GasTurb13PreliminaryDesign复习课程
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For each Component the Input and output is listed in
the corresponding Tab
If you deselect “Show Axis”, by pressing Control you will
be able to move the Drawing with your mouse in
GasTurb 13
PRELIMINARY ENGINE DESIGN
Copyright © GasTurb GmbH
GasTurb 13 Main Window
For this tutorial we will use a Turbojet
and the scope More…
Copyright © GasTurb GmbH
Inlet Design Options (2)
Copyright © GasTurb GmbH
Strut/Chord Height = 0.5 Cone Angle = 10°
Strut/Chord Height = 0.5 Cone Angle = 30°
Number of Struts=0 Cone Angle = 25° Cone Length/Radius = 0.1
- Bézier: use a Bézier curve to define the shape
- Sketch: use a Bézier curve to define the
shape. Additionally you may define blade
geometry for each stage
Adjust min and max value and
click OK
Choose quantity from the list
Burner
Input
annulus geometry
Copyright © GasTurb GmbH
Copyright © GasTurb GmbH
Click on Slider
Interactive Design
See how an input quantity affects the design
Select a quantity
and angles of your design
Copyright © GasTurb GmbH
Inlet Design Options (1)
Input
Output
Copyright © GasTurb GmbH
Strut/Chord Height = 0.5 Strut/Chord Height = 1
and drop way.
Compressor Length
As来自百度文库ect Ratio = 1.5
Aspect Ratio = 2
Copyright © GasTurb GmbH
Compressor Annulus
Here you can get a detailed overview of the compressor
Annulus Shape Descriptor = 1 Annulus Shape Descriptor = 0.5
Annulus Shape Descriptor = 0
Copyright © GasTurb GmbH Inlet Radius Ratio is calculated during cycle design in this example
Compressor Flow Annulus Shape
The compressor annulus shape can also be altered in the control panel. Different
modes are offered:
- Simple: define the shape descriptor
Number of Struts=0 Cone Angle = 35° Cone Length/Radius = 1.3
Compressor Design Options
Input
Output
Copyright © GasTurb GmbH
Compressor Flow Annulus Shape
Copyright © GasTurb GmbH
Copyright © GasTurb GmbH
General Arrangement
Copyright © GasTurb GmbH
General Arrangement
General Arrangement
Select the component you want to design
We Need Some Data
Select the engine model
Open the engine model
Copyright © GasTurb GmbH
Input Data Page
Click on Edit Geometry
There are two more buttons with this scope
a drag and drop way.
By selecting “Show Disk Mass”, the masses will be displayed in the drawing
Copyright © GasTurb GmbH
General Arrangement
If you select “Measure” zooming will be disabled and you can measure distances
Compressor Flow Annulus Shape
By selecting “Show Disk Mass”, the masses will be displayed in the drawing
If you deselect “Show Axis”, by pressing Control you will be able to move the Drawing with your mouse in a drag
the corresponding Tab
If you deselect “Show Axis”, by pressing Control you will
be able to move the Drawing with your mouse in
GasTurb 13
PRELIMINARY ENGINE DESIGN
Copyright © GasTurb GmbH
GasTurb 13 Main Window
For this tutorial we will use a Turbojet
and the scope More…
Copyright © GasTurb GmbH
Inlet Design Options (2)
Copyright © GasTurb GmbH
Strut/Chord Height = 0.5 Cone Angle = 10°
Strut/Chord Height = 0.5 Cone Angle = 30°
Number of Struts=0 Cone Angle = 25° Cone Length/Radius = 0.1
- Bézier: use a Bézier curve to define the shape
- Sketch: use a Bézier curve to define the
shape. Additionally you may define blade
geometry for each stage
Adjust min and max value and
click OK
Choose quantity from the list
Burner
Input
annulus geometry
Copyright © GasTurb GmbH
Copyright © GasTurb GmbH
Click on Slider
Interactive Design
See how an input quantity affects the design
Select a quantity
and angles of your design
Copyright © GasTurb GmbH
Inlet Design Options (1)
Input
Output
Copyright © GasTurb GmbH
Strut/Chord Height = 0.5 Strut/Chord Height = 1
and drop way.
Compressor Length
As来自百度文库ect Ratio = 1.5
Aspect Ratio = 2
Copyright © GasTurb GmbH
Compressor Annulus
Here you can get a detailed overview of the compressor
Annulus Shape Descriptor = 1 Annulus Shape Descriptor = 0.5
Annulus Shape Descriptor = 0
Copyright © GasTurb GmbH Inlet Radius Ratio is calculated during cycle design in this example
Compressor Flow Annulus Shape
The compressor annulus shape can also be altered in the control panel. Different
modes are offered:
- Simple: define the shape descriptor
Number of Struts=0 Cone Angle = 35° Cone Length/Radius = 1.3
Compressor Design Options
Input
Output
Copyright © GasTurb GmbH
Compressor Flow Annulus Shape
Copyright © GasTurb GmbH
Copyright © GasTurb GmbH
General Arrangement
Copyright © GasTurb GmbH
General Arrangement
General Arrangement
Select the component you want to design
We Need Some Data
Select the engine model
Open the engine model
Copyright © GasTurb GmbH
Input Data Page
Click on Edit Geometry
There are two more buttons with this scope
a drag and drop way.
By selecting “Show Disk Mass”, the masses will be displayed in the drawing
Copyright © GasTurb GmbH
General Arrangement
If you select “Measure” zooming will be disabled and you can measure distances
Compressor Flow Annulus Shape
By selecting “Show Disk Mass”, the masses will be displayed in the drawing
If you deselect “Show Axis”, by pressing Control you will be able to move the Drawing with your mouse in a drag