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Anapathur V Ramesh

from Bothell, WA
Age ~62
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Also known as:
Anapathur Dr Ramesh, Anapathur E Ramesh, Ramesh Anapathur, R Ramesh
Phone and address:
18017 27Th Dr SE, Bothell, WA 98012
(425) 489-8415
Related to:
Anapathur R VNalini V Ramesh, 56Karthik Ramesh, 29
Connected to:
Akshay Ramesh, 33Amit Ramesh, 59Amy K Ramesh, 52Anthony Ramesh, 56Aparna T Ramesh, 36Arun Ramesh, 39Balakrishnan Ramesh, 65David E Ramesh, 57Jayanthi G Ramesh, 66Jayashree Ramesh, 59

Anapathur Ramesh Phones & Addresses

  • 18017 27Th Dr SE, Bothell, WA 98012 (425) 489-8415
  • Fountain Hills, AZ
  • Pittsburgh, PA
  • 450 N Mathilda Ave #L204, Sunnyvale, CA 94085 (408) 286-2805
  • Everett, WA
  • Monroeville, PA
  • Lynnwood, WA
  • Great Lakes, IL
  • Snohomish, WA
  • Norristown, PA

Work

Company: The boeing company Position: Systems engineer

Education

Degree: Master of Science, Masters School / High School: Duke University 1991 to 1992 Specialities: Computer Science

Skills

Reliability and Dependability Modeling a... • Stochastic Models • Airplane Systems Safety and Certificatio... • Boolean Stochastic Models • Markov Models and Processes • Numerical Analysis and Linear Algebra • Dependability Analysis Tools and Tool De... • Reliability Statistics and Life Data Ana... • Data Analytics and Statistics • Business Intelligence Toolsets • Structural Engineering and Analysis • Finite Element Analysis and Computationa... • Web and Data Base Technologies • Fault Analysis • Petri Nets • Discrete Event Simulation • Earned Value Management • Engineering Management • Avionics • Aerospace • Space Systems • Systems Engineering • Stochastic Modeling • Configuration Management • System Design • Requirements Management • Engineering • Spacecraft

Interests

Applied Mechanics and Finite Elements • Web and Data Management Technologies • Airplane Certification Analysis • Aerospace Recommended Practices • Reliability Engineering • Statistics and Data Analytics • Stochastic Models • Software Engineering and Architectures • Statistical Models • Reliability • Structural Engineering and Analysis

Industries

Aviation & Aerospace

Resumes

Resumes

Anapathur Ramesh Photo 1

Chair, Sg-3: Ml Design And Verification

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Location:
Bothell, WA
Industry:
Aviation & Aerospace
Work:
The Boeing Company
Systems Engineer
Education:
Duke University 1991 - 1992
Master of Science, Masters, Computer Science Duke University 1987 - 1991
Doctorates, Doctor of Philosophy, Engineering, Philosophy Duke University 1985 - 1987
Master of Science, Masters, Engineering Indian Institute of Technology, Madras 1980 - 1985
Bachelors, Bachelor of Technology, Civil Engineering
Skills:
Reliability and Dependability Modeling and Analysis
Stochastic Models
Airplane Systems Safety and Certification Analysis
Boolean Stochastic Models
Markov Models and Processes
Numerical Analysis and Linear Algebra
Dependability Analysis Tools and Tool Development
Reliability Statistics and Life Data Analysis
Data Analytics and Statistics
Business Intelligence Toolsets
Structural Engineering and Analysis
Finite Element Analysis and Computational Mechanics
Web and Data Base Technologies
Fault Analysis
Petri Nets
Discrete Event Simulation
Earned Value Management
Engineering Management
Avionics
Aerospace
Space Systems
Systems Engineering
Stochastic Modeling
Configuration Management
System Design
Requirements Management
Engineering
Spacecraft
Interests:
Applied Mechanics and Finite Elements
Web and Data Management Technologies
Airplane Certification Analysis
Aerospace Recommended Practices
Reliability Engineering
Statistics and Data Analytics
Stochastic Models
Software Engineering and Architectures
Statistical Models
Reliability
Structural Engineering and Analysis

Publications

Us Patents

Reliability Estimation Methods For Large Networked Systems

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US Patent:
8121042, Feb 21, 2012
Filed:
Jun 29, 2009
Appl. No.:
12/493665
Inventors:
Dazhi Wang - San Jose CA, US
Kishor S. Trivedi - Durham NC, US
Tilak C. Sharma - Tacoma WA, US
Anapathur V. Ramesh - Bothell WA, US
David William Twigg - Federal Way WA, US
Le P. Nguyen - Renton WA, US
Yun Liu - Lynnwood WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
H04J 1/16
US Classification:
370248, 370252
Abstract:
A computer-based method for determining a probability that no path exists from a specified starting node to a specified target node within a network of nodes and directional links between pairs of nodes is described. The nodes and directional links form paths of a reliability graph and the method is performed using a computer coupled to a database that includes data relating to the nodes and the directional links The method includes selecting a set of paths, from the set of all paths, between the starting node and the target node that have been determined to be reliable, calculating a reliability of the union of the selected path sets, setting an upper bound for the unreliability of the set of all paths, based on the calculated reliability, selecting a set of minimal cutsets from all such cutsets that lie between the starting node and the target node, calculating the probability of the union of the minimal cutsets, and setting a lower bound for the unreliability of the set of all cutsets.

Method And System For Evaluating Costs Of Various Design And Maintenance Approaches

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US Patent:
8165968, Apr 24, 2012
Filed:
Oct 25, 2004
Appl. No.:
10/972916
Inventors:
Anapathur V. Ramesh - Bothell WA, US
Paul M. Covert - Lynnwood WA, US
Stephen C. Rhodes - Lake Stevens WA, US
Scott C. Hunter - Bothell WA, US
John L. Vian - Renton WA, US
Timothy J. Wilmering - Saint Charles MO, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06Q 99/00
US Classification:
705400, 705 11, 705 712, 705 737, 702184
Abstract:
The method and system quantify the impact of various design and operational solutions for equipment modules of a structure and the overall structure based upon economic factors. In particular, the method and system provide cost evaluation of various maintenance approaches for at least one equipment module that is part of an overall structure. In addition, a baseline and alternate equipment module may be specified for each equipment module. The costs associated with each of the maintenance approaches for each baseline and alternate equipment module then may be compared and the costs associated with the overall structure having a chosen maintenance approach for each baseline and alternate equipment module may be evaluated. The sensitivity of the costs associated with the overall structure to changes in one or more of the parameter values also may be calculated.

Collaborative Web-Based Airplane Level Failure Effects Analysis Tool

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US Patent:
20070294594, Dec 20, 2007
Filed:
May 18, 2006
Appl. No.:
11/436330
Inventors:
Kevin N. King - Mill Creek WA, US
Anapathur V. Ramesh - Bothell WA, US
Larry R. Schultz - Bellevue WA, US
Tilak C. Sharma - Kent WA, US
David W. Twigg - Federal Way WA, US
International Classification:
G06F 11/00
US Classification:
714 46
Abstract:
Embodiments of methods, apparatuses, and articles for receiving system malfunction effects data including at least one malfunction and a plurality of direct and indirect effects associated with each of the at least one malfunction and storing the received system malfunction effects data, are described herein. The embodiments may also facilitate a user in viewing and/or modifying the system malfunction effects data, and the viewing includes presenting the data in a relational fashion, with each malfunction linked to one or more direct effects, and each direct effect linked to one or more indirect effects.

Freighter Aircraft System And Container System

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US Patent:
20210129972, May 6, 2021
Filed:
Nov 1, 2019
Appl. No.:
16/672423
Inventors:
- Chicago IL, US
Sergey D. Barmichev - Kirkland WA, US
Anapathur Ramesh - Bothell WA, US
International Classification:
B64C 1/22
B64C 1/10
B65D 88/14
B65D 88/12
B65D 90/00
Abstract:
A trunk route aircraft has at least one wing for supporting the aircraft during flight, and at least one propulsor for forward propulsion of the aircraft. The trunk route aircraft further includes a pressurized trunk route fuselage having a double-bubble cross-sectional shape and a generally vertically-oriented longitudinal bulkhead dividing the trunk route fuselage interior into two side-by-side trunk route payload compartments. The longitudinal bulkhead is loaded in tension when the trunk route fuselage is pressurized. The trunk route payload compartments are each configured to receive a plurality of lightweight ISO (International Organization for Standardization) geometry containers arranged end-to-end, or a plurality of container inserts arranged end-to-end, each container insert also configured to be received within the lightweight ISO-geometry container, or a combination of one or more lightweight ISO-geometry containers and one or more container inserts arranged end-to-end.
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Anapathur V Ramesh from Bothell, WA, age ~62 Get Report