Bearbeiten von „Scitek Instrumentation Test Engines“

== Introduction ==
SCITEK Consultants Ltd is aiming to provide a facility to include a number of engines, that are independent of OEMs. The use of new and innovative instrumentation has not greatly increased in gas turbine engines partly because the operating environment is harsh and also due to difficulty in convincing engine manufacturers to try out new sensors on their engines. Engine manufacturers want to buy new technologies in a fully developed state. However, this requires many cycles of testing on GTs leading to a catch 22 situation and in effect stifles innovation. The proposed facility aims to solve this issue. 

== Engines which can be included in the facility ==
* Turbo jet, 
* helicopter and 
* APU Gas Turbines .

The aim is to establish a facility with a number of engines to suit different budgets. For example, engines can be used where the running costs are appropriate to suit the customer requirements. 

== Example Images ==
[ALF 502R5] 
[RR-Gnome]
 
== Location ==
Use of small engines to be carried out at SCITEKs in house facilities in Derby. The larger engines will be housed off site (location to be confirmed). 

Who the facility will be offered to
* Sensor manufacturers 
* Engine OEMs 
* Universities that are looking to utilise the engines to validate some of the work they are doing
* Students and Graduates - SCITEK intends to introduce a gas turbine familiarisation course

== Type of modifications to engines ==
The engine can be modified to accommodate sensors from prospective users of this facility. We invite people to offer additional modifications that they feel would be beneficial on the table below. 

{| class="wikitable"  
! style="text-align:left;" | Type of mods to accommodate: !! style="text-align:left;" |Comments:
|-
| Temperature probes  	 || 
|-
| Emission probes	 || 
|-
| Optical probes	 || 
|-
| Pressure probes	 || 
|-
| Tip-timing 	         || 
|-
| Tip-clearance 	 || We envisage higher complexity to fit sensors at turbine end
|-
| Accelerometer 	 || 
|-
| Strain gauges 	 || Will require a telemetry system to be used to monitor rotating parts
|-
| New combustion chamber  || 	
|-
| On pylon signal conditioning 	 || 
|-
| …	 || 
|}

== Probe specifications ==
We hope to create a database of probe holders, so we welcome potential users to forward sensor holder shapes. Provided there are no confidentiality or intellectual property issues, this database can be made available to the EVI-GTI community. 

We aim to accommodate as many types and sizes of sensors as possible however due to possible space restrictions on the engines, each case will be considered individually. We will also offer smaller engines which are more accessible and have lower running costs.  

We also aim to include multiple sensor holders so that comparisons can be made be between different sensor brands. This will also make it possible to facilitate the sharing of running costs if multiple sensor manufacturers test at the same time.

== Type of running to be considered ==
Please add any other running uses that we have not covered. 

{| class="wikitable"
!style="text-align:left;" |Type of running:	!! style="text-align:left;" |Comments:
|-
| Simulation of flight cycles 	 || For cyclic tests of sensors and for emission tests 
|-
| Endurance testing	 || 
|-
| Engine health monitoring 	 || Faults can be inserted on components 
|-
| Tests under different environments 	 || Spray of water based solutions into intake  
|-
| Model validation 	 || For validating mathematical models under realistic operating conditions 
|-
| New engine control algorithms	 || 
|-
| Monitoring engine performance under adverse intake environments 	 || 
|-
| Use by Engine OEMs and others to trial new technologies	 || Suggestions welcome
|-
| …	 || 
|}	

== Indicative Engine Operating Environment ==

{| class="wikitable"
|-
! colspan="3" | Shaft Speeds
|-
!          !! Ground Idle!! Takeoff
|-
| Fan and LPC	 || 1,826 RPM	 || 7,000 RPM
|-
| HP	         || 10,100 RPM	 || 19,500 RPM
|-
| LPT	         || 4,200 RPM	 || 16,100 RPM
|}

{| class="wikitable"
|-
! colspan="2" | Max MGT (Measured Gas Temperature)
|-
| Startup	      || 732°c
|-
| During acceleration || 886°c
|}

== Expected Availability Date ==
January 2021

== Further information
 ==
SCITEK are happy to discuss individual requirements with interested parties. Please contact Marios Christodoulou on marios@scitekconsultants.co.uk. We also welcome any feedback, and would be interested to hear any alternative proposed uses for the facility.

=== About SCITEK Consultants Ltd. ===
SCITEK Consultants Ltd was established in October 1997 in Derby with the purpose to carry out research and development services in aerospace and other industries and its mission has not changed since incorporation. SCITEK has 24 staff and is located in Derby in the UK. SCITEK Consultants Ltd provides R&D services with expertise in fluids, vibration, noise, test and measurement. The design, manufacture, instrumentation and control of research rigs forms the backbone of our activities.