PIYUSH KANT SINGHMobile: 08197074284 Work: 080-25087131 E-Mail: piyushkantmech@gmail.com

Seeking Aerospace Reliability Engineer assignments with an organisation of repute

Aerospace Reliability & System Safety experience associated with Aeronautical Development Agency (ADA) as Engineer in Quality Assurance & System Effectiveness Group.

Excellent abilities in analyzing complex problems to develop corrective action alternatives; skills in preparing comprehensive, clear and concise reports.

Growth Path

Jun’ 2010-Jul’2010: Industrial trainee Gas Turbine Research Establishment (DRDO), Bangalore

Jan' 2013- Oct’ 2013: Trainee engineer for Bharat Electronics, Bangalore

Oct' 2013- Till Date: Reliability & System Safety Engineer in Aeronautical Development Agency

Functional Hazards Analysis (FHA) as part of System Safety Analysis for MK-II Light Combat Aircraft (LCA).

Reliability Allocation of Hydraulics System for LCA MK-II Fighter Aircraft.

Analyzed system level Failure Modes, Effects & Criticality analysis (FMECA) for hydraulics

system of Light Combat Aircraft (LCA).

Carried out FMEA of BASOV (Bleed Air Shut Off Valve) of Environmental Control System

(ECS) of Naval Variant of LCA for ski- jump from SBTF (Shore-Based Take-Off Facility).

Constructed Reliability Block Diagram (RBD) and Prediction for aircraft Hydraulics

(HYD) System.

Carried out Reliability Prediction for important Line replaceable units (LRU) like non

return valve, quick disconnect coupling, filters, hydraulic release valve, feed line filter

assembly etc of Light Combat Aircraft (LCA).

Sound knowledge of Propulsion And Fuel System (PFS)

Carried out the Fault Tree Analysis (FTA) for Brake Parachute System (BPS) for MK-II.

Zonal Safety Analysis (ZSA) for all LRUs of Prototype Variant of LCA.

Qualification and Acceptance testing of the LRU

working knowledge of Life data analysis, FRACAS

Understood Basics of fighter aircraft gas turbine engine

engine testing at GTRE

CAREER PRÉCIS

CAREER CONTOUR

RELIABILITY ENGINEERING PROFICIENCY

PROFICIENCY IN FOLLOWING TOOLS

INDUSTRIAL TRAINING

Reliasoft BlockSim 6.5, Item Toolkit 8.0, Relex 6.2, Weibull++.

I. Project : Functional Hazards Analysis (FHA) of : LCA MK-II Aircraft

Project Summary: As a part of System Safety Analysis, FHA for has been carried out using Mil-STD-882D. Various hazards were identified and their respective Severity levels and Probability of occurrence was recognized. Further, mishap/Hazard Risk Index (HRI) with suitable acceptance criteria was established.

II. Project : LRU Level Reliability Allocation of hydraulic system for MK II Fighter Aircraft.Tool Used: Microsoft Excel Project Summary: Reliability apportionment is a technique used to allocate the LRU level reliability requirement in order to meet the system level reliability goal using KARMIOL METHOD. In this method, subsystem allocation reliability is computed as a function of numerical factors of system complexity, state of the art, duty cycle, and environmental conditions.

III. Project: Reliability Prediction of LRU level

Tool Used: Relex, Mechrel Project Summary: The LRU Level reliability is predicted using Parts Stress method. It includes LRUs of different systems mainly PFS and HYD.

IV. Project: Reliability Prediction of Hydraulics system

Tool Used: Relex, Mechrel Project Summary: The system level Reliability is predicted for Mission and Safe Return is carried out with the help of BlockSim tool and using Mil-Std-756B. The Reliability analysis enables to identify the measures required to enhance the performance Reliability of the system.

V. Failure Mode Effect Analysis (FMECA) Hydraulic System (MK-I & MK-II)

Project Summary: FMECA is performed to identify basic faults at component level and determine their effects at system level and finally on aircraft level. By tracing the effects of an individual item, failures up to the system level are analyzed and thus how this failure affects the overall aircraft level performance. Failure mode effect analysis is aimed at evaluating adequacy of warnings/other safety provisions available for detection by pilot and ground crew in the event of failure within the guidelines of MIL-STD-1629A.

VI. Project : Risk Assessment For LCA MK-I Tools Used: Item Toolkit 8.0

Project Summary: The safety analysis for LCA MK-I aircraft system involves consideration of many complex situations taken from aircraft level FHA. The various complex situations arising out of the non-availability of essential functions and also due to inadvertent triggering of undesirable events are meticulously identified. A probability of loss of function for all the identified complex situations had been estimated using Fault Tree Analysis (FTA). From the estimated probability and the assessed severity of the hazard of these complex situations, Hazard Risk Index Number has been derived as per the MIL-STD-882D guidelines. Based on the risk index number, the decision criterion is arrived.

VII. Project: Life Cycle Management of SDR (Software Defined Radio)

MAJOR ASSIGNMENTS HANDLED

Tools Used: NPRD-95, Pro-E, CATIA-V5, AutoCAD 2-DProject summary: Responsible for quality, reliability & safety of Audio Adaptor Unit (AAU) and 50W Power Amplifier during product Life Cycle management for LRUs. Modeling and drafting of LRUs of SDR. Conducted Qualification testing viz. vibration, shock, thermal, gun fire, salt fog, bench handling, bump & acceleration.

B.TECH in Mechanical Engineering (2007- 2011)Noida Institute of Engg & Tech. Greater noida (Affiliated to UPTU, Lucknow)

Date of Birth: 16th August 1989 Marital Status: Unmarried

Passport No.: L8178788

REFERENCE

Shri DKP Sinha Shri N. RamalingaiahTD, QA&SEG Scientist/Engineer 'F' Aeronautical Development Agency Aeronautical Development Agency Bangalore - 560017 Bangalore - 560017 Work No: 08025087133 Work No: 08025087174

DECLARATIONI hereby declare that all the statements made above are true to the best of my knowledge and belief.

Piyush Kant Singh

PERSONAL DOSSIER

EDUCATIONAL DETAILS