DLR Portal
Home|Sitemap|Contact Imprint and terms of use Privacy Cookies & Tracking |Deutsch
You are here: Home:Departments:Combustor :Test Facilities and Prototype Design
Advanced Search
News
Institute
Departments
Combustor
Test Facilities and Prototype Design
Experimental Combustor Research
Combustor Simulation
Current Projects
Jobs & Careers
Publications
Combustion Test
Fan and Compressor
Numerical Methods
Engine
Engine Acoustics
Engine Measurement
Turbine
Facilities
Abgeschlossene EU-Projekte
Publications
Offers
Service & Links

Test Facilities and Prototype Design


The department laboratories include several combustor test rigs for combustion  research and industrial investigations. The test rigs are designed to integrate realistic combustor configurations with optical access for visual and laser-based analysis of combustion processes at realistic engine conditions.

The department can rely on long-standing experience in the development and design of new experimental prototypes with optical access for combustion test facilities. Innovative manufacturing techniques are provided by the DLR Sytemhaus Technik and allow reliable test operation for the typical high-temperature and high-pressure range. The department operates a range of test rigs where advanced diagnostics are developed and applied (in cooperation with the Measurement Techniques Department).

OCORE2- Combustion chamber for the laser-based analysis of lean burn applications

Section of an effusion cooled combustion chamber part (SLM)

HBK1

(High Pressure Combustor Test Rig 1)


The HBK1 provides the infrastructure for several single sector and multi sector combustor test sections. The high-pressure combustion test facility allows a detailed investigation of the combustion process with laser-optical measurement techniques under real engine operating conditions.

Read more

SSC

(Single-Sector-Combustor Test Rig)


The SSC is a combustion test rig with optical access to the primary zone on three sides. It is especially suited for the investigation of the burner’s near field with laser-optical measurement techniques.

Read more

OHA

(Optical High Pressure Atomization Test Rig)


The OHA is designed to operate under high pressure, temperature and velocity conditions, approximating the values found in actual gas turbine combustion systems. The Test rig is fully equipped to perform the measurements on sprays and mixing of air and fuel, under non-reactive conditions.

Read more

APZ

(Atmospheric-Primary-Zone Test Rig)


The test rig allows the integration of several test sections for the investigation of spray atomization, cooling and combustion processes under atmospheric pressure.

Read more

HPCR

(High-Pressure-Cooling Test Rig)


Characterisation of cooling efficiency of metal and ceramic combustion chamber wall elements under realistic operating conditions

Read more
Contact
Olaf Diers
German Aerospace Center

Institute of Propulsion Technology
, Combustor
Köln

Tel.: +49 2203 601-2625

Copyright © 2023 German Aerospace Center (DLR). All rights reserved.