Aviation glossary

Compressor

Also: axial compressor, high-pressure compressor, centrifugal compressor

Section of a turbine engine that raises the pressure of incoming air through successive rows of rotating blades and fixed vanes before it reaches the combustor.

What it is

Compressors in modern aero engines are axial: air flows along the shaft through a series of stages, each made up of a rotating row of blades (the rotor) and a fixed row of vanes (the stator). Each stage raises the pressure a little, and in the latest engines the whole compressor can multiply it more than forty times.

A modern turbofan usually splits compression into two or three sections on concentric shafts that turn at different speeds, each driven by its own turbine. Rolls-Royce Trent engines use three shafts; most General Electric and CFM engines use two.

Small turboprops and many auxiliary power units also use centrifugal compressors, in which an impeller flings the air outwards. The compressor absorbs a large share of the energy the turbine produces, and on many aircraft it also supplies the bleed air used to pressurise the cabin.

On Vuelopedia

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This page was last updated on October 9, 2026

APA

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MLA

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Harvard

Vuelopedia (2026) Compressor. Available at: https://vuelopedia.org/en/glossary/compressor (Accessed: 17 October 2026).

BibTeX

@misc{vuelopedia_en_glossary_compressor,
  author       = {{Vuelopedia}},
  title        = {{Compressor}},
  publisher    = {Fundación Poderia},
  year         = {2026},
  date         = {2026-10-09},
  url          = {https://vuelopedia.org/en/glossary/compressor},
  howpublished = {\url{https://vuelopedia.org/en/glossary/compressor}},
  urldate      = {2026-10-17},
  note         = {Accessed 2026-10-17}
}

Wikipedia

{{cite web |url=https://vuelopedia.org/en/glossary/compressor |title=Compressor |website=Vuelopedia |publisher=Fundación Poderia |date=2026-10-09 |access-date=2026-10-17 |language=en}}

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