Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Design and development  





2 Specifications  





3 Sources  





4 References  





5 External links  














Collins X-112






Français
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


X-112
Role Ground effect vehicle
National origin United States
Manufacturer Collins Radio Company
Designer Alexander Lippisch
First flight 1963
Number built 1
Developed into RFB X-113

The Collins X-112 was an experimental two-seat ground-effect vehicle, designed by Alexander Lippisch in the United States in the early 1960s to test his thick reverse delta wing concept.

Design and development[edit]

Lippisch's development of his Aerofoil Boat, a ground-effect vehicle for use over water, began whilst he was working in the aviation division of the Collins Radio CompanyinCedar Rapids, Iowa, US. The Collins X-112 was built to test the concept.[1][2]

The Airfoil Boat was an inverse-delta aircraft, that is, it had a wing which was triangular in plan but with a straight, unswept leading edge.[1] Combined with strong anhedral, this layout produces stable flight in ground effect.[3] Specifically, it is claimed that it is stable in pitch and also that it can fly in ground effect at altitudes up to about 50% of its span, allowing it to operate over rough water. This contrasts with the lower-aspect-ratio square wing of the ekranoplans, which leaves ground effect at only 10% of span, limiting them to the calmer waters of lakes and rivers.[4]

Its fuselage was conventional, with flat sides and rounded decking. The nose-mounted single engine was of very low power, only 25 hp (19 kW). Two open cockpits were arranged in tandem, both over the wing. Aft of the trailing edge root the bottom of the fuselage rose strongly to carry a tall, broad fin and rudder. The X-112 had a T-tail, carrying elevators. Its thick airfoil wings were low-mounted, each with a tip float or "pontoon", which in combination with the strong anhedral kept the fuselage well clear of the water surface. Each float carried a winglet fitted with an aileron for roll control. A retractable water-rudder, fuselage-mounted at the point at which the lower fuselage rose upwards, provided directional control on the water surface.[1]

Tests made during 1963 began with the Airfoil Boat operated like any fast motor boat, planing on the surface. With speeds increased to around 36 mph (58 km/h) the X-112 rose clear of the surface as a ram-air air cushion or ground-effect vehicle. Solo free flights at up to 77 mph (124 km/h) were made; tests with two occupants were also conducted. "Entirely satisfactory" stability and control characteristics were reported under all these conditions.[1] With the Airfoil Boat proved, the X-112's mission was completed, and Lippisch, suffering from cancer, left Collins Radio. He recovered sufficiently to design and build its successor, the fibreglass, more powerful X-113 with Rhein-Flugzeugbau GmbH in Germany.[2]

Specifications[edit]

Data from Jane's All the World's Aircraft[1]

General characteristics

Performance

Sources[edit]

References[edit]

  1. ^ a b c d e Taylor, John W. R. (1964). Jane's All the World's Aircraft 1964–65. London: Sampson Low, Marston & Co. Ltd. p. 207.
  • ^ a b Taylor, John W. R. (1974). Jane's All the World's Aircraft 1974–75. London: Jane's Yearbooks. p. 98. ISBN 0-354-00502-2.
  • ^ Lee Qihui (2006). "Stability and Control of an Inverted Delta Wing In Ground Effect Aircraft" (PDF). Archived from the original (PDF) on June 22, 2007. Retrieved 25 September 2013.
  • ^ "Ekratoplan vs. Lippisch". Archived from the original on 4 September 2013. Retrieved 25 September 2013.
  • External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Collins_X-112&oldid=1121851257"

    Categories: 
    Ground effect vehicles
    Low-wing aircraft
    Single-engined tractor aircraft
    Aircraft first flown in 1963
    1960s United States experimental aircraft
    T-tail aircraft
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Aircraft specs templates using more performance parameter
    Articles containing potentially dated statements from November 2020
    All articles containing potentially dated statements
     



    This page was last edited on 14 November 2022, at 13:35 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki