Browse Topic: Airline fleets
Eaton’s Aerospace Group is collaborating with original equipment manufacturers (OEMs) on the advancement of technologies to increase aircraft efficiency, enable aircraft electrification, and reduce carbon emissions. Leveraging our expertise as an intelligent power management company, Eaton’s products and research include hydraulic power packs, electromechanical actuation (EMA), thermal management systems, and sustainable aviation fuel (SAF) compatible systems. Eaton Blended Power TM systems improve efficiency through eliminating all centralized hydraulic circuits with distributed power that is provided by a combination of hydraulic power packs and EMA for a More Electric Aircraft (MEA). EMA systems, including electrical synchronization, reduce the usage of hydraulics and provide additional functionality that benefits the aircraft. With MEA comes higher energy and thermal densities, resulting in the need for advanced thermal management. Eaton’s scalable and modular thermal management
ABSTRACT For the last few decades, Canada's National Research Council (NRC) has been at the forefront in analyzing dynamic systems and developing tools to construct aircraft models based on flight test data. With a fixed and rotary-wing aircraft fleet available, NRC has the capability to perform leading edge R&D System Identification (SI); this worldleading SI technology has been developed and has assisted industry partners, Department of National Defense (DND), and various universities in aircraft simulation and development. As a result, NRC has gained extensive experience in modeling aircraft using SI techniques. In collaboration with CAE, this paper demonstrates the acceleration of the NRC's current flight modeling techniques, highlighting recent advances in Artificial Intelligence (AI) and Machine Learning (ML). A new Bayesian ML software is being developed to identify a 6 degrees of freedom (6-DoF) quasisteady model using simulated flight test data. To achieve this, data from the
ABSTRACT The U.S. Army monitors the structural integrity of its rotary-wing aircraft fleet through annual evaluations and reporting via the Airframe Condition Evaluation (ACE) program. ACE evaluations capture the location and character of structural defects for each aircraft, which are then available for trending and detailed analysis by engineers with the U.S. Army Combat Capabilities Development Command Aviation & Missile Center (CCDC AvMC). As analytic methods are increasingly advanced through the digital thread, CCDC AvMC has sought to improve available trending, modeling, and analysis tools beyond status quo to provide higher fidelity visuals to both aid communication with decision makers, and also to reveal structural defect trends which may not otherwise be evident. This paper will detail the development and utility of the ACE Color Mapping Application within the ACE Mapping Module and its impact on product support of U.S. Army aircraft with regard to airframe structural
ABSTRACT Australia has embarked on an extraordinary reform to design, develop and implement a new and contemporary Defence Aviation Safety Framework. The program seeks to establish a single Defence Aviation Safety Authority (DASA) and issue a comprehensive and integrated suite of Defence Aviation Safety Regulation (DASR) for initial and continuing airworthiness, flight operations, air navigation, aerodromes (inclusive of ship-borne heliports) and safety management systems. While reforms of this scale can often be triggered by reviews into major aircraft accidents, such as The Nimrod Review by Charles Haddon-Cave QC in October 2009, Australia initiated the reform when new aircraft fleets were being introduced and at a time of arguably high-levels of aviation safety. The purpose of this paper is therefore to explain the compelling reason for change; providing a twenty-five-year retrospective analysis of Australia’s previous Defence aviation safety framework to give a rich picture of the
Fuel availability is a security imperative for aircraft fleets, and tactical dependence on fuel will critically tie global fleets to investments in new drag-reduction technologies that optimize fuel utilization. Roberto Guerrero, Deputy Assistant Secretary of the U.S. Air Force for Operational Energy, recently wrote in Defense News that “when we use our assets more efficiently in peacetime, we build a more energy-aware culture that will better prepare our airmen for tomorrow's fight, if and when it happens.” Adopting sustainability measures today directly affects operational and national security, and it benefits us all to find ways to use less. In its 2019 Sustainability Report and Implementation Plan, the Department of Defense states that its sustainability efforts “focus on mission assurance, operational readiness, and cost-effective business practices.” The report goes on to add that, “The Department strives to maximize the efficient use of mission-critical energy, water, and
ABSTRACT The U.S. Army traditionally has used a time-based, on-condition maintenance paradigm that relies on at-aircraft inspections and periodic in-depth phased inspections to determine condition and ensure airworthiness. The result is a significant maintenance burden, both scheduled and unscheduled, and excessive aircraft downtime. The objective of the Aviation Development Directorate (ADD) and Sikorsky Aircraft Corporation (SAC) Capability-Based Operations and Sustainment Technology-Aviation (COST-A) program was to develop and demonstrate an integrated set of high value diagnostics, prognostics, and system health management technologies that reduce scheduled inspections and preventive maintenance while enhancing safety. More than two dozen Prognostics and Health Management (PHM) technologies across six primary rotorcraft systems (propulsion, drive train, airframe/structural, rotor, electrical, and vehicle management) were matured to technology readiness level (TRL) 6. These
ABSTRACT Usage credits may be used to extend retirement lives for structural components. However, any credit substantiation must account for the contribution of conservative usage assumptions to the current level of safety. Structural reliability methods have been proposed as a means to achieve this end. Herein a new, relative method to determine a practically equivalent reliability (and safety) for aircraft fleets is developed using system reliability theory. Simple mathematical examples are used to illustrate the basic principles. A more realistic example based on the AHS Fatigue and Damage Tolerance subcommittee Round Robin problem is presented. These examples show that, even if only a few aircraft in a fleet operate in a severe manner, these aircraft drive the overall fleet reliability. This means that many aircraft may be able to receive credit without having any appreciable change on fleet reliability. A generalized procedure to apply the method to real world problems is
ABSTRACT The U.S. Army traditionally has used a time-based, on-condition maintenance paradigm that relies on at-aircraft inspections and periodic in-depth phase inspections to determine condition and ensure airworthiness. The result is a significant maintenance burden, both scheduled and unscheduled, and excessive aircraft downtime. The objective of the Aviation Development Directorate (ADD) and Sikorsky Aircraft Corporation (SAC) Capability-Based Operations and Sustainment Technology-Aviation (COST-A) program was to develop and demonstrate an integrated set of high value diagnostics, prognostics, and system health management technologies that reduce scheduled inspections and preventive maintenance while enhancing safety. More than two dozen Prognostics and Health Management (PHM) technologies across six primary rotorcraft systems (propulsion, drive train, airframe/structural, rotor, electrical, and vehicle management) were matured to technology readiness level (TRL) 6. These
Industry is in the midst of new initiatives to develop lighter, stronger aero engine fan blades. The ongoing competitive battle to supply the engines for tens of thousands of new-generation commercial airplanes that are predicted to be required to satisfy airline demands over the next two decades has seen the major powerplant suppliers developing twin roadmaps for the future. While long-term prospects for true game-changing engine configurations remain real, and advanced work continues on ultra-high-bypass ducted-fan and openrotor solutions, other efforts are being directed by the major players that aim at achieving ever-better performance out of improved aerodynamic design and advanced materials manufacturing techniques applied to more evolutionary turbofan configurations.
This document sets forth design and operational recommendations concerning the human factors issues and criteria for airborne terrain separation assurance systems. The visual and aural characteristics are covered for both the alerting components and terrain depiction/situation components. The display system may contain any one or a combination of these components. Although the system functionality assumed for this document exemplifies commercial aircraft implementation, the recommendations do not exclude other fixed wing aircraft types. Because of their unique operations with respect to terrain, rotorcraft will be addressed in a separate document. The assumptions about the system that guided and bounded the recommendations included: the system will have a human centered design based on the "lessons learned" from past systems; the system is not intended to replace the Ground Proximity Warning System (GPWS) function; the system is an on-board system that is not dependent on ground
NASA's Strategic Plan for the Aerospace Technology Enterprise includes ambitious objectives focused on affordable air travel, reduced emissions, and expanded aviation-system capacity. NASA Dryden Flight Research Center, in cooperation with NASA Ames Research Center, the Boeing Company, and the University of California, Los Angeles, has embarked on an autonomous-formation-flight project that promises to make significant strides towards these goals.
This article examines trends and issues in the regional aircraft industry through the eyes of Aerospace Congress & Exhibition (ACE) host company Bombardier Aerospace. It also takes a look at ACE, which addresses topics such as aviation safety, manufacturing; automated fastening, and aircraft design. The regional aircraft industry has seen a bit of a growth spurt post 9/11. In fact, according to the Federal Aviation Administration (FAA), regional jets will lead the recovery in commercial passenger traffic over the next decade. Regional airlines are more flexible than major airlines in response to rapidly changing industry conditions, providing them with the unique ability to service a wide variety of market types, both efficiently and effectively. John Holding, the Executive Vice President of Engineering and Product Development for Bombardier Aerospace who is serving as Executive Chair for the 2003 Aerospace Congress & Exhibition (see sidebar on next page), has witnessed the shift in
JUST YESTERDAY, simulation tackled the issues of digital technology in a new generation of aircraft, but here we face another quantum leap as we look beyond the Boeing 757/767 model airplanes. The engineering simulator has evolved, over a period of 25 years, from a relatively modest beginning, to a sophisticated design tool essential to the development of new airplanes and weapons systems. The decisions involved in the management of simulation facilities has also evolved from choosing a modest “take-what-you-can-get” product line, to picking from warehouses full of “goodies,” all of which have their associated payoffs. As a background, the authors will attempt to outline from personal experience and long-term history with engineering simulation, the steps that were taken to reach the present level of sophistication in engineering simulators at Boeing. Engineering flight simulators have assumed an increasingly crucial role in the development and testing of new product lines in the
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