Robert White Email & Phone Number

Guelph, On, Ca

Usa/Canada

aeros.designThis is the Aero Domain Segment of my freelance work. All studies were defined within the framework of 14CFR23/25/27/29 and their international equivalents. My primary goal was to illustrate promising technologies related to Compound Rotorcraft with Reaction Driven Main Rotors. Of particular interest is the possibility of incorporating Fredrik Ljungström's Radial Turbine into the Rotor Hub as a structural member ... thought provoking stuff? ....- Conceptual Study: Design/Analysis (CAD/CFD): UM250A00 Full Composite UAV airframe (250kg MTOW)- Conceptual Study: Design/Analysis (FEA/CFD): HS325 Full Composite Airframe (3250kg MTOW), Reaction Drive Rotor System, Contra-Rotating Profpan (CRP) (SR-7) Propulsion.- Conceptual Study: Design/Analysis (FEA/CFD): HS625 Full Composite Airframe (6250kg MTOW), Reaction Drive Rotor System, Contra-Rotating Profane (CRP) (SR-7) Propulsion.- Conceptual Study: Design/Analysis (FEA/CFD): UWB-35 (70t MTOW) Full composite Ultra Wide Body Airframe, Reaction Drive Rotor System, Contra-Rotating Profpans (CRP).- MRB composite structures representative for a GA (2 seat) aircraft to obtain it's PC (Production Certificate)NOTE:All images/designs in this section are my IP and personal property except where noted.

Canada

terras.designThis segment of my freelance work is devoted to ground based articles/equipment. Specifically vehicles requiring domain conformity to NCAP/EuroNCAP (FMVSS/CMVSS) regulations. I am currently working with a young designer in the Mumbai area, as he appears to have a much better handle on what appeals to the younger generation than myself. His name is Sasank Gopinathan and all of the terras designs originate from him. I just help to ensure the design can be built and is crashworthy.- Conceptual Study: Structural Design/Analysis (FEA) - TFM750-UT 750kg (GVW) ePower Cargo Mini-Truck - NCAP Class- Conceptual Study: Structural Design/Analysis (FEA) - TFM750-LS 750kg (GVW) ePower Micro Car - NCAP Class - Proposal: Design/Analysis (FEA) - 4m Diameter/1500kg (7DOF) Diameter Driving Simulator Dome.Conceptual Study: Design/Analysis (FEA) - 600kg Composite Wheel Rim Assy for a 375t Ultra Class Mining Truck- Conceptual Study: Design/Analysis (FEA) - 3750kg Composite Frame Assy for a 375t Ultra Class Mining Truck- Conceptual Study: Design/Analysis (FEA) - Composite Lift Beams for Telescopic Mobile Cranes (1-50t/50-10m)NOTE:All images/designs in this section are my IP and personal property except where noted

Usa/Canada

aquas.designThis segment is devoted to Defense and waterborne equipment. In general I found myself involved with projects requiring precision close-tolerance (+/-0.005") net moulded parts, that had burned through most of their schedule and budget. Fortunately, the situation brought some nice clarity and provided a singular "go forward" path.- Develop/Qualify/Test: Lamination/Manufacturing Scheme - Acoustic SLS Housings AN/AQS-20 - CFRP/EP- Develop/Qualify/Test: Lamination/Manufacturing Scheme - Sonar Domes- Astroquartz |||/CE- Conceptual Manufacturing Study (CAD/FEA): M61A1 - Inner Drum Helix- Conceptual Study (CAD/FEA): GAU22/A - Composite AHS

Canada

This segment of my freelance work utilizes all of my technical skills and understanding of tailored flexural performance and failure modes of composites. Simulation and subsequent correlation tests are particularly problematic.humanus.design- Conceptual Study (FEA, LS-Dyna): EA Design/Material options for Helmets at 5, 10, 15m/s impact management and concussion control (orthogonal/rotational).NOTE:All images/designs in this section are my IP and personal property except where noted.

Burlington, On, Canada

- Conceptual Design/Analysis (CAD/FEA/CFD): MLG Fairing System - CFRP/EP- Design/Develop/Analyze (CAD/FEA): 6 lengths of >1.25m D (+/-0.15mm) Test Engine Ducts - CFRP/EP- Design/Develop: Rotorcraft Imaging System Mounting Panel - CFRP/EP- Define/Report: VARTM Carbon/Epoxy Materials Equivalency/Characterization Program- Define 15 CRA accepted SRED Technical Reports (Design of Experiments)

Salt Lake City, Ut, Usa

- Conceptual Structural-Thermal Design/Analysis (CAD/FEA/CFD): DARPA TTO Heliplane Reaction Driven Rotor Blade. Significant Flexural Tailoring of the Blade Laminate Scheme was required to optimize harmonics and retain structural integrity of the 300lb blades.- Conceptual Structural-FSI Design/Analysis (CAD/FEA/CFD): fully composite Arrowhawk Airframe.- Conceptual Structural-FSI Design/Analysis (CAD/FEA/CFD): fully composite Shadowhawk Airframe.

Clearwater, Fl, Usa

- Define/Analyze/Qualify (CAD/FEA): NGC/DHS Guardian (CMANPADS) - Aeroshell CFRP/EP - Laminate Scheme for Thermal/AeroLoads, Lightning/PStatic Grounding/Bonding, and EMI Shielding. ( 7 built/ ground/flight tested and STC approved)- Manufacturability Analysis: UAV Ordinance Doors.- Proposal Design/Analysis (CAD) Fully Composite Part25 Crashworthy Seating System - CFRP/EP

Lynn, Ma, Usa

Reported to Munich and Clemens Linden (Rocky Hill)- Program/Technical Liaison between GEAE and MTU for the LPT (including VATN) development to achieve a successful 14month FETT - Define - 22MUSD SOW, OTRD (Overarching Technical Requirements Document).- Defined the Technical/Programmatic Review Criteria iaw the GEAE NPI and Concurrent Design process. - Verification of Phase Entry/Exit Definition/compliance.- Integration of MTU IPPD (Integrated Product/Process Development) to GEAE-Honeywell-TACOM (US Army Command). - Critical Safety/Performance requirements were elicited and contractually parameterized as Quality Engineering/Manufacturing development requirements/constraints.

Wessling, Germany

Reported to G. Dirschl, T. Thiele, and M. Hein.- Redefine (CAD) 328Jet Pylon Geometry for manufacturability & Integrity. - Define (CAD) - Conceptual Geometry, Laminate Schemes, Attachment/Joint fittings for the Carbon Fiber Tail Plane (Horizontal and Vertical Stabilizers)- Define-146M/USD SOW, CDRL (Contract Data Requirements List), CETs (Contract Engineering Tasks), suppler (CASA - F. Fransisco/ M. Hita-Romero) contract negotiations.- Define Systems & Design Engineering Management Planning (DEMP/SEMP/TEMP) and certification MoCs using modified IPPD (DoD 5000.2-R) to JAR/FAR25. - Support update to the DOH (Design Organization Handbook) and QMH (Quality Manufacturing Handbook) to incorporate Level 2 & 3 Design Authority for Suppliers (Subcontract/Risk Sharing Partners).

Hanauer Str. Munich, Germany

R. Mueller (ECD Analysis) recommended me to M.Thiessen and U. Schiefer for this project.- Define (CAD) -Geometry, Laminate Schemes, Tooling, VARTM Process Specifications for a 42M/DM Carbon Fiber Body-In-White Technology Demonstrator: - Define (CAD) Inter/Intrafaces for Front, Sides, Floor, Roof Panels, Bonding Joints, and Hard Points.- Development included Digital PamCrash Simulation, Sub-scale Test Assy, Full-scale demonstration and qualification to Euro-NCAP crashworthiness (Multibody Impact Analysis/Test Demonstration).- Two were built, one was impact tested, the other is in the Zentrum Museum in Munich.

Ottobrunn, Germany

Klaus Brunsch set me to OTN to work for A. Engeleder, C. Zwicker and G. Kuntze-Fechner.- Define (CAD) - Part Geometry, Laminate Schemes, for the Lower Fuselage Shell, Net-Molded & Co-Cured Pax & Crew Door Skins/Frames, HSTAB End Plates/Attach Frames, and Entrance Step.- Define (CAD) Door Transparencies and Blistered Slide (Lofting and E-Exit)- Redefine (CAD) – Part Geometry, Laminate Schemes, and Build Process for the Rotor Blade – Cuff, Flexbeam, Spar for reduced in/out of plane marcelling and Leading Edge Erosion Strip manufacturability.- Define (CAD) - Rotor Control System Kinematics model.NOTE:As of May 2013, 1100 EC135 Airframes are in service. Of the 18 components on each rotorcraft only 11 SDRs and no AD's have been raised against my designed parts.

Richmond , Bc, Canada

- New Product Development and structural repairs for Fixed Wing/Rotor Aircraft, Nacelles, Radomes, Interiors. Develop Product Specifications, Certification MoC (Means of Compliance) and Structural Repair Schemes/Procedures. Composite part development fin support of the Turbine Conversion of the Grumman S-2 Tracker into the Conair TurboFirecat- Define/Report: Prepreg Out-of-Autoclave Carbon-Glass/Epoxy Materials Equivalency/Characterization Program.- Design/Develop/Qualify an Inertial Air Separator for PT6A-67R Turbine Engine (Brazilian Navy)- My business acumen was made abundantly clear to me with the closure of this venture ....

Richmond, Bc, Canada

- Develop Tooling/Manufacturing/Qualification Acceptance Procedures for the DH-8-100 Empennage Leading Edges compliant with DH PPS requirements.- Develop Tooling/Manufacturing/Qualification Acceptance Procedures for the MK41 VLS Tomahawk Frangible End Closures, compliant with NAVSEA WS/MIS requirements.- Qualify NAVSEA sIte through FAI.

Richmond, Bc, Canada

- Setup and operate horizontal and vertical winders producing corrosion resistant fiberglass piping and tanks 6" - 360" Diameter and up to 42ft long (8000kg)- Quality Process Control - Batch promotion of Derakanes, Atlac, and orthophalic resins.- Optimization of wind process using exothermic reaction of inner windings to boost outer windings.

Ce - Continuing Education Course, Structural Airframe Design - M Nui

Ce - Continuing Education Course, Think Composite Design Workshop - S. Tsai

S. Tsai G. Springer L. Hart-Smith K. Bailie J. Patterson Best high intensity course ever!