Difference between revisions of "White Dwarf Combustion Chamber"

From CUSF Wiki
Jump to navigation Jump to search
 
(12 intermediate revisions by the same user not shown)
Line 1: Line 1:
== Overview ==
== Overview ==
The White Dwarf combustion chamber uses a water-cooled jacket, with a graphite nozzle. The cooling channels are cut into an off-the-shelf copper tube using a CNC machine. The outer walls of the cooling jacket are made of stainless steel and are welded together.
The [[White Dwarf]] combustion chamber uses a water-cooled jacket, with a graphite nozzle. The cooling channels are cut into an off-the-shelf copper tube using a CNC machine. The outer walls of the cooling jacket are made of stainless steel and are welded together.
 
[[File:Combustion Chamber Assembly Summary.png|thumb|700x700px|Cutaway of the White Dwarf combustion chamber, with key components labelled. This image is taken from the [[:File:COMBUSTION CHAMBER ASSEMBLY.pdf|overall assembly drawing]].]]
[[File:White dwarf chamber labelled.png|thumb|Cutaway of the White Dwarf combustion chamber CAD (without the injector).]]


=== Resources ===
=== Resources ===
Line 10: Line 9:


=== Engineering Drawings ===
=== Engineering Drawings ===
A. [[:File:COMBUSTION CHAMBER ASSEMBLY.pdf|Overall Assembly]]
1. [[:File:WHITE DWARF CHAMBER.pdf|Copper Chamber]]
2. [[:File:WHITE DWARF NOZZLE.pdf|Nozzle]]
3. [[:File:STEEL OUTER WALL.pdf|Steel Outer Tube]]
4. [[:File:COMBUSTION CHAMBER ASSEMBLY.pdf|Coolant Inlet Closure Ring]]
5. [[:File:WHITE DWARF RET RING.pdf|Retainer Ring]]
8. [[:File:OUTLET RING TO GEOMIQ.pdf|Outlet Ring]]
9. [[:File:INJECTOR ENDCAP WITH SLOT.pdf|Injector Face / Test Stand Mount]]
== Water Pump ==
The engine uses an electric water pump to feed the cooling jacket, on a closed loop system. The water that leaves the cooling jacket returns to a main reservoir, where it is recycled so that the cooling jacket can operate indefinitely. This is useful for cooling the combustion chamber, and especially the nozzle, after engine shutdown, since the nozzle may act as a large heatsink. Post-shutdown, it may be possible for the nozzle to transfer sufficient heat to the metal components to damage them, if they were left uncooled.


* [[:File:WHITE DWARF CHAMBER.pdf|Copper Chamber]]
The pump used is a Pentax CR 75, 230 V single-phase electric pump, which provides just under 1 kg/s of water flow rate (measured experimentally).
* [[:File:WHITE DWARF NOZZLE.pdf|Nozzle]]
* [[:File:WHITE DWARF RET RING.pdf|Retainer Ring]]


==Copper Chamber==
==Copper Chamber==
Line 19: Line 34:
*
*


Made of copper due to it's high thermal conductivity, which significantly reduces the thermal stress across the walls as well as the wall temperatures. If steel was used, the thermal stresses would be much higher (and would outweigh the gain received from steel's higher yield stress).
Made of copper due to it's high thermal conductivity, which significantly reduces the thermal stress across the walls as well as the wall temperatures. If steel was used, the thermal stresses would be much higher, and would outweigh the gain received from steel's higher yield stress.


Temperature and pressure drop predictions were generated using Bamboo, and the results are available on the [https://github.com/cuspaceflight/White-Dwarf-Cooling simulations GitHub page].
Temperature and pressure drop predictions were generated using Bamboo, and the results are available on the [https://github.com/cuspaceflight/White-Dwarf-Cooling simulations GitHub page].
Line 25: Line 40:


== Nozzle==
== Nozzle==
The nozzle is made of graphite, and is intended to be manufactured by [http://en.tokaicarbon.eu/ Tokai Carbon Europe]. It contains 16 holes that will contain M5 x '3D' [https://www.stanleyengineeredfastening.com/brands/optia/heli-coil helicoil] inserts, allowing the nozzle to be pulled into the retaining ring, whilst simultaneously compressing the graphite gasket in between the nozzle and retainer ring. Graphite thread failure calculations are available on the [https://github.com/cuspaceflight/White-Dwarf-Cooling simulations GitHub page].
The nozzle is made of graphite, and was manufactured by [http://en.tokaicarbon.eu/ Tokai Carbon Europe]. It contains 16 holes that will contain M5 x '3D' [https://www.stanleyengineeredfastening.com/brands/optia/heli-coil helicoil] inserts, allowing the nozzle to be pulled into the retaining ring, whilst simultaneously compressing the graphite gasket in between the nozzle and retainer ring. This graphite gasket is used to seal the leak path between the nozzle and retainer ring.
 
Graphite thread failure calculations are available on the [https://github.com/cuspaceflight/White-Dwarf-Cooling simulations GitHub page]. Extra 'samples' of the graphite-helicoil threads were ordered, separate from the nozzle, so they could be tested until failure experimentally. This provided useful data to ensure that the threads on the nozzle were not overtightened and damaged when it came to tightening bolts into them.


==Retainer Ring==
==Retainer Ring==


The retainer ring is manufactured from a single large piece of stainless steel billet. It has an inlet for the water coolant, and is intended to be brazed to the copper jacket, and welded to the rest of the steel components.
The retainer ring is manufactured from a single large piece of stainless steel billet. It has an inlet for the water coolant, and is brazed to the copper jacket, and welded to the rest of the steel components.  
 
===Notes===
 
*The design needs to be updated to include some radial leeway in the bolt holes, so that the bolts can move outwards/inwards if the graphite and steel expand at different rates.
*Increased back wall thickness from 5 mm to 6 mm, so the Dyson can make the nozzle-side wall flat with a lathe if it warps after brazing.


==Distribution Ring Front==
Triangular gusset plates were added between the retainer ring and the steel outer tube, after an FEA analysis revealed a stress concentration at original (circumferential) weld point between the two. The gussets are intended to increase the weld length and reduce the risk of failure, which would arise from the combustion chamber pressure pushing the nozzle against the retainer ring.
The flat ring that encloses the inlet distribution ring is intended to be a water-jet cut piece of stainless steel. It will be welded to the steel tube and the retainer ring.


==Steel Tube==
==Steel Outer Tube==
The steel tube that encloses the copper fins will slide over the copper, and is not connected to the copper directly. It is intended to be a custom-made welded stainless steel tube, manufactured in the Dyson centre.
The steel tube that encloses the copper fins will slide over the copper, and is not connected to the copper directly. It is intended to be a custom-made welded stainless steel tube, manufactured in the Dyson centre.


== Water Pump ==
==Outlet Ring==
The engine uses an electric water pump to feed the cooling jacket, on a closed loop system. The water that leaves the cooling jacket returns to a main reservoir, where it is recycled so that the cooling jacket can operate indefinitely.
The coolant outlet ring increases the water flow area from the channels to the circumferential path it that must be taken to reach the outlet pipe. This increased flow area reduces the flow velocity, thus reduces pressure losses in the coolant outlet ring.
 
==Injector Connection==
Not yet designed. The injector-end flange is designed to connect to both the injector and the test stand.
 
===Notes ===


*The outlet distribution ring needs to have a larger flow cross section, as right now it is very narrow, which causes very large pressure drops as the coolant tries to leave it. This would also cause uneven velocity distributions in the coolant channel, as the pressure would vary significantly around the outlet distribution ring.
The outlet ring also contains 19 x M4 through-holes, to enable the injector face to be pulled against the outlet ring. A graphite gasket is present between the injector face and outlet ring to prevent combustion gas leaking out of that leak path.

Latest revision as of 00:20, 14 August 2022

Overview

The White Dwarf combustion chamber uses a water-cooled jacket, with a graphite nozzle. The cooling channels are cut into an off-the-shelf copper tube using a CNC machine. The outer walls of the cooling jacket are made of stainless steel and are welded together.

Cutaway of the White Dwarf combustion chamber, with key components labelled. This image is taken from the overall assembly drawing.

Resources

Engineering Drawings

A. Overall Assembly

1. Copper Chamber

2. Nozzle

3. Steel Outer Tube

4. Coolant Inlet Closure Ring

5. Retainer Ring

8. Outlet Ring

9. Injector Face / Test Stand Mount

Water Pump

The engine uses an electric water pump to feed the cooling jacket, on a closed loop system. The water that leaves the cooling jacket returns to a main reservoir, where it is recycled so that the cooling jacket can operate indefinitely. This is useful for cooling the combustion chamber, and especially the nozzle, after engine shutdown, since the nozzle may act as a large heatsink. Post-shutdown, it may be possible for the nozzle to transfer sufficient heat to the metal components to damage them, if they were left uncooled.

The pump used is a Pentax CR 75, 230 V single-phase electric pump, which provides just under 1 kg/s of water flow rate (measured experimentally).

Copper Chamber

Made of copper due to it's high thermal conductivity, which significantly reduces the thermal stress across the walls as well as the wall temperatures. If steel was used, the thermal stresses would be much higher, and would outweigh the gain received from steel's higher yield stress.

Temperature and pressure drop predictions were generated using Bamboo, and the results are available on the simulations GitHub page.

The final copper combustion chamber, after having the cooling channels machined into it by a CNC machine in the Whittle Laboratory.

Nozzle

The nozzle is made of graphite, and was manufactured by Tokai Carbon Europe. It contains 16 holes that will contain M5 x '3D' helicoil inserts, allowing the nozzle to be pulled into the retaining ring, whilst simultaneously compressing the graphite gasket in between the nozzle and retainer ring. This graphite gasket is used to seal the leak path between the nozzle and retainer ring.

Graphite thread failure calculations are available on the simulations GitHub page. Extra 'samples' of the graphite-helicoil threads were ordered, separate from the nozzle, so they could be tested until failure experimentally. This provided useful data to ensure that the threads on the nozzle were not overtightened and damaged when it came to tightening bolts into them.

Retainer Ring

The retainer ring is manufactured from a single large piece of stainless steel billet. It has an inlet for the water coolant, and is brazed to the copper jacket, and welded to the rest of the steel components.

Triangular gusset plates were added between the retainer ring and the steel outer tube, after an FEA analysis revealed a stress concentration at original (circumferential) weld point between the two. The gussets are intended to increase the weld length and reduce the risk of failure, which would arise from the combustion chamber pressure pushing the nozzle against the retainer ring.

Steel Outer Tube

The steel tube that encloses the copper fins will slide over the copper, and is not connected to the copper directly. It is intended to be a custom-made welded stainless steel tube, manufactured in the Dyson centre.

Outlet Ring

The coolant outlet ring increases the water flow area from the channels to the circumferential path it that must be taken to reach the outlet pipe. This increased flow area reduces the flow velocity, thus reduces pressure losses in the coolant outlet ring.

The outlet ring also contains 19 x M4 through-holes, to enable the injector face to be pulled against the outlet ring. A graphite gasket is present between the injector face and outlet ring to prevent combustion gas leaking out of that leak path.