I have been making the mistake of using words "propeller" and "rotor" interchangeably when they are not the same thing. What is the difference between a propeller and a rotor?

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    $\begingroup$ 'at times' ... 'somewhat interchangeable'. When? Can you provide examples? It might help someone like me who's so accustomed to aviation terminology that these terms don't really ever feel interchangeable at all. The only exception is maybe the V-22, which uses what they call proprotors. $\endgroup$ – egid Jan 25 '17 at 19:06
  • $\begingroup$ I've always understood a rotor to be a horizontal propeller mounted on a helicopter, while a propeller was a vertical rotor mounted on a airplane. i.e., they're the same thing, differing only in the angle at which they're mounted to the craft in question. (I do realize that there tends to be a fair bit of twist in some propeller blades that doesn't seem to occur in rotor blades, but otherwise, same-same.) $\endgroup$ – FreeMan Jan 25 '17 at 20:00
  • $\begingroup$ @FreeMan A helicopter rotor and a propeller both have aerofoils, fixed to a hub and rotated by an engine. That's about the end of the similarities. Propellers and rotor heads are far from same-same. Most aspects of their design are different. $\endgroup$ – Simon Jan 25 '17 at 20:32
  • $\begingroup$ @egid Modified to address your comment, thanks. $\endgroup$ – ryan1618 Jan 25 '17 at 21:49
  • $\begingroup$ @egid: The "rotor" part of the word "Proprotor" is due to the V22's Propellers being able to rotate perpendicular to their main axis, I would think. $\endgroup$ – jjack Feb 25 '18 at 8:35

Short answer:

  • A propeller is used to propel something, the force at stake being called thrust. Thrust is usually horizontal (but not always, think about rockets). This device comes from the navy domain.

  • A rotor of a rotorcraft is used to control anything, including the altitude, the generated force being called lift. Lift is generally vertical (but not always, think about a rudder). Rotors have generally more than two blades.

Lift and thrust involved are components of the same physical force (the aerodynamic force) to which we refer to differently based on their purpose after an arbitrary breakdown based on the direction they act (compared to the direction of the aircraft or to the gravity field).

For our pleasure, let's also talk about a turbine rotor, which is a rotor/propeller which doesn't produce lift or thrust, but convert the fluid velocity (actually momentum) into torque. For example the wind turbine rotor. A turbine rotor is certainly a propeller, but we don't refer to it as a propeller, as it propels nothing.

Rotor is the most generic name for something spun by a shaft. It can be used for a propeller, the rotating wing of an helicopter, the rotating elements of a compressor or a turbine, etc. You can't be wrong using rotor for any spinning device. Rotor (rotating) is the antonym of stator (stationary). These terms are not specific to aerodynamics, in a electric motor there is usually a stator and a rotor as well.

The rotor of a rotorcraft comprises blades and is comparable to a propeller, if we except blades additional freedom in flapping and leading-lagging to limit vibrations created by repeated force swings encountered while performing a 360° turn.

enter image description here
Source: Wikipedia

But actually the main rotor is a (rotating) wing, and the anti-torque rotor is a (rotating) rudder. Their blades are meant to produce lift like the wing and the rudder they replace. Because lift is involved, we tend to name them rotors rather than propellers.

A propeller also comprises blades, fixed on the rotation axis.

enter image description here

The purpose of a propeller is to propel the aircraft, that is to push it in the direction of its flight.

Both a rotorcraft rotor, a propeller and a wing create the same aerodynamic force. However the conventions are:

  • A rotor and a wing are used to eventually counter weight and control altitude, and a propeller to eventually counter drag and control velocity along the flight path (I say eventually because to gain altitude you usually temporary increase thrust, that's a detail)

  • A rotor and a wing create lift, a propeller creates thrust.

Wing, propeller blade and rotorcraft blades work exactly the same from an aerodynamic standpoint. The resultant of their action is the total aerodynamic force, which is then broken down arbitrarily into lift, drag, thrust and torque to facilitate mechanical analysis.


  1. Moving an aircraft along its path (thrust) is easier than maintaining its altitude (lift), and therefore a main rotor is far larger than a propeller for aircraft of the same mass.

  2. The horizontal displacement of the rotorcraft is also produced by the main rotor (cyclic control), so some part of the aerodynamic force can also be seen as thrust, and the rotor also acts as a propeller.

  3. Propeller is used for simple propellers and not in turbine engines. While the fan of a turbofan is comparable to a propeller, participates to thrust production and aircraft propulsion, the fan is still only one part of a system (guide vanes, fan duct and exhaust nozzle greatly maximize final thrust). Bottom line the fan is a rotor, not a propeller.

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    $\begingroup$ Hmm. (Some) Rotor blades (rotorcraft) are not fixed, some are. Depending on the head design, they may or may not have flapping and lead-lag hinges. $\endgroup$ – Simon Jan 25 '17 at 19:56
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    $\begingroup$ @Simon: You're the master of rotorcraft :-) I mean they can lead-lag thanks to their flexibility. Correct? $\endgroup$ – mins Jan 25 '17 at 20:02
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    $\begingroup$ Exactly. In a fixed head, the forces from flapping and drag (lead/lag) are absorbed by the blades flexing. Plus 1 anyway ;) $\endgroup$ – Simon Jan 25 '17 at 20:07
  • $\begingroup$ And what would be the most correct term or terms for the non- flapping fixed-blade rotors or propellers used on radio-controlled quadcopter models, and on manned aircraft designed along similar principles? $\endgroup$ – quiet flyer Mar 30 '20 at 0:57
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    $\begingroup$ @Auberron: You're right, that's explained in the answer, and also in the previous comment. $\endgroup$ – mins Mar 30 '20 at 11:33
  • Rotor is a generic term for a rotating part of a mechanical device.
  • Fan is a rotor that creates a flow within a fluid (i.e. gas or liquid).
  • Propeller is a fan with the purpose to create thrust.

According to these definitions, it is not wrong to name propellers as rotors and vice versa.

In aviation language usually helicopters have rotors and planes have propellers, because:

  • A plane propeller creates (mostly) thrust, and the lift is created (mostly) by the wings.
  • The air flow from a helicopter rotor generates both, lift and thrust.

  • Helicopters are differentiated from planes by rotary wings versus fixed wings.


In general a rotor is anything that requires continuous rotation to function. Rotors also occur in devices such as the distributor in an electrical ignition system and in some rotary pumps.

The vertical-axis rotary wing, used for lift by helicopters and gyroplanes, is commonly called a rotor. Horizontal-axis lifting rotors also exist; the flanged cylindrical Flettner rotor and the flat wing rotor are two examples of Magnus rotors. More complex horizontal-axis lifting rotors include the cyclogyro and FanWing, both examples of the cross-flow fan.

A spinning set of blades designed to create gas flow is often called a fan. Such fans are typically housed in a duct.

A spinning set of blades designed to create thrust for forward motion is often called a propeller. But this is not so far from the function of a fan, so here we get into niceties, such as;

  • Where a ship's propeller typically has very broad short blades, an aircraft propeller typically has long thin ones.
  • Where a propeller typically has a small number of blades, a fan typically has a large number. For aircraft this is sometimes expressed as disc coverage; if you look through the rotor disc and see mostly the far scenery then it is a propeller but if you see mostly blades then it is a fan (note that it does not apply to marine propellers).
  • The ducted front stage of a high-bypass turbofan engine, which provides much of the thrust, is called a fan. This contrasts with the free-air propeller of the turboprop.
  • A piston engine with a ducted propeller is likely to have it called a ducted propulsor.
  • Some modern turbine engines have multi-blade thrusters curved to avoid compressibility effects and spinning in free air; these have sometimes in the past been described a ductless fans, although Europrop call them propellers.

I trust that is wholly clear and unambiguous to you! Or, to put it another way, the industry just makes it up as it goes along and uses whatever word seems like a good idea at the time. You just have to remember what they have decided for each gadget.

  1. Propeller is getting lift from the wing and thrust from the propeller but helicopter gets both from the rotor.
  2. propeller aircraft can not hover over a spot but helicopter can.
  3. Propeller aircraft can not perform vertical landing but helicopter can do.
  4. Propeller blade is pre-twisted but helicopter blade are symmetrical.
  5. Propeller aircraft has two hard/re-enforcing point such as: Wing root and Engine mount but helicopter has only one hard point that is "ROTOR MAST" and more differences are there.
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    $\begingroup$ Please don't use a signature, tagline or similar. If you want to display your credentials, you can do so in your profile. See What kind of behavior is expected of users?, specifically the point on Do not use signature, taglines, or greetings. $\endgroup$ – user Feb 25 '18 at 11:28
  • $\begingroup$ This answers a different question: "list some differences between airplanes and helicopters." $\endgroup$ – Camille Goudeseune Mar 29 '20 at 17:35

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