aat injector nozzle test chamber p15681 calibration fluid exhaust system
TRANSCRIPT
Team IntroductionTeam Members Major Roles
Zach Huston ISE Project Manager
Hayden Cummings ME Customer Relations
Robert Moshier ME Facilitator
Andrew Heuser ME Scribe/Primary Edge Support
Timothy Nichols ME Purchasing
Adam Farnung ME Manufacturing Lead
Agenda• Introductions• Background• Problem Definition • MSDS• Use Scenerios • Benchmark Parameters • Project Deliverables • Constraints and Challenges
• Stakeholders • Communication Plan• Customer Requirements • Engineering Requirements • House of Quality• Project Schedule • Risk Assessment• Going Forward
Background - AAT
Advanced Atomization Technologies (AAT)• Joint venture between General Electric Aviation and
Parker Aerospace• Formed in 2012• Specializes in manufacturing and testing fuel nozzles for
gas turbine engines
Background - Project
Fuel Injection Nozzle Testing System• Qualifying fuel injection nozzles• Specialized calibration equipment• Expensive, odorous calibration fluidProblems with system• Offensive odor permeates entire building• Loss of expensive calibration fluid
Problem Definition• All commercial aircraft nozzles must undergo a flow test to
assure that requirements are met for spray angle.• This test uses Stoddart Solvent (MIL-PRF-7024F Type II)• Petroleum derived, clear, transparent liquid.• The fluid is very expensive and has an offensive odor• The current exhaust system is ineffective at both containing
containing the odor and recovering the atomized fluid for reuse.
MSDS“Inhalation:
Breathing of vapor or mist is possible. Breathing small amounts of
this material during normal handling is not likely to cause harmful effects.
Breathing large amounts may be harmful.”
“Symptoms:
Signs and symptoms of exposure to this material through breathing, swallowing,
and/or passage of the material through the skin may include:, stomach or
intestinal upset (nausea, vomiting, diarrhea), irritation (nose, throat, airways),
central nervous system depression (dizziness, drowsiness, weakness, fatigue,
nausea, headache, unconsciousness) and other central nervous system
effects, and death.”
Additional Scenarios• Angle test - purge atomized fluid, remove
nozzle• Flow test, connection failure - purge atomized
fluid, reconnect nozzle, repeat test• Angle test, connection failure - purge atomized
fluid, reconnect nozzle, repeat test
Benchmark Parameters • Air Quality (PPM)• Overall cycle time (Min)• Setup time for system/nozzle so testing can begin (Min)• Volume of collected fluid (fl. oz)• Function of door lock mechanisms (no opening during
test)• Visibility in chamber during test• Maintain proper spray angles
Project Deliverables• Fully operational system for the GE90 nozzle
• Documentation package for application to additional chambers
Constraints and Challenges
• Cannot impact flow testing
• Flow test materials and test procedures may not change
• Should be able to fully contain the calibration fluid
• Must be adaptable to current test chambers
• Must meet all applicable wire & safety codes and specifications
• Must be within budget (Also, no one item can be >$5,000)
• Must fit within current footprint
• Must not add too much additional process time
Stakeholders• AAT (Jim Kalinski, David DeWispelaere)• GE Aviation• Parker Aerospace• Floor Operator• Financial team• MSD team• Gary Werth
Communication Plan• Contact with AAT is ongoing• Will be contacting them primarily with questions or
concerns• Will be providing updates on project status only as
needed• Points of contact for general project questions as well as
purchasing questions.