Skip to main content
← Back to jobs
Apply on site Advanced Technologies Aerospace Engineering

Helicopter Vibrational Health Monitoring (VHM) Analyst

Bishop GmbH · Europe · Onsite · Contract

Salary: Top money for top people Helicopter Vibrational Health Monitoring (VHM) Analyst

Role overview

About this role

<p>We urgently require a Helicopter Vibrational Health Monitoring (VHM) Analyst, for th efollowing study:</p> <p>The tasks to be carried out in the study shall be as follows:&nbsp;</p> <p>Phase 1 &nbsp; 1. Analyse the proposed strategies for rotor and drive train component incipient failure&nbsp; detection through a survey of the existing literature and using available incident /&nbsp; accident data in order to provide a consolidated view on the main failure modes of&nbsp; rotating parts (transmission and rotor system) and respectively what deviations from&nbsp; normal behaviour occur. A series of reference cases to assess different detection&nbsp; techniques and technologies shall be determined.&nbsp; &nbsp; Perform a survey of detection techniques and sensing technologies from existing&nbsp; literature and through a consultation of key industries and research organisations. As&nbsp; the case may be customer might introduce the contractor to the concerned research&nbsp; consortiums.&nbsp; &nbsp; 2. Based on the results of task 1, assess the main techniques and related technologies&nbsp;identified against the reference cases for transmission / rotor system faults. &nbsp;&nbsp; &nbsp; The assessment shall encompass the quantitative determination of performance&nbsp; figures for each detection technique proposed while quantitatively analyse their&nbsp; respective limitations. The risk of false alert shall also be considered.&nbsp; &nbsp; The environment of a helicopter main gearbox (MGB) in terms of space and weight&nbsp; constraints, temperature, lubrication, etc. shall be taken into account to assess the&nbsp; integration of proposed new fault detection techniques. A comparison with current&nbsp; HUMS systems used for large helicopters shall also be developed.&nbsp; &nbsp; The conclusion of Phase 1 shall be a list of the new detection methods and sensing&nbsp; technologies assessed and a synopsis of each one indicating whether there is possibility that&nbsp;they could provide a reliable and practical method for improved advance warning of rotor or&nbsp;drive system component failures. &nbsp; &nbsp; This will be reviewed with the customer in order to determine the detection methods&nbsp; and/or sensing technologies for the tests to be performed during Phase 2. Customer&nbsp; reserves the right to at its full discretion end the contract at the end of Phase 1.&nbsp; &nbsp; Should the customer following its analysis of the second interim report at the end of&nbsp; Phase 1, decide to let the Contractor continue the execution of the tasks foreseen&nbsp; by the contract in Phase 2 it shall instruct the Contractor to that effect in writing. &nbsp; Phase 2&nbsp; &nbsp; 3. For the new detection methods and sensing technologies selected for Phase 2, prepare&nbsp;the test plan and test fixtures to demonstrate the basic functioning of each technique&nbsp;on a transmission / rotor mock-up(s). &nbsp; The test cases to perform shall include a seeded fault test and a bearing fault test in a&nbsp; MGB. For comparison a typical set of HUMS accelerometers shall also be installed on &nbsp;the test fixture. A test plan shall be submitted to EASA for review prior to the&nbsp; performance of tests. &nbsp; 4. Perform the agreed test cases and analyse the results with respect to the objective of &nbsp;improving the detection of incipient failure and comparing to existing HUMS.&nbsp; &nbsp; 5. Identify the main lessons learnt during the tests and the conclusions regarding the&nbsp; different drive train components for which effective incipient failure detection can be&nbsp; provided. &nbsp;The recommendations to support the further development and introduction of new HUMS&nbsp;techniques shall be identified. Any recommendations shall be justified and shall address&nbsp;practical steps to be taken. &nbsp;The &nbsp;final report shall provide a complete view on the tasks performed, clearly identifying&nbsp;the main results obtained and the remaining open issues. Recommendations for complete&nbsp;assessment of new HUMS techniques as well as the status of the on-going research activities&nbsp;shall be provided in this report.&nbsp; &nbsp; &nbsp;</p>

Hiring organisation

Bishop GmbH

<p>Bishop GmbH was founded by Mr Bishop in 1997 for the general advancement of aeronautical art, science and engineering and more particularly for promoting that species of knowledge which distinguishes the profession of aeronautics. Mr Bishop has 25+ years experience (21 stress at Airbus) and also regular flies as PIC. The company is based in Hamburg-Blankenese on the river Elbe opposite the Airbus Germany factory. Together with other complementary partners, BISHOP jointed founded SYNITED GmbH in May 2004, which is listed as a Airbus Strategic Transnational Supplier. BISHOP excels mainly in the areas of stress analysis, systems, fatigue &amp; DT, composites and engineering tool code writing. Together with its partners, BISHOP has a combined force of circa 1000 engineers throughout Europe. BISHOP is corporate members of the RAeS and DGLR. BISHOP is engaged in international research, and collaborative programs.</p> <p>Please visit our website for further jobs;</p> <p><a href="https://www.bishop-gmbh.com/jobcenter/" rel="no-follow">https://www.bishop-gmbh.com/jobcenter/</a></p>

View employer profile →