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WEIGHT CONTROL RESPONSIBILITY, AUTHORITY, and ACCOUNTABILITY (RAA). Presentation at the 67th Annual Conference of the Society of Allied Weight Engineers, Inc. Seattle, Washington 17-21 May, 2008 Kenneth LaSalle 787 Weight Engineering The Boeing Company. Weight Control RAA Agenda. - PowerPoint PPT Presentation
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WEIGHT CONTROL RESPONSIBILITY, WEIGHT CONTROL RESPONSIBILITY, AUTHORITY, and ACCOUNTABILITY (RAA)AUTHORITY, and ACCOUNTABILITY (RAA)
Presentation at the67th Annual Conference
of theSociety of Allied Weight
Engineers, Inc.Seattle, Washington
17-21 May, 2008
Kenneth LaSalle787 Weight EngineeringThe Boeing Company
Weight Control RAAWeight Control RAAAgendaAgenda
Importance of Weight Control
Weight Derivation Ingredients
Roles & Responsibilities
Weight Control Engineering Attribute Overview
Summary
Weight Control RAAWeight Control RAA Q: Why is weight efficiency important to airlines?
A: Weight affects 2/3 of the airplane operating cost
Weight Control RAAWeight Control RAAHow is the airplane weight, at Entry Into Service, derived & improved through design process (structural perspective)?
Weight = f f Configuration + Aerodynamics + Loads + Stress + Design
Weight is the result of the released design. To influence the airplane weight, the weight control engineer must influence the design process.
• Mission req’ts
• 3-View
• Planform
• Integration
• Functionality
• New Technology
• Etc.
• Airfoil Type
• Sweep
• T/c
• Aspect ratio
• Span
• Etc.
• External
• Preliminary
• Design
• MLA
• Internal
• Thermal
• Combined
• Etc.
• Strength
• Fatigue
• Stiffness
• Criteria
• Min Gage
• MS
• Etc.
• Producibility
• Layouts
• Ply maps
• Buy to Fly
• Detailed Part Modeling
• Integration
• Noise
• Design Growth
• Etc.
Product Development
“Design Sensitive” Tools/Parametrics
Firm Concept
Parametrics + LCPT Initial Sizing
Detail Design
Fully Released MBDs / Actual Weights
Weight Control RAAWeight Control RAA
Roles and Responsibilities (or RAA) Ensure the weight efficiency & weight compliance of our company’s
products Provide airplane weight estimates given “any” level of design definition Documented weight estimations w/all assumptions defined Articulate differences between new design concept and existing fleet Proactive design influence (must integrate ourselves into the design community)
Lead airplane weight optimization effort (New, Derivative, or Sustaining) Company leadership’s “primary” resource for weight efficient project planning Provide technology & weight optimization roadmap (Chart the course w/ R&D
Team) Lead weight reduction planning activities (Idea collection thru implementation)
Required Weight Control Engineering Attributes Big Picture / Vision / Strategy Focus Teamwork Technical Competence Personal Attitude / Challenge / Development
Big Picture / Vision / StrategyBig Picture / Vision / Strategy
Commercial Airplane Business Unit (Investment in enhanced performance?) Conditions affecting airlines
High fuel prices? Passenger expectations (more comfort or direct flights)
Company fleet condition (aging or gaps in family?) Launched Programs (competing resources)
787 Family, 777 Freighter, 747-8 A380, A350
Airplane Performance Organization (How Do We Balance Risk?) Engine Performance (SFC) vs. Weight (OEW) vs. Aero Performance
(L/D)
Weight Engineering Organization Communicate frequently to the design team
What is the airplane weight level (understand all assumptions) Where the airplane level is going (forecasting) Why we are pursuing target weight level How we are going to achieve target weight level
Teamwork Teamwork (Establish Trust & Dependability)(Establish Trust & Dependability)
Establish Network Leadership (First-line to program level) Configuration & Engineering Analysis (C&EA) Design Stress Loads Manufacturing Finance Global Supplier(s)
Build Relationships… More than just requesting information
Provide Data On time (meet commitments) Accurate (fidelity required, list & discuss all assumptions)
Team Player Ask trade study team to request missing disciplines’ participation Represent airplane level interests, not just Weight Engineering
Technical CompetenceTechnical CompetenceDetermine Mission Requirement Design ImpactsDetermine Mission Requirement Design Impacts
Range (wing planform & loft size, fuel capacity, low speed devices)
Passenger count (fuselage length & diameter, wing center section width)
Passenger Accommodations (higher humidity, lower cabin alt pressure, large windows)
Speed (wing sweep, airfoil depth, etc.)
Take off & landing performance (i.e. icy runway conditions, field length)
Family plan (weight impacts due to commonality)
Interior architecture (New vs. Derivative vs. Existing Fleet) Interior flexibility impacts Overhead space utilization (Crew rest compartments, OCAS, etc.) Option strategy (what to make basic vs. options)
Cost (NR & Recurring)
Noise - Environmental & Passenger Maintenance and reliability enhancements Aviation authority requirements (FAA or EASA)
Entry into service goal
Technical CompetenceTechnical Competence Understand Schedule & Key Design GatesUnderstand Schedule & Key Design Gates
Product Development Firm Concept Systems Architecture Initial Loads Preliminary Loads Aerodynamic Lines Freeze Firm Configuration Firm Interior Architecture Detail Design Phase Final Loads Flight Testing Entry Into Service (EIS)
Weight Reduction Opportunity
1000’s of pounds
10’s of pounds
Tim
e
Technical CompetenceTechnical CompetenceUnderstand Work Package DefinitionUnderstand Work Package Definition
Structures– Ensure clear understanding of: Part-level definition Primary vs. secondary structure Integration structure (splices, sealant, fastener type & size, etc.) Attachments (composite – bolts in lieu of rivets) Interfaces (systems to structures, eccentricities, etc.)
Systems – Ensure clear understanding of: Systems architecture definition (fuel, high lift, hydraulic, electrical, etc.) Systems separation Bomb blast Engine/APU blade off/rotor burst
Loads (determine which ones are critical, how close is next condition) External (static – 2.5G flaps down, dynamic – gust) Internal (buckling, combined loading, thermal, etc.) Systems (fan blade out, voltage, heat, power, , flow, rpms, psi, etc.)
Materials Allowables (A-basis vs. B-basis, criteria effects, etc.) Density (areal weight, density, etc.) Sizing criteria (choose most efficient material, i.e., for fatigue or strength or
durability) Application (CFRP… ply orientation/optimization, etc.) Cost (Titanium vs. Aluminum)
Technical CompetenceTechnical CompetenceUnderstand Weight, Cost, Schedule RelationshipUnderstand Weight, Cost, Schedule Relationship
Determine significant technical weight drivers Material selection Planform (Wing & Empennage) Body cross-section Airfoil technology High lift systems Load alleviation Architecture Integration Supplier base System’s performance requirements (Temp, flow, power, pressure,
etc.)
Determine large cost drivers (typically compete with large weight drivers)
Advanced materials (procurement cost, manufacturing, etc.) Advanced build technology (new facilities, tooling, etc.) New Technology (high-pressure hydraulics, fiber optics, advanced
magnetics, etc.)
Balance weight vs. performance vs. cost vs. schedule
Ask questions & compare existing fleet data What requirements and objectives guide the design? What advisories are circulating that affect the design? Study or create “Tops Down” charts to compare fleet data
Challenge decisions and criteria Requirements Commonality designs Material selections Production Constraints
Inspectable Preferred materials and standard parts Handling constraints (envelope, weight, robustness) Assembly techniques & tooling
Architectural or layout arrangement Loads, stress and design assumptions (Conservative?)
Provide Feedback Positive & negative Say “thank you”
Technical CompetenceTechnical CompetenceAsk Questions / Challenge DecisionsAsk Questions / Challenge Decisions
Personal Attitude/Challenge/DevelopmentPersonal Attitude/Challenge/Development
Having a positive and optimistic outlook and approach enables: Strong design team working relationships - trust, integrity, ethics More cross-functional participation resulting in accumulation of known and
unknown information Mentoring & friendship opportunities
Developing weight control attributes takes repetition working through new designs
Learning to be inquisitive, while providing appropriate support, is necessary
Communication skills are an essential asset
Implementation of short- and long-term career development plans needs to occur early
SummarySummary
Weight Engineering is a diverse and technical field
Weight control engineering is proactive
Roles and responsibilities change as program progresses through design cycle
Communication, both verbal and written, are key
It takes a lengthy period to become an adept weight control engineer