Präsentation ACAT Services

AneCom AeroTestEngineering and Test Services

for the Gas and Steam Turbine Industry

© AneCom AeroTest 2013 Company Profile Slide 2

Content

� Our Company

� Our Team

� Our Services

� Contact


Development partner for gas and steam turbines

Founded 2002

Employees 140

Located Aerospace Technology Centre „Schönefelder Kreuz“ - Wildau, Germany

„AneCom AeroTest is a highly professional, independent

development service provider for various key players in the

aero engine and gas turbine industry. The prime focus of our

operation is to satisfy our customers needs.“

Dr. Edmund Ahlers

Managing Director

Certified to EN 9100 and EN 14001


Our Teams

Engineering

Teams



From single service to turnkey projects



Test Vehicles and Prototype Machines

� Concept & Design

� Instrumentation, Build & Commissioning

Measurement Solutions

� Validation Strategy & Selection of Technology

� Implementation & Field Support

Component and Instrumentation Design & Analyse

� Design to Cost

� Dedicated Customer Teams

Testing of Compressors , Combustion & Turbine systems

� In-house Compressor Test Operation

� Off-site Combustor Test Operation


Our Services









� Design to Cost






Our Services


…from the Aeroline … …to the Test Vehicle

Measurement technique

Design (Test Vehicle HW & Instrumentation)

Analysis (Stress, Thermal, CFD, Vibration)

PDM/BOM (part handling & parts list)

Design Review @ Engineering Board

Make & Rework of Hardware

Instrumentation Application

Build & Installation

Mission Support

Test Vehicles and Prototype Machines – full service


SIEMENS Mülheim – AC-100 HPC Rig

AC-100 HPC Rig for SIEMENS Mülheim – SGT5-8000 compressor last stages

© Siemens 2012


Test Vehicles and Prototype Machines – Design & Analysis

Engineering Team

� ~ 60 Designer & Analysis Engineers

SW Tools

� Unigraphics - UG, CADDS 5, ProE

� Ansys, SC03, Nastran

� Siemens Multiside Conection

Capabilities

� Rig Design & Analysis

� Instrumentation Design

� Engine Hardware Definition & Analysis

� Build Tooling Design


Test Vehicles and Prototype Machines – Manufacturing & Supply Chain

© Siemens 2012

• Dedicated Team

• VI Capability

• Outstanding Prototype HW Manufacturing pool

• Interlinked with Design


Test Vehicles and Prototype Machines – Instrumentation Application

Instrumentation application and build area under “one

roof”, integrated work planning (Instrumentation & Build)

allows short turnaround times without external gates


• Highly qualified & experienced staff

• > 1000 m² build shop

• 4-off separated customer bays

• Appropriate tooling and crane capacity

• 1500 m² storage capacity

Test Vehicles and Prototype Machines – Build & Commissioning


Test Vehicles and Prototype Machines – Compressor Test Vehicle

© Siemens 2012

© RR Plc 2012

© AneCom Aerotest 2012

© MAN 2012


– possible range of service

Organisation & Design :

– test bed selection & booking

– design, manufacturing and procurement of rig & test parts

– rig build and test bed installation

– coordination of test activities with the partner organisation

Test execution:

– test execution in cooperation with the partner organisation

– data acquisition and validation

– test bed changes

Post processing:

– removal from the test bed

– test vehicle strip and inspection

– project documentation

Test Vehicles and Prototype Machines - Combustor Test Vehicle


Test Vehicles and Prototype Machines - Combustor Test Vehicle References

Our contribution

Design of:

− Inlet− Baffle Plates− Burner Modules− Fuel Spray Nozzle− Heat Shields

Analysis of:

− Rakes (Gas Sampler)− mechanical parts of combustor moduls









� Design to Cost






Our Services


Measurement Solutions – Validation Strategy & Selection of Technology

Specification, Configuration & Installation of Measurement Systems

• Procurement of hardware or systems

• Calibration

• Commissioning

Data validation and Analysis

• Processing & Visualization

• Frequency Analysis

• Correlations

• Presentation & Reporting


300 m² state of the art instrumentation laboratory,

24 Instrumentation Fitter & Specialists

Visual inspection area, photo documentation microscope, borescope inspections

Measurement Solutions – Implementation & Field support

- Design & laboratory

closely linked

- Proven ACAT standards

- Lessons learned

closeout after each

project









� Design to Cost






Our Services


Component and Instrumentation Design – Component Analysis

Capabilities

• Stress and thermal analysis, steady state and transient

• Resonance frequency, harmonic analysis

and modal shape determination

• Optimised strain gauge positioning

• Bolted flange assessment

• Rotor dynamic analysis

Analysis Tools

Ansys, SC03, Nastran/ Patran


Orbitplott –Eigenformen: Rotor,

Casing, Fan

Component and Instrumentation Design – Rotor Dynamic Analysis


• Live & Integrity assessment on rotating components


• Live & Integrity assessment on

rotating components

Component and Instrumentation Design – Rotatives Analysis


Component and Instrumentation Design – Component Design

© MAN 2012

e.g.:

• Management of sub system D&M supplier on behalf of the customer

• Design assessment of concessions and manufacturing errors

• Cost Reduction Design Support, using VI & DfX

• Customer integrated Teams with component responsibility



© MAN 2012

e.g.:








© MAN 2012

e.g.:








© MAN 2012

e.g.:








© MAN 2012

e.g.:







Engine Combustor Design & Analysis

Our contribution

Component and Instrumentation Design – Component Design References

Design of:

- Heat shields- Combustion Liner

Design and Analysis of:

- Pressure Casings

Modification of Combustor for Instrumentation


Component and Instrumentation Design – Probes Design & Adaptation

More than 5 Engine development programs supported

Tip-Clearance/ -Timing


Component and Instrumentation Design – Probes Design & Adaptation

0

1000

2000

3000

4000

5000

6000

7000

0 1000 2000 3000 4000 5000 6000 7000 8000

Speed (RPM)

Freq

uen

cy (

Hz)

1F axial

2F axial

1F tang

2F tangential

3F tangential

1T

48EO, 2BPF

2EO

24EO, 1BPF

1EO

Frequency range of possible

Karman instabilities

Design, Analysis & definition of H&S strain gauges


Telemetry

Speed

Component and Instrumentation Design – Telemetry Adaptation









� Design to Cost






Our Services


2 Compressor Test Facilities

for aero-performance testing

� drive power 18MW (24000 hp)

� air flow up to 200 kg/s

� split flow capability for fan testing

� min. inlet pressure 20 kPa (0,2 bar)

� exhaust temperature up to 650 °C

Testing of Compressors - C T C Wildau


Fan Noise Test Facility

for aero-performance testing and noise investigations

under free-field conditions

• drive power 18MW (24000 hp)

• air flow up to 200 kg/s

• split flow capability for fan testing

• 1000 m2 anechoic chamber (200 Hz – 40 kHz)

• far field microphone array

Testing of Fan systems - C T C Wildau


Testing of Combustion & Turbine systems

DLR Cologne for combustor testing (HBK2 & 3):

• Full Annular Combustor Test – FANN

• Multi Sector Combustor Test - HPMS + LPMS

• Single Sector Combustor Test – HPSS

ILA Stuttgart for altitude testing:

• Test of complete flight engines under flight

conditions (also core engines and components)

• Two test beds

• Cold flow turbine rig testing

Third party test facilities used by AneCom


41 customers from aviation and industrial gas turbine industry

References - Customer Project History

Quality. Flexibility. Solution Orientation. …… and Satisfied Customers worldwide.


Contact

AneCom AeroTest GmbH

im Zentrum für Luft- und Raumfahrt

Freiheitstrasse 122, 15745 Wildau, Germany

www.anecom.de

Ansprechpartner

Colin Sheehan

Manager Design & Analyse

Telefon +49 (0) 3375 9226 16

Mail: [email protected]


Thank You!

© AneCom AeroTest GmbH. All rights reserved. Confidential and proprietary

document. This document and all information contained herein is the sole

property of AneCom AeroTest GmbH. No intellectual property rights are

granted by the delivery of this document or the disclosure of its content. This

document shall not be reproduced or disclosed to a third party without the

express written consent of AneCom AeroTest GmbH. This

document and its content shall not be used for any purpose other than that for

which it is supplied. The statements made herein do not constitute an

offer. They are based on the mentioned assumptions and are expressed in

good faith. Where the supporting grounds for these statements are not shown,

AneCom AeroTest GmbH will be pleased to explain the basis thereof.


Reference

High Pressure Full Annular Combustor Rig Test Traverse System


The Company

Documents

Präsentation ACAT Services