Level to HN: An initiate source tool to generate Jet Engine compressors

Level to HN: An initiate source tool to generate Jet Engine compressors

the initiate-source turbomachinery trend designer


chat on Discord


donate to Patreon

assets/shaft.png

Axial Shaft

assets/stage_casing.png

Axial Stage Casing

Turbodesigner is a tool that given parameters similar to stress ratio and mass drift rate can generate designs utilizing imply-line accomplish, blade drift prognosis, and on the cease generate a CAD mannequin that would possibly perhaps be exported to STL and STEP files.

For the time being this generates axial compressors and with additional tweaks axial turbopumps for liquid rocket engines

To lead definite of feature traipse or attributable to lack of increase the next assumption are made:

  • Turbomachinery is an axial compressor (will suport more in later variations)
  • FlowStation assumes an Ideal Gas
  • Mean line is continuing and is in line with hub to tip ratio
  • Blade calculations are execrable on the imply (rm) situation
  • Mosey angles are generated with FreeVortex (will enhance more within the long bustle)
  • Blade airfoil is easiest a Double Circular Arc for the time being since other geometries have not been implemented
  • incidence (i) and deviation (delta) values are defaulted 0 (will receive Johnson Map working, but for the time being it’s disabled)

There are plans later to connect the classes that attach calculations
extendable for definite situations

pip install --pre cadquery
pip install -r requirements.txt
pip install jupyter-cadquery==3.4.0 cadquery-massembly==1.0.0rc0 # for viewing in Jupyter

Stunning now there are some items similar to verifying calculations, CFD prognosis, and adding extra common sense for blade prognosis. Observe Projects tab for command asks. Please join the Discord for finishing up communications and collaboration. Please bask in in thoughts donating to the Patreon to enhance future work on this finishing up.

𝚆𝚊𝚝𝚌𝚑 𝙽𝙾𝚆 📺