Berlin, Berlin, Germany
Instrumentation Planning Development of business jet engines -providing work instruction for instrumentation fitters - planning build/instrumentation sequence of development/test vehicles e.g turbo jet engines, power gear boxes or test rigs -interdisciplinary colaboration with instrumentation design, validation, assembly line, project and store management
AÜG Instrumentation Planning for Development engines for business jet engines.
Structures and Transmissions Front Bearing Chamber Design for Business Jet Engine
-latest BR700 engine design support for HPC Blades and Vanes; creation of DDRs -design support for HPC casing design, model checks, model data set checks, drawing data set checks, tolerance stack ups -XWB instrumentation design HPC thermal survey -XWB design support for ICC Flying Test Bed, IDD for heavy instrumentation ICC -latest BR700 engine instrumentation design: HPT ST1 Liner Tip Clearance Solution: DDR and separate solution drawing, drawing creation for HPT ST1 Liner Tip Clearance; HPT ST1 Liner Casting and HPT St1 Liner with Windows and Towers TCC manifold Strain Gauge Survey solution: preparation of DDR and separate solution drawing; TCC manifold thermal and pressure survey solution: preparation of DDR and separate solution drawing; preparation of TCC manifold instr. part drawings. -solution owner of No1 Bearing Arrangement of new small RR engine, -writing the DDR -preparing and updating the Solution Issue Report (parts list) using PDM, -predefining 3d models with hand calculation, -detailed design assessment in corporation with the stress department -presenting the status of the solution in frequently technical reviews with tech leads, subsystem CDE and specialists -checking the compliance of the solution to the requirement documents (e.g. SSRD,SSDD,CRD,EDSS etc.) -determing the fits of mating components taking in to account deflections assessed by the thermal department -providing 3d models, drawings and other important data for the value engineer to assess the should costs for each component -reviewing the design with the manufacturer/supplier and check the feasibility of manufacturing -having meetings with the build team to check build issues planning tooling and ground support equipment availability/new design -Design Failure Mode& Effect Analysis (DFMEA) sessions held to identify risks in case of failure of the components of the solution
- assisting Compressor/ Fan tests - online monitoring of H&S parameters and performance parameters (temperature, pressure, speed) of Rigs during tests via EDAS (Enhanced Data Acquisition System) - Maintenance and calibration of facility measurement equipment. - hook up and signal check of Rig instrumentation and facility measurement equipment prior to test - running up and running down the measurement system EDAS - analysis of performance parameters in terms of feasibility - writing test reports - specialist of mass flow measurement and temperature measurement -writing Specifications (Specs) for the acquirement of new temperature measurement system - writing calibration procedures - supported Rig Tests : XWB build1-2 (RR), Rig 648 Blade tip modification back to back test (RR), AC100 build 1-3 (Siemens), GTRE build 1-3 (GTRE Gas Turbine Research Establishment india), GT26 (Alstom), Open Air, OPAL (RR), VITAL (RR) etc.
-designing and drafting AC100 (Siemens) compressor rotor and assisting manufacturing of the rotor components (no blading) -in addition assisting the design of interfacing assemblies such as front bearing housing, rear bearing housing and casings module - working closely with the analysis department to iterate the final rotor design - design of tooling for both assembly and balancing the rotor module - defining the fiiting instruction - defining the balancing scheme - definition of the balancing planes - assisting rotor instrumentation design
-modeling and drafting of the UFFA (Universal Fan Facility for Acoustic) cable tray -designing and drafting components of the facility integration of the MIR (Modular Industrial compressor Rig) (MAN-Turbo)