Michael James Evans Email & Phone Number

Shanghai

mech systems expert

Mje Consulting Hq

Design of four individual Houses with a tolal area no 1500 meters squared. layout of terracing , boundary wallsinstallation of house wiring and water systems

Toulouse, France And Hamburg And Speyer Germany

All conceptual design and detail design in Toulouse and Hamburg divisions. Providing design / manufacturing assistance to PFW team in Bristol at Airbus UK.A member of a team working on Qualification plans and compilation of Verification and Validation (V&V) matrix.Conceptual design of bleed air system test rig ducting from Wing to APU and all users in between employing Ti CP, 3AL-2.5V. and 6AL-4V. Routing, support brackets and flex units (vi-breakers) on Airbus A350 XWB aircraft. This is challenging as system delivery is prior to CDR. Drainage system cargo compartmentsDirect supervision of six member of our team and training and guidance as requiredApproval of all drawings-tolerance stack-ups and geometric tolerancesLiaise and contribute to stress, manufacturing activitiesWeekly presentations to Airbus and RSPScheduling and management of engineering tasksManage risks, weight and costsProvide presentations to both PFW and Airbus upper managementPartly responsible for bid preparation for Comac aircraft

Germany And Spain

SYSTEMS ENGINEEREADS CASAMadrid, Spain Compilation of system description, Master Minimum Minimum Equipmem.List MMEL, Qualification test programme and certification test programme for A400M aircraft.Review and comment on hazard document.CONCEPT DESIGN ENGINEEREADSMunich and Bremen, GermanyResponsible for redesign and support of titanium pneumatic ducting system using catia V5 from partial base line as provided by Bremen EADS on A 400 aircraft. Routing and support of leak detect wire. Routing and support of temperature control system ducting. Responsible for integration of system with stress and manufacturing departments.Supervision of pneumatics team contractorsPresentations on design philosophy and recommendations

Paris, France

Responsible for two door A318 Thrust Reverser Actuation System (PW6000 turbo fan engine). Role includes design improvement/recommendations and coordination between suppliers, maintaining test schedules, Airbus and HH departments. System fault finding on the aircraft. Preparation and presentation of PDR, CDR and other documents. Review and approval of all TRAS system qualification documentation material and also test witnessing.

Cambridge United Kingdom

For Boeing 747 and 777 flight extension tanks, conceptual design installation of fuel system ducting, supports, valve, valves housings, coverplates and sensors. Fuel quantity indicating system probes installation and wiring harness routing and clipping. Participation in teleconferences and presentations to Boeing. Design & detail using catia versions 5.6 & 4.2

Sao Paulo, Brazil

Proposed Installation of: anti-icing system within wing leading edges and routing of bleed air system in gondola using catia version 4.2Compilation of procedures design guide for: - installation of bleed air systems. Provided design assistance to Hamilton standard with critique and recommendations of bleed and anti-icing system for ERJ 170/190 aircraft.

Montreal, Canada

Responsible for conceptual bleed air installation design routing and structural support requirements of Wing Anti Ice and Environmental Control System ducting excluding APU and Engine Bay. A tension system designed with cres 321/347 and Titanium 6AL-4V operating at temperature up to 993ºF. Installation of ECS pack and heat exchanger, exhaust and distribution ducting to pressure bulkhead on twin engine continental business jet BD100, using Catia v 4.2. Preparation of: Specification - motion compensators, insulation and system testing in accordance with JAR/FAR 25 and RTCA/DO-160D.Regular presentations including Preliminary Design Review.Supervision of two catia designers.Co-ordination and definition of stress analysis (MSC Nastran) with stress engineer.

Wessling, Germany

For Dornier 328-300 (33 seat Turbofan): Preparation of FAR/JAR 25 Certification Documentation, System Description, Safety Analysis, Hazard Assessment, Ground and flight Testing on the following systems: Airfoil De-Icing, Windshield Ice & Rain Protection, Ice Detection & Wing Inspection Light.Identification and Introduction of system architectural modifications: additional Overtemp Switch revised Isolation Valve specification for Airfoil De-Icing System due to catastrophic event.For Dornier 328-100 (33 seat Turboprop) system improvement - ballooning detection enhanced and increased service life with metering orifice.

Bandung, Indonesia

Conceptual Bleed Air Installation Layout, using catia ver 3.2.Design & Detail for both IAe N-250 prototype and production aircraft (50 and 70 seat twin-turbo prop).Prototype Aircraft: Sub Systems ATA sect 48, 46, 44 & 11 (nacelle, wing, fuselage & tail). A tension system employing Cress 321, Com pure and 6AL-4V Titanium ducting.Production Aircraft: Sub systems ATA sect 60, 48, 46, 44 & 11 (nacelle, wing, fuselage & tail). Both a tension & compression duct system employing titanium Com pure, alloy & Inconel 625, Duct operating Temperatures up to 750ºF.Air Gap Insulation design & detail, comprising of two ply fibreglass shells lined with Al Alloy foil & bonded compressed Silica fibre spacers plus Silicone rubber boots. Precooler Installation Design plus associated inlet & outlet ducting.Assorted design review presentations including P.D.R & support of C.D.R.A member of a task force team responsible for weight saving and system improvements reporting directly to VP engineering. Exchange of technology & training of personnel.

Toronto, Canada

Seconded to Menasco Aerospace, where I provided assistance on design & detail of main landing gear Brake Harness, Electrical Harness, Torque Links and details for FOKKER 100 Aircraft

Prestwick, United Kingdom

Engaged on installation layout, design & detail of: Pitot / Static System, Oxygen System, pipe routing, charging panels, outlets, bottle mounting and supports. Mounting of E.C.S packs, water separators & associated ducting in fuselage pod.Conceptual design of aft end engine nacelle and structure for Garret test including definition of all surfaces. All work carried out on Bae JETSTREAM 41 Aircraft using anvil 4000

Belfast. United Kingdom

Responsible for installation of customer modifications, general alterations & weight saving redesign of assorted components used in the following systems:- Oxygen, Air Distribution, Bleed Air & Hydraulic. Work carried out utilising Computervision CADDS 4x on the Embraer EMB 312 Tucano (2 seat prop trainer). Also Engaged on the installation design of Wing Tip Camera for observation of munitions deployment. Yaw & Incidence boom, assorted recorders, temperature sensors, air data units, relays and circuit panels on the TUCANO (2 seat prop trainer).

Naples, Italy

ATR72, ATR 42 and G222 Aircraft- Responsible for System Installation design of: Bleed Air, Leak Detect, Fire / Smoke Detect systems. Conceptual Fuel System from gondola to upper fuselage penetration, Main Air Distribution in floor & sidewalls, De-Icing system in tail. Various conceptual layouts for APU installations in Fuselage / wing fillet radius, tail section & tail cone.

Molly Millars La, Wokingham, Berkshire, Uk

Design of refrigerated galley unit for AIRBUS 310-300 and Boeing 747-200.

5 Years Eitb Technician Apprenticeship Mechanical Engineering, Mechanical Engineering

Activities and Societies: Design, NC programming, planning, jig and tool design, test and development.

Full Technical Certificate Mechanical Engineering, Mechanical Engineering

Bsc Mechanical Eng, Mechanical Engineering

2 Years completed of BSc Mechanical Eng.

Higher National Certificate, Engineering

Plus 3 supplementary subjects Mechanical Engineering completed 2 years BSC mechanical engineering at South Bank Polytechnic - not.