<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = Gallaudet hydroplane | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = | aim = | outcome = | related = | national_origin = United States of America | manufacturer = Gallaudet Aircraft Corporation | design_group = | designer = Edson Fessenden Gallaudet, H.A. Lewis<ref>{{cite book|title=Technology's war record: an interpretation of the contribution|author=Massachusetts Institute of Technology. Alumni Association. War Records Committee|page=704}}</ref> | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}

The '''Gallaudet Hydroplane''' ({{aka}} '''Gallaudet Wing-Warping Kite''' or '''Hydro-Bike''') is an early aircraft employing the use of wing-warping for roll control.<ref>{{cite web|title=Flying Machines|url=http://www.flyingmachines.org/gallau.html|accessdate=28 December 2011}}</ref>

==Development==

The Gallaudet Hydroplane was built in Norwich, Connecticut, by Edson Fessenden Gallaudet. The principle of wing-warping was independently applied to this kite/aircraft/glider several years before the Wright Brothers applied it to their Wright Flyer. (along with Jean-Marie LeBris, John J. Montgomery, Clement Ader, D.D. Wells, and Hugo Mattullath).<ref>{{cite journal|title=Oldies and Oddities: Where Do Ailerons Come From?|journal=Air & Space Magazine|date=September 2009|author=Tom Couch}}</ref><ref>Harwood, Craig S. and Fogel, Gary B. ''Quest for Flight: John J. Montgomery and the Dawn of Aviation in the West,'' University of Oklahoma Press 2012.</ref> The Wrights later applied for a patent on wing-warping, which led to the widespread use of the aileron control method to avoid the Wright's airplane patents. Gallaudet generically employed the name hydroplane to many of his future seaplane designs. In 1908, Gallaudet would form the Gallaudet Engineering Company, (later the Gallaudet Aircraft Corporation). Later hydroplane models were built for the United States Navy.<ref name="a1" >{{cite news|newspaper=The News|title=Trying Out Norwich Built Hydroplane on the Thames|date=3 August 1916}}</ref>

==Design== The 1897 Gallaudet Hydroplane glider featured twin floats, a central pyramidal support frame, and flexible wooden wing ribs (employing wing warping) with fabric-covering.<ref>{{cite web|title=Galludet Glider|url=http://flyingmachines.ru/Site2/Crafts/Craft30387.htm|accessdate=28 December 2011}}</ref><ref>{{cite web|title=Washington D.C. Gallaudet|url=http://oes.gallaudet.edu/washingtondc/History_Culture/|accessdate=28 December 2011|archive-url=https://web.archive.org/web/20120426080106/http://oes.gallaudet.edu/washingtondc/History_Culture/|archive-date=26 April 2012|url-status=dead}}</ref>

In 1913, Gallaudet filed U.S. Patent# 1,214,536 for the Hydroplane. The single-place open cockpit aircraft featured most of the engine enclosed in the fuselage. The fuselage tapered upwards to the rear with a small attached rudder. A single landing wheel protruded partially from the center of the fuselage for ground landings.<ref>{{cite book|title=Official gazette of the United States Patent Office, Volume 235|author=United States. Patent Office|page=20|date=6 February 1917}}</ref>

==Operational history== The Gallaudet Hydroplane was on display at the East Hall of the Arts and Industries Building of the Smithsonian Museum.<ref>{{cite web|title=Gallaudet Hydroplane|url=http://siarchives.si.edu/collections/siris_sic_433|accessdate=26 December 2011}}</ref>

Test flights for later hydroplanes built for U.S. Navy acceptance were performed at Gales Ferry, Connecticut in 1916.<ref name="a1" /> <!--==Variants==--> <!-- ==Units using this aircraft/Operators (choose)== -->

==Specifications (Hydroplane) == {{Aircraft specs |ref=Smithsonian<!-- for giving the reference for the data --> |prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> <!-- General characteristics --> |genhide=

|crew= |capacity= |length m= |length ft=7 |length in= |length note= |span m= |span ft=11 |span in=6 |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m=<!-- swing-wings --> |swept ft=<!-- swing-wings --> |swept in=<!-- swing-wings --> |swept note= |dia m=<!-- airships etc --> |dia ft=<!-- airships etc --> |dia in=<!-- airships etc --> |dia note= |width m=<!-- if applicable --> |width ft=<!-- if applicable --> |width in=<!-- if applicable --> |width note= |height m= |height ft=5 |height in=6 |height note= |wing area sqm= |wing area sqft= |wing area note= |swept area sqm=<!-- swing-wings --> |swept area sqft=<!-- swing-wings --> |swept area note= |volume m3=<!-- lighter-than-air --> |volume ft3=<!-- lighter-than-air --> |volume note= |aspect ratio=<!-- give where relevant eg sailplanes --> |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=25 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg=<!-- lighter-than-air --> |lift lb=<!-- lighter-than-air --> |lift note= |more general= <!-- Powerplant --> |eng1 number= |eng1 name= |eng1 type= |eng1 kw=<!-- prop engines --> |eng1 hp=<!-- prop engines --> |eng1 kn=<!-- jet/rocket engines --> |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |power original= |thrust original= |eng1 kn-ab=<!-- afterburners --> |eng1 lbf-ab=<!-- afterburners -->

|eng2 number= |eng2 name= |eng2 type= |eng2 kw=<!-- prop engines --> |eng2 hp=<!-- prop engines --> |eng2 kn=<!-- jet/rocket engines --> |eng2 lbf=<!-- jet/rocket engines --> |eng2 note= |eng2 kn-ab=<!-- afterburners --> |eng2 lbf-ab=<!-- afterburners -->

|eng3 number= |eng3 name= |eng3 type= |eng3 kw=<!-- prop engines --> |eng3 hp=<!-- prop engines --> |eng3 kn=<!-- jet/rocket engines --> |eng3 lbf=<!-- jet/rocket engines --> |eng3 note= |eng3 kn-ab=<!-- afterburners --> |eng3 lbf-ab=<!-- afterburners --> |more power=

|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note=

|rot number=<!-- helicopters --> |rot dia m=<!-- helicopters --> |rot dia ft=<!-- helicopters --> |rot dia in=<!-- helicopters --> |rot area sqm=<!-- helicopters --> |rot area sqft=<!-- helicopters --> |rot area note= <!-- Performance --> |perfhide=

|max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=<!-- aerobatic --> |stall speed mph=<!-- aerobatic --> |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms=<!-- sailplanes --> |sink rate ftmin=<!-- sailplanes --> |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note=

|power/mass= |thrust/weight=

|more performance= <!-- Armament --> |armament=<!-- add (bulleted list) here or if you want to use the following specific parameters, remove this parameter--> |guns= |bombs= |rockets= |missiles=

|hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other=

|other armament=

|avionics= }}

==See also== {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related= *Gallaudet D-4<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}

==References== {{reflist}} <!-- insert the reference sources here --> <!-- ==Further reading== --> <!-- ==External links== -->

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Category:Floatplanes Category:Glider aircraft Hydroplane