(12) United States Patent (10) Patent No.: US 7.546,280 B1 Ershov (45) Date of Patent: *Jun

Total Page:16

File Type:pdf, Size:1020Kb

(12) United States Patent (10) Patent No.: US 7.546,280 B1 Ershov (45) Date of Patent: *Jun USOO754628OB1 (12) United States Patent (10) Patent No.: US 7.546,280 B1 Ershov (45) Date of Patent: *Jun. 9, 2009 (54) USE OF NEURAL NETWORKS FOR 5,819,245 A * 10/1998 Peterson et al. ............... TO6, 16 KEYWORD GENERATION 6,304.864 B1* 10/2001 Liddy et al. ................... TO6.15 (75) Inventor: Alexander V. Ershov, Sergiev Posad (RU) (Continued) OTHER PUBLICATIONS (73) Assignee: Quintura, Inc., Alexandria, VA (US) "Inhibitory connections in the assembly neural network for texture (*) Notice: Subject to any disclaimer, the term of this segmentation'. A. Goltsev, Donald C. Wunsch, Neural Networks, patent is extended or adjusteds under 35 WO 1. 11, No.O. 5, Jul. 1998, pppp. 951-962.* U.S.C. 154(b) by 379 days. (Continued) is- Primary Examiner David R Vincent This patent is Subject to a terminal dis Assistant Examiner Mai T Tran Ca10. (74) Attorney, Agent, or Firm Bardmesser Law Group (22) Filed: Sep. 27, 2006 A system for identifying keywords in search results includes Related U.S. Application Data a plurality of neurons connected as a neural network, the (63) Continuation-in-part of application No. 1 1/468,692. neurons being associated with words and documents . An activity regulator regulates a minimum and/or maximum filed on Aug. 30, 2005, now Pat. No. 7,475,072. number of neurons of the neural network that are excited at (60) Provisional application No. 60/735,858, filed on Nov. any given time. Means for displaying the neurons to a user 14, 2005, provisional application No. 60/722,412, and identifying the neurons that correspond to keywords can filed on Oct. 3, 2005, provisional application No. be provided. Means for changing positions of the neurons 60/719,975, filed on Sep. 26, 2005. relative to each other based on input from the user can be s- a-s s provided. The change in position of one neuron changes the (51) Int. Cl. keywords. The input from the user can be dragging a neuron G06E I/00 (2006.01) on a display device, or changing a relevance of two neurons 52) U.S. C 706/20: 707/6 relative to each other. The neural network can be excited by a (52) ir grgrrr. s query that comprises words selected by a user. The neural (58) Field of Classification Search ................... 706/20; network can be abidirectional network. The user can inhibit 707/6 neurons of the neural network by indicating irrelevance of a See application file for complete search history. document. The neural network can be excited by a query that (56) References Cited identifies a document considered relevant by a user. The neu ral network can also include neurons that represent groups of U.S. PATENT DOCUMENTS words. The neural network can be excited by a query that identifies a plurality of documents considered relevant by a 5,086.479 A * 2/1992 Takenaga et al. ............ 382,157 user, and can output keywords associated with the plurality of 5.535,303 A * 7/1996 Ekchian et al. ............... T06/26 documents. 5,546,503 A * 8/1996 Abe et al. ..................... 7O6.25 5,548,683 A * 8/1996 Engel et al. ................... T06/20 24 Claims, 5 Drawing Sheets INACTIVENEURON - XCITEDNEURON m INHIBITING NEURON ... MAGNIFYING CONNECTION ... INHIBITING CONNECTION C C M K EY O US 7.546,280 B1 Page 2 U.S. PATENT DOCUMENTS OTHER PUBLICATIONS 6,463,423 B1 * 10/2002 Wada .......................... TO6.15 "Structure of Neural Assembly” by E. M. Kussul, T. N. Baidyk, 6,574,632 B2 * 6/2003 Fox et al. .................... 707/102 Neuroinformatics and Neurocomputers, 1992, RNNS/IEEE Sympo 7,296,009 B1 * 1 1/2007 Jiang et al. ..................... 707/3 sium on, s M.A. Sir 423-434. 1 ck “An assembly neural network for texture segmentation'. A. Goltsev 2003/02169 19 A1* 11/2003 Roushar ..................... TO4,260 Neural Networks, vol. 9, No. 4, Jun. 1996, pp. 643-653.* 2005/024.6296 A1* 11/2005 Ma et al. ...................... TO6/12 2007/0009151 A1 1/2007 Pittman et al. .............. 382,159 * cited by examiner U.S. Patent Jun. 9, 2009 Sheet 1 of 5 US 7.546,280 B1 O - INACTIVE NEURON (D - EXCITED NEURON () - INHIBITING NEURON -s ...... MAGNIFYING CONNECTION w ...... INHIBITING CONNECTION yY WORDS OBJECTS SENTENCES DOCUMENTS : i APPLE & u-- - - o Ys - C&N I-C)FRUIT ( -" Q-N S.ra sea-------A------J. us &\\ is y M. i arr rra combuTER)-\\- //O- Kirst Sis-Avi Su's v Y, 's-ck Y y Y.\ S- v --- -1 n . N k \- N l Y y w KEYBOARD O^^g. HARDWARE DO--- s y v. \\ O Y i- I \ l \ Y- v \ --- ^ X --Y. 1 -ol. \ ar. \ & N Ex ser sy - | ADAM re-Y N O - \-ANATOMY i - N res.~~ - \ M i S. O. o- or i sr S. Y. k LOUID CIDER i. 1- Y'^^ ' Y- \-- ...r FIG. 1 U.S. Patent Jun. 9, 2009 Sheet 2 of 5 US 7.546,280 B1 O U.S. Patent Jun. 9, 2009 Sheet 3 of 5 US 7.546,280 B1 U.S. Patent Jun. 9, 2009 Sheet 4 of 5 US 7.546,280 B1 U.S. Patent Jun. 9, 2009 Sheet 5 of 5 US 7.546,280 B1 PrOCeSSOr 301 302 FIG. 3 Main Memory 308 Secondary Memory 310 Hard Disk Drive 312 Removable Storage Removable Drive 314 Storage Unit 318 Removable Interface 320 Storage Unit 422 NetWOrk Interface 323 COmmunicationS Path 326 US 7,546,280 B1 1. 2 USE OF NEURAL NETWORKS FOR and managing the search process. Keywords identify what the KEYWORD GENERATION documents are “about they may be words that are men tioned in the documents themselves, or they may be concepts CROSS-REFERENCE TO RELATED that are related to the meaning of the document, and which APPLICATIONS capture, in one or a handful of words, the meaning of the document. Accordingly, there is a need in the art for an effec This application is a continuation-in-part of U.S. patent tive and efficient system and method for identifying keywords application Ser. No. 1 1/468,692, filed on Aug. 30, 2006, relating to context-based searching. entitled CONTEXT-BASED SEARCH VISUALIZATION AND CONTEXT MANAGEMENT USING NEURAL 10 SUMMARY OF THE INVENTION NETWORKS, which is a non-provisional of U.S. Provisional Patent Application No. 60/719,975, filed on Sep. 26, 2005, Accordingly, the present invention is related to use of neu entitled CONTEXT-BASED SEARCH VISUALIZATION ral networks for keyword generation that substantially obvi USING NEURAL NETWORKS, and is a non-provisional of ates one or more of the disadvantages of the related art. U.S. Provisional Patent Application No. 60/735,858, filed on 15 In one aspect, there is provided a system for identifying Nov. 14, 2005, entitled ONE-CLICK SEARCHING SYS keywords in search results including a plurality of neurons TEMAND METHOD, which are both incorporated by ref connected as a neural network, the neurons being associated erence herein in their entirety. with words and documents. An activity regulator regulates a This application is a non-provisional of U.S. Provisional minimum and/or maximum number of neurons of the neural Patent Application No. 60/722,412, filed on Oct. 3, 2005, network that are excited at any given time. Means for display entitled USE OF NEURAL NETWORKS FOR KEYWORD ing the neurons to a user and identifying the neurons that GENERATION, which is incorporated by reference herein in correspond to keywords can be provided. Means for changing their entirety. positions of the neurons relative to each other based on input from the user can be provided. The change in position of one BACKGROUND OF THE INVENTION 25 neuron changes the keywords. The input from the user can be dragging a neuron on a display device, or changing a rel 1. Field of the Invention evance of two neurons relative to each other. The neural The present invention relates to generation of keywords for network can be excited by a query that comprises words document digesting, and, more particularly, to keyword gen selected by a user. The neural network can be abidirectional eration for search engine output as a means for assisting the 30 network. The user can inhibit neurons of the neural network user in selecting relevant documents and search results. by indicating irrelevance of a document. The neural network 2. Description of the Related Art can be excited by a query that identifies a document consid The World Wide Web (“web”) contains a vast amount of ered relevant by a user. The neural network can also include information. Locating a desired portion of the information, neurons that represent groups of words. The neural network however, can be challenging. This problem is compounded 35 because the amount of information on the web and the num can be excited by a query that identifies a plurality of docu ber of new users inexperienced at web searching are growing ments considered relevant by a user, and can output keywords rapidly. associated with the plurality of documents. In another aspect, a system, method and computer program Search engines attempt to return hyperlinks to web pages product for identifying keywords, include a plurality of neu in which a user is interested. Generally, search engines base 40 their determination of the users interest on search terms rons arranged into a neural network comprising a plurality of (called a search query) entered by the user. The goal of the layers, the layers including words, objects and documents. A search engine is to provide links to high quality, relevant plurality of connections connect the neurons, such that each neuron is connected to only some of the other neurons.
Recommended publications
  • NTSB-AAR-72-18 TECHNICAL REPORT STANDARD Title PAGE
    SA-424 FILE NO. 1-0002 AIRCRAFT ACCIDENT REPORT WESTERN AIR LINES, INC. BOEING 720-047B,N3166 ONTARIO INTERNATIONAL AIRPORT ONTARIO, CALIFORNIA MARCH 31, 1971 ADOPTED: JUNE 7, 1972 NATIONAL TRANSPORTATION SAFETY BOARD Washington, 0. C. 20591 REPORT NUMBER: NTSB-AAR-72-18 TECHNICAL REPORT STANDARD TiTLE PAGE . Report No. 2.Government Accession No. 3.Recipient's Catalog No. NTSB-AAR-72-18 I. Title and Subtitle 5.Report Date Aircraft Accident Report - Western Air Lines, InC., Sune 7, 1972 Roeing 720-047B, N3166, Ontario International Airport, 6.Performing Organization Ontario. California, March 31, 1971 Code '. Author(s) 8.Performing Organization Report No. I. Performing Organization Name and Address IO.Work Unit No. Bureau of Aviation Safety 11 .Contract or Grant No. National Transportation Safety Board Washington, D. C. 20591 13.Type of Report and Period Covered 12.Sponsoring Agency Name and Address Aircraft Accident Report March 31, 1971 NATIONAL TRANSPORTATION SAFETY BOARD Washington, 0. C. 20591 14.Sponsoring Agency Code 15.Supplementary Notes I6.Abstract Flight 366, a Boeing 720B, on a proficiency check flight, yawed and rolled out of control, and crashed while in the process of executing a 3-engine missed- approach from a simulated engine-out ILS instrument approach. The five crew- members and only occupants died in the crash. The weather conditions at Ontario were 600 feet overcast, with 3/4-mile visibility in fog, haze, and smoke. The National Transportation Safety Board determines that the probable cause of this accident was the failure of the aircraft rudder hydraulic actuator support fitting. The failure of the fitting resulted in the inapparent loss Of left rudder control which, under the conditions of this flight, precluded the pilotk ability to maintain directional control during a simlated engine-out missed- approach.
    [Show full text]
  • B-162897 Aircraft Owned Or Leased By
    Dear Mr, Thompson: Reference is made to your letter of February 10, 1970, requesting that we update information which we furnished to you in a report dated March 4, 1968, relative to aircraft owned or leased by the Federal Avia- 1 tion Administration (FAA). In accordance with this request, we are fur- nishing you the following information. 1. Inventory of active aircraft owned as of June 30, 1967, 1968, 1969, and January 1, 1970 (enclosure I). 2. Installed passenger capacity and cost of aircraft owned as of June 30, 1967, and January 1, 1970 (enclosure II). 3. Aircraft leased or on loan during the period July 1, 1967, through June 30, 1969 (enclosure III). 4. Aircraft mazntenance, maJor overhaul, and modification costs by aircraft type, for fiscal years 1968 and 1969 (enclosure IV). 5. Average cost per flxght hour by aircraft type, fiscal years 1968 and 1969 (enclosure V>. 6. Aircraft utilization by aircraft type and maJor cate- gories, fiscal years 1968 and 1969 (enclosure VI). 7. Utilization and cost of open market rental aircraft, fiscal years 1968 and 1969 (enclosure VII). In addition, you requested that we advise you of the progress that has been made in establishing a uniform maintenance and operating cost re- porting system for all FAA owned and leased aircraft. As shown zn our March 4, 1968, report, FhCl had 101 aircraft which cost approximately $46 mzlllon 1n its inventory of active aircraft as of June 30, 1967. On January 1, 1970, the number of active air craft had decreased Co 98; however, the cost of the aircraft in the inventory was approximately $52 million, This increase was the net result of.
    [Show full text]
  • Canada Aviation and Space Museum
    CANADA AVIATION AND SPACE MUSEUM BOEING MODEL 720B PRATT & WHITNEY CANADA FLYING EXPERIMENTAL TEST BED REGISTRATION C-FETB Introduction The practical era of jet-age passenger transport aircraft officially dawned when the British de Havilland Company D.H.106 Comet made its premiere flight to great acclaim from the Hatfield, Hertfordshire aerodrome in England on 27 July 1949. Catering to British and mid to long-range routes to European, Middle Eastern and overseas destinations, the Comet series of airliners carried their passengers aloft in luxurious opulence for more than twenty years. Military and test derivatives followed suit and these continued flying for many decades, including two Comets for the Royal Canadian Air Force (RCAF). Just 14 days later, across the vast Atlantic Ocean, in the small town of Malton, Ontario, Canada, a new aviation company called Avro Canada successfully accomplished the same task with much less fanfare and accolades. Avro sent its small, medium-range, turbo-jet transport, called the C-102 Jetliner, aloft for its first flight, inaugurating the dreamed potential for such a unique travel experience for the public on the North American continent. United States Air Force personnel found the aircraft favourable when they tried it out on flights at Wright Field, Ohio in March 1951. However, this Canadian dream didn’t last for long. The modestly successful Comet-series didn’t shine as brightly as its popular name when a series of tragic, fatal accidents to production civil aircraft nearly snuffed out its very existence. Following design rectification’s, the Royal Air Force continued to employ Comets in versatile roles, such as modifying the design into the Nimrod.
    [Show full text]
  • Fuel Consumption Fc (SFC) PERFORMANCE of CIVIL AIRCRAFTS in 1960S
    Inspired by Physics – Just How Big is Disruptive? Design a FlyingJumbo Jet in Just One Hour ESADE Executive Program, Markus Nordberg November 15, 2017 Development & Innovation Unit (CERN) WHY ARE WE DOING THIS EXERCISE? • Like the experiments at CERN, the aerodynamic design of aircraft are also much determined by the was of physics • We wish to give an example of physics-driven experimentation process, requiring cross-disciplinary collaboration • Here, we wish to bring in business management, engineering and design • They all contribute, even if emphasis is here on aerodynamics • Prototyping is a good way to start to learn about the design process (even if incremental) • If I am able to design a stupid jumbo, well, then I can …. • Physics and Design Thinking is Fun PLEASE REMEMBER THAT … • … Modern aircraft designers are not taught like this • (The difference between this intro and designing real airliners is only about 10 000 hours … But make no mistake, our jumbo will fly) • … Modern aircrafts are not designed by beginners • … You will not be a certified aircraft designer after this course • … Folks at CERN can’t do anything • (Alas - but they do know how far the laws of physics will take you) WHO DESIGNED THIS? OR THIS? NATURE SEEMS TO KNOW ITS SHAPES WELL ALL YOU NEED TODAY TO KNOW ABOUT FLYING Finesse F = L/D Aspect Ratio Ar = b²/S b S Shape (F) Performance (engines) codecogs Well, Almost … F = ma or, in terms of pressure (assuming air ~ fluid) W/S ~ 0.3 x σ x v² Where: W = weight of the object (N) S = wing area (m²) σ = density of
    [Show full text]
  • Air Transport
    The History of Air Transport KOSTAS IATROU Dedicated to my wife Evgenia and my sons George and Yianni Copyright © 2020: Kostas Iatrou First Edition: July 2020 Published by: Hermes – Air Transport Organisation Graphic Design – Layout: Sophia Darviris Material (either in whole or in part) from this publication may not be published, photocopied, rewritten, transferred through any electronical or other means, without prior permission by the publisher. Preface ommercial aviation recently celebrated its first centennial. Over the more than 100 years since the first Ctake off, aviation has witnessed challenges and changes that have made it a critical component of mod- ern societies. Most importantly, air transport brings humans closer together, promoting peace and harmo- ny through connectivity and social exchange. A key role for Hermes Air Transport Organisation is to contribute to the development, progress and promo- tion of air transport at the global level. This would not be possible without knowing the history and evolu- tion of the industry. Once a luxury service, affordable to only a few, aviation has evolved to become accessible to billions of peo- ple. But how did this evolution occur? This book provides an updated timeline of the key moments of air transport. It is based on the first aviation history book Hermes published in 2014 in partnership with ICAO, ACI, CANSO & IATA. I would like to express my appreciation to Professor Martin Dresner, Chair of the Hermes Report Committee, for his important role in editing the contents of the book. I would also like to thank Hermes members and partners who have helped to make Hermes a key organisa- tion in the air transport field.
    [Show full text]
  • Air Travel, Life-Style, Energy Use and Environmental Impact
    Air travel, life-style, energy use and environmental impact Stefan Kruger Nielsen Ph.D. dissertation September 2001 Financed by the Danish Energy Agency’s Energy Research Programme Department of Civil Engineering Technical University of Denmark Building 118 DK-2800 Kgs. Lyngby Denmark http://www.bvg.dtu.dk 2001 DISCLAIMER Portions of this document may be illegible in electronic image products. Images are produced from the best available original document Report BYG DTU R-021 2001 ISSN 1601-2917 ISBN 87-7877-076-9 Executive summary This summary describes the results of a Ph.D. study that was carried out in the Energy Planning Group, Department for Civil Engineering, Technical University of Denmark, in a three-year period starting in August 1998 and ending in September 2001. The project was funded by a research grant from the Danish Energy Research Programme. The overall aim of this project is to investigate the linkages between energy use, life style and environmental impact. As a case of study, this report investigates the future possibilities for reducing the growth in greenhouse gas emissions from commercial civil air transport, that is passenger air travel and airfreight. The reason for this choice of focus is that we found that commercial civil air transport may become a relatively large energy consumer and greenhouse gas emitter in the future. For example, according to different scenarios presented by Intergovernmental Panel on Climate Change (IPCC), commercial civil air transport's fuel burn may grow by between 0,8 percent a factor of 1,6 and 16 between 1990 and 2050. The actual growth in fuel consumption will depend on the future growth in airborne passenger travel and freight and the improvement rate for the specific fuel efficiency.
    [Show full text]
  • The Propulsive-Only Flight Control Problem
    NASA-CR-202408 The Propulsive-Only Flight Control Problem by Daniel J. Biezad Cal Poly State University San Luis Oblspo, CA 93407 Abstract aircraft remained controllable in-flightby the skillful application of thrust, but the extreme difficulty of this Attitude control of aircraft using only the task, combined with the stress of the emergency, did throttles is investigated The long time constants of not allow a successful landing. both the engines and of the aJmraft dynamics, The fundamental problem is that an alrcratt together with the coupling between longitudinal and cannot be easily and predictably maneuvered by the lateral aircraft modes, make piloted flightwith failed pilot with the throttles alone. Although the control control surfaces hazardous, especially when power is often sufficient to fly the aircraft, the long time attempting to land. This research documents the constants and couplings between dynamic modes results of in-flight operation using simulated failed make pilot control uncertain and precarious for flight controls and ground simulations of piloted demanding tasks such as landing. Exposure to these propulsive-only control to touchdown. Augmentation situations in training simulations may alleviate the control laws to assist the pilot are described using gross misapplication of throttles, but will not eliminate both optimal contre_ and classical feedback methods. the potential for a serious accident to occur. Piloted simulation using augmentation shows that A complimentary solutionto more training simple and effective augmented control can be would be the addition of a simple, low cost pilot-assist achieved in a wide variety of lailed configurations. mode to be activated by the pilot in the event of complete failure of the high bandwidth pitch and roll Nomenclature controls.
    [Show full text]
  • Fsd Mar93.Pdf
    During Adverse Conditions, Decelerating to Stop Demands More from Crew and Aircraft Hydroplaning, gusting cross winds and mechanical failures are only a few of the factors that contribute to runway overrun accidents and incidents after landing or rejecting a takeoff. Improvements in tire design, runway construction and aircraft systems reduce risks, but crew training remains the most important tool to stop safely. by Jack L. King Aviation Consultant Decelerating an aircraft to a stop on a runway traction during wet-weather operations and can become significantly more critical in ad- the use of anti-skid braking devices, coupled verse conditions, such as heavy rain in mar- with high-pressure tires, has reduced greatly ginal visibility with gusting cross winds. Add the risk of hydroplaning. Still, accident and the surprise of a malfunction, which requires incident statistics confirm that several major a high-speed rejected takeoff (RTO) or a con- runway overrun accidents each year are caused trolled stop after a touchdown on a slightly by unsuccessful braking involving either a high- flooded runway, and a flight crew is challenged speed landing or an RTO on a wet runway to prevent an off-runway excursion. surface; the factors involved in decelerating to a controlled stop are very similar in these Research findings and technological advances two situations. in recent years have helped alleviate, but not eliminate, the hazards associated with takeoff Overrun Accidents and landing in adverse weather. The U.S. Na- tional Aeronautics and Space Administration Continue to Occur (NASA) and the U.S. Federal Aviation Admin- istration (FAA) conducted specialized tests on A recent Boeing Company study reported that tire spin-up speeds after touchdown rather than during 30 years of jet transport service there spin-down speeds in rollout that confirm that have been 48 runway overrun accidents with hydroplaning occurs at substantially lower more than 400 fatalities resulting from RTOs speeds than noted previously.
    [Show full text]
  • Boeing History Chronology Boeing Red Barn
    Boeing History Chronology Boeing Red Barn PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 Boeing History Chronology PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 PRE -1910 1910 Los Angeles International Air Meet Museum of Flight Collection HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1881 Oct. 1 William Edward Boeing is born in Detroit, Michigan. 1892 April 6 Donald Wills Douglas is born in Brooklyn, New York. 1895 May 8 James Howard “Dutch” Kindelberger is born in Wheeling, West Virginia. 1898 Oct. 26 Lloyd Carlton Stearman is born in Wellsford, Kansas. 1899 April 9 James Smith McDonnell is born in Denver, Colorado. 1903 Dec. 17 Wilbur and Orville Wright make the first successful powered, manned flight in Kitty Hawk, North Carolina. 1905 Dec. 24 Howard Robard Hughes Jr. is born in Houston, Texas. 1907 Jan. 28 Elrey Borge Jeppesen is born in Lake Charles, Louisiana. HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1910 s Boeing Model 1 B & W seaplane HOME PRE-1910 1910 1920 1930 1940 1950 1960 1970 1980 1990 2000 2010 1910 January Timber baron William E. Boeing attends the first Los Angeles International Air Meet and develops a passion for aviation. March 10 William Boeing buys yacht customer Edward Heath’s shipyard on the Duwamish River in Seattle. The facility will later become his first airplane factory. 1914 May Donald W. Douglas obtains his Bachelor of Science degree from the Massachusetts Institute of Technology (MIT), finishing the four-year course in only two years.
    [Show full text]
  • Lossoflicensebrochureenglish.Pdf
    Unexpected illness or injury can pose many problems for Pilots. GBG’s Loss of License Insurance provides peace of mind with a comprehensive package made to suit your individual needs. • Annual plan that follows pilots worldwide • Maximum benefit amount of USD$500,000 • Covers pilots of commercial airliners and business jets, plus other types of business aircraft including twinjets, corporate helicopters and air taxis • Flexibility of covering both temporary and permanent disabilities • Coverage for For Pilots and First Officers that hold a Commercial Pilots License or an Air Transport License • Sickness and/or Bodily injury Benefits: Eligibility up to age 60 • Upon attainment of age 60, benefits for “accident only” coverage continue up to the sooner of retirement age or age 65. Schedule Of Benefits BENEFIT PLAN BENEFIT MAXIMUM Permanent Total Disablement by A 100% of the Sum Insured Bodily Injury or Sickness Permanent Total Disablement by B 25% of the Sum Insured Classified Illness or Psychological Illness Temporary Total Disablement by C 2% of the Sum Insured per month* Bodily Injury or Sickness Temporary Total Disablement by D 0.5% of the Sum Insured per month* Classified Illness or Psychological Illness *TTD monthly payment not to exceed 75% of monthly salary. Payments made on Temporary Total Disablement will erode the Permanent Total Disablement sum insured. One payment of 100% of the Sum Insured shall exhaust the Sum Insured per Insured Person. In the event the Insured Person holds more than one License, all Licenses must be cancelled for a claim to be considered. Permanent Total Disablement means the Insured Person is totally unable to perform the essential duties of their own previous occupation as a license holder, and which lasts 180 days and at the end of that period is beyond hope of improvement.
    [Show full text]
  • On Time. Every Time. Airbus Thsa Overhaul|Exchange Boeing Hsta Overhaul
    Leading Manufacturer and FAA/Repair Station For Commercial and Military Aircraft Actuation Systems ON TIME. EVERY TIME. AIRBUS THSA OVERHAUL|EXCHANGE BOEING HSTA OVERHAUL|EXCHANGE BOEING HSTA AND AIRBUS THSA OVERHAUL AND FORWARD EXCHANGES AVAILABLE AIRBUSAIRBUS Why pay more from the OEM when you can get quality service at a competitive price? As a leading FAA, EASA, and CAAC certified Repair Station, Skytronics, Inc. provides complete repair and exchange services for Airbus Trimmable Horizontal AIRBUS MODELS Stabilizer Actuators (THSAs). Model P/N EASA and FAA Airworthiness Directives (AD) and Airbus A300 47142 Series Airbus Service Bulletins (SB) require repetitive Airbus A300-600 47142 Series detailed inspections of the THSA for continued Airbus A310 47142 Series airworthiness. You can rely on Skytronics for Airbus A318 47145 Series inspection, test, repair and overhaul requirements Airbus A319 47145 Series with SAME DAY forward exchange service to Airbus A320 47145 Series avoid AOGs. Airbus A321 47145 Series Airbus A330/A340 47147 Series Airbus A330 47172 Series Airbus A340 47175 Series ON TIME. EVERY TIME. SKYTRONICS SPECIALIZES IN THE FOLLOWING: • Test and Repairs • Hydraulic Motor Test, Repairs, • Overhauls & Exchange Units Overhauls and Replacements • Ball Screw Assembly, Screw Shafts, Ballnut Test, • Hydraulic Brake Test, Repairs, Repairs, Overhauls and Replacements. Overhauls and Replacements State-of-the-Art In-House Ball Screw Overhaul and Testing Capabilities Skytronics, established in 1956, is an FAA, EASA and CAAC certified repair station committed to providing superior repair and overhaul services that enhance the safety and operational performance of your fleet. We maintain an extensive inventory and have the fastest turn-time in the business.
    [Show full text]
  • When Boeing Is Dreaming – a Review
    Journal of Aircraft and Spacecraft Technology Review When Boeing is Dreaming – a Review 1Relly Victoria Virgil Petrescu, 2Raffaella Aversa, 3Bilal Akash, 4Juan Corchado, 2Antonio Apicella and 1Florian Ion T. Petrescu 1ARoTMM-IFToMM, Bucharest Polytechnic University, Bucharest, (CE), Romania 2Advanced Material Lab, Department of Architecture and Industrial Design, Second University of Naples, 81031 Aversa (CE), Italy 3Dean of School of Graduate Studies and Research, American University of Ras Al Khaimah, UAE 4University of Salamanca, Spain Article history Abstract: Boeing is an aeronautical and aerospace manufacturer. Its head Received: 17-04-2017 office is located in Chicago, Illinois. Its two largest plants are located in Revised: 09-05-2017 Wichita, Kansas and Everett, near Seattle. This aircraft manufacturer Accepted: 07-07-2017 specializes in the design of civil aircraft, but also in military aircraft, helicopters Corresponding Author: and in satellites and rockets with its Boeing Defense, Space and Security Florian Ion Tiberiu Petrescu division. In 2012, it ranks second in world military equipment sales. The ARoTMM-IFToMM, Bucharest company was born on July 15, 1916, thanks to its two fathers William E. Polytechnic University, Boeing and George Conrad Westervelt and is named "B and W". Shortly Bucharest, (CE), Romania afterwards, his name became "Pacific Aero Products" and finally "Boeing E-mail: [email protected] Airplane Company". In 1938, Boeing commissioned the 307 Stratoliner; It was the first airplane with pressurized cabin; He was able to fly at a cruising altitude of 20,000 feet, so above most weather disturbances, making him the strongest aircraft in the Boeing fleet. In response to the concentration move in the US defense industry initiated by its competitor Lockheed in 1995, Boeing acquired Rockwell International's space and defense operations in August 1996 for $3.2 billion.
    [Show full text]