Automated Inspection Of Aircraft
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Author | : |
Publisher | : |
Total Pages | : 90 |
Release | : 1998 |
Genre | : Airplanes |
ISBN | : |
This report summarizes the development of a robotic system designed to assist aircraft inspectors by remotely deploying non-destructive inspection (NDI) sensors and acquiring, processing, and storing inspection data. Carnegie Mellon University studied the task 9f aircraft inspection, compiled the functional requirements for an automated system to inspect skin fastener rows, and developed a conceptual design of an inspection robot. A prototype of the robotic inspection system (the Automated Nondestructive Inspector or ANDI) was developed. The first phase of system development resulted in a laboratory system that demonstrated the abilities to adhere to the surface of an aircraft panel and deploy a standard eddy-current sensor. The second phase of development included enhancing the mechanics, adding video cameras to the robot for navigation, and adding an on-board computer for low-level task sequencing. The second-phase system was subsequently demonstrated at the FAA's Aging Aircraft NDI Validation Center (AANC). During the final phase of development, emphasis was placed on the enhancement of the robot's navigational system through automated recognition of image features captured by the navigation cameras. A significant development effort remains to be accomplished before this robotic inspection technology is suitable for operational deployment. Outstanding development issues include: (1) reducing the weight of the robot so that it is more comfortable to lift and position on the aircraft; (2) improving the mechanical reliability and speed of the system; (3) minimizing the scratching of the skin surface by the suction cups and eddy-current sensors; (4) reduction or elimination of the umbilical cable; and (5) automation of the manually controlled operations. To commercialize the technology, a new mechanical system would need to be designed and built incorporating the lessons of this work.
Author | : C. J. Alberts |
Publisher | : |
Total Pages | : 56 |
Release | : 1994 |
Genre | : Airplanes |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1000 |
Release | : 1998 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. Flight Standards Service |
Publisher | : |
Total Pages | : 100 |
Release | : 1978 |
Genre | : Airplanes |
ISBN | : |
Author | : Robert C. Nelson |
Publisher | : |
Total Pages | : 464 |
Release | : 1998 |
Genre | : History |
ISBN | : |
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author | : |
Publisher | : |
Total Pages | : 702 |
Release | : 1994 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. Office of the Chief of Naval Operations |
Publisher | : |
Total Pages | : 828 |
Release | : 1990 |
Genre | : Aeronautics, Military |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 922 |
Release | : 1993 |
Genre | : Power resources |
ISBN | : |
Author | : Markus G. R. Sause |
Publisher | : Springer Nature |
Total Pages | : 292 |
Release | : 2021 |
Genre | : Aerospace engineering |
ISBN | : 3030721922 |
This open access book presents established methods of structural health monitoring (SHM) and discusses their technological merit in the current aerospace environment. While the aerospace industry aims for weight reduction to improve fuel efficiency, reduce environmental impact, and to decrease maintenance time and operating costs, aircraft structures are often designed and built heavier than required in order to accommodate unpredictable failure. A way to overcome this approach is the use of SHM systems to detect the presence of defects. This book covers all major contemporary aerospace-relevant SHM methods, from the basics of each method to the various defect types that SHM is required to detect to discussion of signal processing developments alongside considerations of aerospace safety requirements. It will be of interest to professionals in industry and academic researchers alike, as well as engineering students. This article/publication is based upon work from COST Action CA18203 (ODIN - http://odin-cost.com/), supported by COST (European Cooperation in Science and Technology). COST (European Cooperation in Science and Technology) is a funding agency for research and innovation networks. Our Actions help connect research initiatives across Europe and enable scientists to grow their ideas by sharing them with their peers. This boosts their research, career and innovation.
Author | : Federal Aviation Administration (FAA) |
Publisher | : Ravenio Books |
Total Pages | : 275 |
Release | : 2016-09-25 |
Genre | : Transportation |
ISBN | : |
The Federal Aviation Administration (FAA) has published the Private Pilot - Airplane Airman Certification Standards (ACS) document to communicate the aeronautical knowledge, risk management, and flight proficiency standards for the private pilot certification in the airplane category, single-engine land and sea; and multiengine land and sea classes. This ACS incorporates and supersedes the previous Private Pilot Practical Test Standards for Airplane, FAA-S-8081-14. The FAA views the ACS as the foundation of its transition to a more integrated and systematic approach to airman certification. The ACS is part of the safety management system (SMS) framework that the FAA uses to mitigate risks associated with airman certification training and testing. Specifically, the ACS, associated guidance, and test question components of the airman certification system are constructed around the four functional components of an SMS: Safety Policy that defines and describes aeronautical knowledge, flight proficiency, and risk management as integrated components of the airman certification system; Safety Risk Management processes through which internal and external stakeholders identify and evaluate regulatory changes, safety recommendations and other factors that require modification of airman testing and training materials; Safety Assurance processes to ensure the prompt and appropriate incorporation of changes arising from new regulations and safety recommendations; and Safety Promotion in the form of ongoing engagement with both external stakeholders (e.g., the aviation training industry) and FAA policy divisions. The FAA has developed this ACS and its associated guidance in collaboration with a diverse group of aviation training experts. The goal is to drive a systematic approach to all components of the airman certification system, including knowledge test question development and conduct of the practical test. The FAA acknowledges and appreciates the many hours that these aviation experts have contributed toward this goal. This level of collaboration, a hallmark of a robust safety culture, strengthens and enhances aviation safety at every level of the airman certification system.