To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

GFS Projects Limited is a British company developing a vertical take-off and landing aircraft shaped like a flying saucer. The company was established in 2002 by Geoff Hatton, and won a contract with the US government in 2007 to design an unmanned aerial vehicle.

The GFS Projects design uses the Coandă effect, unlike the failed 1950s Avrocar project. The GFS Projects design is mechanically simpler, using negative upper surface air pressure caused by the Coanda effect. Scale prototypes capable of controlled flight have existed since 2005, constructed by both GFS Projects Ltd and amateur (enthusiast) UAV builders.

GFS is an abbreviation of Geoff's Flying Saucer[1].

Technical background

The concept of creating a disk or polygonal aircraft has been around for many years and there are numerous patent applications but the first relying on the Coanda effect acting on the upper surface alone was first put forward in a paper by R. J. Collins.[1]

Collins' invention is intended for civil UAV applications and aerial monitoring of urban areas.

A further paper described for a fully steerable and controllable air space platform accompanied by video footage of lift and attitude control.[2] The Coanda disk concept has a number of attractive features for use in a non hostile environments, however one disadvantage is that flight control presents a heavy power over head compared to other vertical take off and landing air platforms. As a consequence, flight endurance using electric or even internal combustion engines does not compare favorably with helicopters.. Archived 13 September 2017 at the Wayback Machine To overcome this problem, a disk gas turbine engine has been specifically designed to be accommodated on a Coanda disk aircraft.[3]

References

  1. ^ Coanda - A New Airspace Platform for UAVs by R J Collins, Seventeenth International conference at Bristol University in 2002
  2. ^ Coanda Flight Controls by R J Collins, Eighteenth International conference at Bristol University in 2003
  3. ^ Torque Equalised Disk Gas Turbine Engine for Coanda Class UAVs by R J Collins, Twenty-second International conference at Bristol University in 2007

External links


This page was last edited on 16 May 2024, at 10:12
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.