Ducted fan

Summary

In aeronautics, a ducted fan is a thrust-generating mechanical fan or propeller mounted within a cylindrical duct or shroud. Other terms include ducted propeller or shrouded propeller.[1] When used in vertical takeoff and landing (VTOL) applications it is also known as a shrouded rotor.[2]

The duct reduces losses in thrust from the tips of the fan blades. By varying the cross-section of the duct the designer can advantageously affect the velocity and pressure of the airflow according to Bernoulli's principle. Ducted fans are used for propulsion or direct lift in many types of vehicle including aeroplanes, airships, hovercraft, and powered lift VTOL aircraft.

DesignEdit

A ducted fan has three main components; the fan or propeller which provides thrust or lift, the duct or shroud which surrounds the fan, and the engine or motor which powers the fan.

FanEdit

Like any other fan, propeller or rotor, a ducted fan is characterised by the number of blades. The Rhein Flugzeugbau (RFB) SG 85 had three blades, while the Dowty Rotol Ducted Propulsor had seven.[3][4] The blades may be of fixed or variable pitch.

DuctEdit

The duct or shroud is an aerodynamic ring which surrounds the fan and closely fits the blade tips. It must be made rigid enough not to distort under flight loads and touch the blades as they turn. The duct performs several functions:

Principally, it reduces the vortices created by air flowing round the ends of the blades. This reduces the aerodynamic losses or drag, thus increasing the overall efficiency of the fan. Because of this, the fan can either be used to provide increased thrust and aircraft performance, or be made smaller than the equivalent free propeller.

It provides acoustic shielding which, together with the reduced energy waste, significantly cuts noise emissions from the propeller.[4]

It acts as a protective device, both to protect objects such as ground staff from being hit by the whirling blades, and to protect the blades from damage during such an impact.

The reduced tip vortices also mean that the fan wake is less turbulent. With careful design, the heated discharge from the engine cooling system can be injected into the low-turbulence fan wake to increase thrust.[4]

PowerplantEdit

A ducted fan may be powered by any kind of motor capable of turning the fan. Examples include piston, rotary (Wankel), and turboshaft combustion engines, as well as electric motors.

The fan may be mounted directly on the powerplant output shaft, or driven remotely via an extended drive shaft and gearing. In the remote arrangement, several fans may be driven by a single powerplant.

Ducted propulsorEdit

An assembly designed throughout as a single integrated unit is referred to as a fan pod or ducted propulsor.[3][4]

An advantage of the pod approach is that the design of each component can be matched to the others, helping to maximise performance and minimise weight. It also eases the vehicle designer's task of integration with the vehicle and its systems.

LimitationsEdit

  • Good efficiency requires very small clearances between the blade tips and the duct.
  • Efficiency advantages are reduced, and may even be reversed, at lower rotation speeds, thrust levels and airspeeds.
  • Requires reduced vibration levels compared to a free propeller or rotor.
  • Complex duct design, and weight increase even if constructed from advanced composites.
  • At high angle of attack, parts of the duct will stall and produce aerodynamic drag.[5]

ApplicationsEdit

 
Ducted fans on an airship or dirigible

In aircraft applications, the operating speed of an unshrouded propeller is limited since tip speeds approach the sound barrier at lower speeds than an equivalent ducted fan. The most common ducted fan arrangement used in full-sized aircraft is a turbofan engine, where the power to turn the fan is provided by a gas turbine. High bypass ratio turbofan engines are used on nearly all civilian airliners, while military fighters usually make use of the better high-speed performance of a low bypass ratio turbofan with a smaller fan diameter. However, a ducted fan may be powered by any source of shaft power such as a reciprocating engine, Wankel engine, or electric motor. A kind of ducted fan, known as a fantail or by the trademark name Fenestron, is also used to replace tail rotors on helicopters.

 
A Sailor checks the ducted propeller of a Landing Craft Air Cushion (LCAC) Hovercraft

Ducted fans are favored in VTOL aircraft such as the Lockheed Martin F-35 Lightning II, and other low-speed designs such as hovercraft for their higher thrust-to-weight ratio.

In some cases, a shrouded rotor can be 94% more efficient than an open rotor. The improved performance is mainly because the outward flow is less contracted and thus carries more kinetic energy.[6]

Among model aircraft hobbyists, the ducted fan is popular with builders of high-performance radio controlled model aircraft. Internal-combustion glow engines combined with ducted-fan units were the first achievable means of modeling a scaled-size jet aircraft. Despite the introduction of model-scale turbojet engines, electric-powered ducted fans remain popular on smaller, lower-cost model aircraft. Some electric-powered ducted fan airplanes can reach speeds of more than 320km/h (200mph).

Most types of fans used in computers contain a duct integrated into the fan assembly; the duct is also used for mechanically mounting the fan to other components.

 
The Martin Jetpack, a personal aircraft powered by ducted fans

See alsoEdit

ReferencesEdit

  1. ^ Anita I. Abrego and Robert W. Bulaga; "Performance Study of a Ducted Fan System", NASA, 2002.
  2. ^ Kotwani, Kailash; "Ducted Fan or Shrouded Rotor Aerodynamics and its Application in Miniature VTOL Aerial Vehicles", 2009. (retrieved 22 March 2022).
  3. ^ a b Jane's All the World's Aircraft 1980-81, Jane's, 1980. p.704.
  4. ^ a b c d Jane's All the World's Aircraft 1980-81, Jane's, 1980. p.725.
  5. ^ Jon Longbottom - Mechanical aeronautics, thesis in PDF format
  6. ^ Pereira, Jason L. Hover and wind-tunnel testing of shrouded rotors for improved micro air vehicle design p147+p11. University of Maryland, 2008. Accessed: 28 August 2015.