Calculate swept displacement from bore, stroke, rpm and cylinders.
These optional products are directly related to the pneumatic task you are calculating.
If you buy through these links, PneumaForge may receive a commission at no extra cost to you.As an Amazon Associate, PneumaForge earns from qualifying purchases.
Use the Reciprocating Compressor Displacement Calculator to calculate swept displacement from bore, stroke, rpm and cylinders. The calculator uses Bore diameter, Stroke, Number of cylinders, Speed and Acting mode and reports theoretical displacement.
Read the result in the context of the selected units and pressure basis. For this tool, the primary outputs are theoretical displacement. Change one input at a time when comparing scenarios so the effect of each variable remains clear.
PneumaForge applies this verified method: Swept volume × cycles/time. The functional engine is shared with related tools in the compressor-displacement family, while this page solves the specific intent represented by reciprocating compressor displacement calculator.
Swept volume × cycles/timeReproducible example: start with the calculator's default values (Bore diameter = 100; Stroke = 100; Number of cylinders = 2; Speed = 1000) and calculate the result. Then change the variable most relevant to your application and compare the new theoretical displacement against the baseline.
All flow and power bases must match; ISO 1217/CAGI package data preferred for real compressor comparison.
It is designed to calculate swept displacement from bore, stroke, rpm and cylinders. The reported outputs are theoretical displacement.
The calculator uses Bore diameter, Stroke, Number of cylinders, Speed and Acting mode. Only use values that represent the same operating condition or design case.
The calculation follows: Swept volume × cycles/time. The page also states the assumptions that define where the method is valid.
All flow and power bases must match; ISO 1217/CAGI package data preferred for real compressor comparison.
Yes. PneumaForge converts supported units through canonical engineering units. For compressed-air reference flows and pressure bases, the reference pressure and temperature must also remain consistent.