The Hong Kong Polytechnic UniversityDepartment of Aeronautical and Aviation Engineering

STORE MASS. STORE ENERGY.

Cabin Pressurisation & Thermal Control

Set the climb, change the supply and open a leak. Trace cabin pressure and temperature as a controller changes the outflow area.

INTERACTIVE CALCULATED DIAGRAMB · LIVE
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A · no saved reference

01 / READ THE CHANGE

Control the outflow

With a prescribed supply, the controller changes outflow area to follow an illustrative cabin-altitude schedule. Relief paths act separately.

02 / READ THE CHANGE

Pressure depends on temperature too

The gas follows pV = mRT. A pressure change can come from stored mass, temperature, or both.

03 / READ THE CHANGE

Close both balances

The cabin stores mass and internal energy. Incoming enthalpy, outgoing enthalpy and wall heat transfer determine its thermal response.

THE SAME MODEL, CONNECTED VIEWS

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B · solid turquoise   A · dashed amber

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QuantityA · savedB · liveB − AUnit

A remains fixed until saved again. Export includes the model version, settings and plotted data.

Equations, assumptions & sources

Read the balance, then connect each symbol to the model. Open a symbol key for definitions and units. Long equations can be scrolled sideways.

01 · Store or release cabin air

dmdt=m˙in−m˙out

Pressure responds to stored mass, not just to the instantaneous inlet flow.

Symbols & units
m
Air mass stored in the fixed cabin volume, kg.
m˙in,m˙out
Aggregate mass-flow rates, kg/s. Incoming streams include any ambient backflow represented by the model.

02 · Balance stored energy

d(mcvT)dt=∑jm˙in,jcpTin,j−m˙outcpT−UA(T−Tamb)

Incoming streams carry enthalpy. The air already inside the cabin stores internal energy.

Symbols & units
cv,cp
Constant-volume and constant-pressure specific heat, J/(kg K).
T,Tin,j,Tamb
Absolute temperatures, K. Each incoming stream j has its own temperature.
UA
Overall cabin-to-ambient thermal conductance, W/K; this model uses 25 W/K.

03 · Convert the stored state to pressure

pV=mRT

Both mass and temperature influence cabin pressure.

Symbols & units
p,V
Cabin absolute pressure, Pa; fixed volume, m³.
R
Specific gas constant for air, 287.05 J/(kg K).

Rigid 60 m³ well-mixed cabin, initial sea-level pressure and 293.15 K. Aircraft climbs linearly for 900 s then levels; cabin target is min(0.25 × aircraft altitude, 2400 m). Synthetic outflow controller, 55 kPa relief onset and vacuum relief. Compressible orifice coefficient 0.7, wall UA = 25 W/K. Finite relief flow can permit pressure overshoot. No physiological limits, ECS pack cycle or aircraft-specific operating schedule.

FAA · aviation handbook library ↗

Physical relations and teaching sources support the stated concepts. Generic coefficients are explicitly illustrative; they are not measured manufacturer data. Numerical verification is separate from experimental validation. Model version: applied-labs-v1.1.

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