intentionally left blank. PAGE 76 MINNESOTA GO STATE AVIATION SYSTEM PLAN AIRPORT FACILITY REQUIREMENTS This chapter outlines the state’s airport facility requirements necessary to accommodate aviation demand in Minnesota over the next 20 years as well as the processes and assumptions used to analyze them. Airport facility requirements are useful in planning how to expend anticipated revenues and are identified through consideration of an individual airport’s existing facilities (Chapter 2: Inventory), airport activity forecasts (Chapter 3: Forecast), and certain minimum objectives established for the system (Table 5-2). -
Chapter: 2. En Route Operations
Chapter 2 En Route Operations Introduction The en route phase of flight is defined as that segment of flight from the termination point of a departure procedure to the origination point of an arrival procedure. The procedures employed in the en route phase of flight are governed by a set of specific flight standards established by 14 CFR [Figure 2-1], FAA Order 8260.3, and related publications. These standards establish courses to be flown, obstacle clearance criteria, minimum altitudes, navigation performance, and communications requirements. 2-1 fly along the centerline when on a Federal airway or, on routes other than Federal airways, along the direct course between NAVAIDs or fixes defining the route. The regulation allows maneuvering to pass well clear of other air traffic or, if in visual meteorogical conditions (VMC), to clear the flightpath both before and during climb or descent. Airways Airway routing occurs along pre-defined pathways called airways. [Figure 2-2] Airways can be thought of as three- dimensional highways for aircraft. In most land areas of the world, aircraft are required to fly airways between the departure and destination airports. The rules governing airway routing, Standard Instrument Departures (SID) and Standard Terminal Arrival (STAR), are published flight procedures that cover altitude, airspeed, and requirements for entering and leaving the airway. Most airways are eight nautical miles (14 kilometers) wide, and the airway Figure 2-1. Code of Federal Regulations, Title 14 Aeronautics and Space. flight levels keep aircraft separated by at least 500 vertical En Route Navigation feet from aircraft on the flight level above and below when operating under VFR.