Piasecki PV-2

{{Short description|US helicopter prototype}}

{{Infobox Aircraft Begin

|name = PV-2

|image = File:Piasecki PV-2 hovering (1943).jpg

|caption = PV-2 in flight testing

|logo =

}}{{Infobox Aircraft Type

|type = Helicopter

|manufacturer = P-V Engineering Forum

|designer = Frank Piasecki

|first flight = April 11, 1943

|introduction =

|retired =

|status =

|primary user =

|more users =

|produced = 1943

|number built = 1

|program cost=

|unit cost =

|developed from =

|variants with their own articles =

}}

The Piasecki PV-2 is a helicopter designed by Frank Piasecki. The PV-2 is best known for being one of the first successful helicopters flown in the United States. The PV-2 first flew on April 11, 1943.[http://nationalaviation.blade6.donet.com/components/content_manager_v02/view_nahf/htdocs/menu_ps.asp?NodeID=-911146831&group_ID=1134656385&Parent_ID=-1 National Aviation Hall of Fame - Frank Piasecki] {{webarchive|url=https://web.archive.org/web/20080522160248/http://nationalaviation.blade6.donet.com/components/content_manager_v02/view_nahf/htdocs/menu_ps.asp?NodeID=-911146831&group_ID=1134656385&Parent_ID=-1 |date=2008-05-22 }} Developed as a technology demonstrator, the PV-2 brought several new features such as the first dynamically balanced rotor blades, a rigid tail rotor with a tension-torsion pitch change system, and a full cyclic and collective rotor pitch control.

The PV-2 is now on display at the National Air and Space Museum's Steven F. Udvar-Hazy Center

Specifications

{{Aircraft specs

|ref=History - single rotor helicopters: PV-2{{cite web|url=http://www.piasecki.com/pv-21.htm |title=History - single rotor helicopters: PV-2| archive-url=https://web.archive.org/web/20080315062936/http://www.piasecki.com/pv-21.htm |archive-date=2008-03-15 |date=2001}}

|prime units?=imp

|crew=1

|capacity=2

|length ft=21

|length in=6

|length note=fuselage

|height ft=

|height in=

|height note=

|empty weight lb=

|empty weight note=

|gross weight lb=

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|max takeoff weight lb=1000

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Franklin 4AC-199

|eng1 type=4-cylinder horizontally-opposed piston engine

|eng1 hp=90

|eng1 note=at 2,500 rpm{{cite web |last1=Erickson |first1=Jack |title=Franklin1 |url=http://www.enginehistory.org/Piston/HOAE/Franklin1.html |website=www.enginehistory.org |publisher=Aircraft Engine Historical Society |accessdate=21 January 2020 |date=1 November 2016}}

|rot number=1

|rot dia m=7.6

|rot dia in=

|rot area sqft=488.4

|rot area note=

  • Blade section: NACA 0012{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}

|max speed mph=100

|max speed note=

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|never exceed speed mph=

|never exceed speed note=

|range miles=150

|range note=

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|ferry range miles=

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|ceiling ft=

|ceiling note=

|g limits=

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}}

References

{{Reflist}}