Engineer Design

Anthony B. Clarke

***** ** **** ***** # *, Redmond WA 98052 ?(M)206-***-**** ?(H)425-***-****

? ***********@*****.*** ?

SENIOR DESIGN ENGINEER

Structural Design ? Mechanical Systems Design ? Electro-Mechanical Design

Professional Profile

Innovative Senior Design Engineer with 40 years of international experience

in a wide field of design skills involving military and commercial aircraft

projects. Proficient in Catia, V4, V5, PDM Enovia, Solid Edge/Works,

Autocad and Anvil computer systems,GD&T application. Competent problem

solving and liaison skills.

Areas of Expertise

. Aircraft Primary/Secondary Structure.

. Aircraft Composite Structures

. Hydraulic Systems design and Installation

. Fuel System Design and Installation

. A.P.U. and E.C.S. System Installation

. Flap and Slat Structures

. Engine Bleed and Anti-icing Systems

. Flight Test Installation

. Electronic System Installation

. Furnishings and Interior Trims

. Liaison - Product Support Team

. Iron Bird Mechanical Tests

Professional Experience

BOEING,

everett, WASHINGTON, U.S.A.

October 2010 - Present: Senior Design Engineer. Assigned to Tanker KC46.

Layouts and Design approval presentations for Re-fuel/De-fuel, Vent,Secondary Shut Off, Fuel quantity instantiating system and Dip Sticks.

Layout, Design approval presentation, Installation and Detail of Fuel

Scavenge and Water Scavenge Systems using V5, Enovia and P.D.M.

BEECHCRAFT,

WICHITA, KANSAS U.S.A.

April 2010 - October 2010: Senior Design Engineer. Models of parts for

quotations from vendors to facilitate cost reduction using V5.

BOEING,

RENTON, WASHINGTON, U.S.A.

November 2004 - October 2009: Senior Engineer. Assigned to design of 737-

900ER, Trailing edge and wing installation. In 2006 assigned to 737

liaison, Product support team. Utilizing Catia V4, Catia V5 at the latter

stage.

QINETIQ,

BOSCOMBE DOWN, WILTSHIRE, ENGLAND.

June 2004 - September 2004: Senior Design Engineer. Design and detail of

various mechanical and structural components. Installation of flight test

instrumentation. Using Solid Edge.

GCT ENGINEERING SERVICES,

BROADSTONE, DORSET, ENGLAND.

March 2003 - May 2004: Design Team Lead. Assigned to Airbus A380 A.P.U.

and TTS Fuel system. Task collated at PFW, Speyer, Germany. Went as Team

Leader to collect and co-ordinate all design information for the APU and

titanium fuel system which was taken back to base office for finished

design and detail using Catia V4.

BAe SYSTEMS,

SAMLESBURY, LANCASHIRE, ENGLAND.

November 2002 - March 2003: Senior Design Engineer. Project-Joint Strike

Fighter. Preliminary conceptual design and installation concepts for

frames, firewalls, ribs and primary aft structure. Design layouts using

Catia V4.

GAMESA AERONAUTICS,

VITTORIA, SPAIN.

July 2000 - November 2002: Senior Design Engineer. Assigned to Embraer

170 elevator and rudder, comprising of design and detail of composite

panels, skins, ribs and leading edge along with support structure. Interior

furnishings and fittings for Eurocopter. Using Catia and Autocad.

BAe SYSTEMS,

WARTON, LANCASHIRE, ENGLAND.

December 1999 - July 2000: Senior Design Engineer. Nimrod primary and

secondary structure modifications.

anthony b. clarke Page Two / ***********@*****.***

GKN WESTLAND AEROSPACE,

COWES, I.O.W. ENGLAND.

July 1997 - December 1999: Senior Design Engineer. Project-RJX 700-Design

and detail of deep stall recovery parachute installation involving

conceptual design modifications to accommodate APU support structure and

installation.Nacelle static test (RJX-700). Assigned to Fokker F50 and

Westwind nacelle design build liaison.

I.P.T.N.

BANDUNG, INDONESIA.

August 1991 - July 1997: Senior Design Consultant Lead. Project-N250-

Conceptual design of wing trailing edge, flap track mountings, tracks and

mechanisms. Catia training course attended. Supervision of local labor in a

technology transfer environment. Vendor interface control, production

liaison, anti-icing and engine bleed system.

W.D.S.

WATERLOOVILLE, ENGLAND.

January 1991 - August 1991: Senior Design Engineer. Project-BAC Harrier-

Secondary structure and avionic bracketry, re-routing of hydraulics to

accommodate updated avionics. Using CADAM system.

BAe SYSTEMS,

PRESTWICK, SCOTLAND.

September 1987 - October 1989: Senior Design Engineer. Project-Jetstream

41-Primary structure. Definition of passenger door and surround structure,

design of composite cargo pod. Using the ANVIL system.

ATLAS AIRCRAFT,

JOHANNESBURG, SOUTH AFRICA.

October 1989 - January 1991: Senior Design Engineer. Project-Mirage III-

Primary structure. Definition of nose parameters to accommodate nose bay

cameras and re-routed pitot tube.

McDONNELL DOUGLAS,

TORONTO, CANADA.

April 1987 - September 1989: Senior Design Engineer. Project-MD 11-Primary

structure. Definition and detail of front and rear wing spar, skin

drawings. Using CADAM.

I.A.I.

TEL AVIV, ISRAEL.

November 1982 - April 1987: Design Engineer. Project-Lavi Fighter-Primary

structure. Design of rear fuselage, fuselage doors, longerons, skins and

composite structures. APU and ECS installations. Iron bird mechanical test.

Westwind commercial jet interior furnishings and fittings.

De HAVILLAND,

TORONTO, CANADA.

September 1981 - November 1982: Engineer. Project-Dash 8-Primary

structure. Definition of canopy sills and windshield surround structure.

Main frame nacelle and support structure for flight test aircraft. Interior

furnishings.

CANADAIR,

MONTREAL, CANADA.

January 1981 - September 1981: Design Engineer. Project-Challenger-Primary

structure. Design of frames, stringers and skins for fuselage plug. Design

and detail of composite ground equipment.

BAe SYSTEMS,

BRISTOL, ENGLAND.

January 1978 - January 1981: Design Engineer. Project-Airbus A310-Primary

structure. Definition of wing ribs, skins and attachments. Re-assigned to

VC10 tanker, worked on frame and stringer attachments for fuselage plug,

floor support structure, fuselage fairings and hose retraction guides.

B.I.D.

BATH, ENGLAND.

1975 - December 1977: Project-Concord/Hawker Siddely HS146-Primary

structure. Definition of HS146 wing loft lines, spine fairing, frames and

skin joints. Concord wing joint crack stoppers, shear attachments and bolt

layouts.

CAMEL OF CORNWALL,

BODMIN, ENGLAND.

1969 -1975: Design Engineer. Design of thin walled pressure vessels for

industrial use, hydraulic lifting equipment following a full 5 year

engineering apprenticeship.

Education

Cornwall Technical College

. Higher National Certificate in Mechanical Engineering.(equivalent to BSc

in U.S.A.)

. City and Guilds in Engineering.

. G.C.E. A Levels, G.C.E. O Levels.

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