Nieuport B.N.1: Difference between revisions
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{{Use dmy dates|date=February 2018}} |
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{{Use British English|date=February 2018}} |
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{|{{Infobox Aircraft Begin |
{|{{Infobox Aircraft Begin |
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|name = B.N.1<!--please avoid stating manufacturer in this field; it's stated two lines below --> |
|name = B.N.1<!--please avoid stating manufacturer in this field; it's stated two lines below --> |
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|designer = [[Henry Folland]] |
|designer = [[Henry Folland]] |
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|first flight = February 1918 |
|first flight = February 1918 |
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|retired = |
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|introduced = <!--date the aircraft entered or will enter military or revenue service--> |
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|status = abandoned prototype |
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|introduction= <!--date the aircraft will enter military or revenue service, if the aircraft is still in development --> |
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|retired = <!--date the aircraft left military or revenue service. If vague or multiples, it probably should be skipped--> |
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|status = Prototype<!--in most cases, this field is redundant; use it sparingly--> |
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|primary user = <!--please list only one, and don't use those tiny flags as they limit horizontal space--> |
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|more users = <!--limited to three "more users" total. please separate with <br/>--> |
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|produced = <!--years in production, e.g. 1970-1999, if still in active use but no longer built--> |
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|number built = 1 |
|number built = 1 |
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|developed from = <!-- the aircraft which formed the basis for the topic type --> |
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==Specifications == |
==Specifications == |
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{{Aircraft specs |
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{{aircraft specifications |
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|prime units?=imp |
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|plane or copter?=plane<!-- options: plane/copter --> |
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|jet or prop?=prop<!-- options: jet/prop/both/neither --> |
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|crew=One |
|crew=One |
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|length ft=18|length in=6 |
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|capacity= |
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|span ft=28|span in=0 |
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|length alt=5.64 m |
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|span main= 28 ft 0 in |
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|span alt=8.54 m |
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|height alt=2.74 m |
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|area alt=24.2 m² |
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|airfoil= |
|airfoil= |
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|gross weight lb=2030 |
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|fuel capacity={{cvt|36|impgal|USgal L}}<ref>Bruce 1957, p. 318.</ref> |
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|empty weight alt=<!-- kg --> |
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<!--Powerplant--> |
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|loaded weight main= 2,030 lb |
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|loaded weight alt= 923 kg |
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|eng1 hp=230<!-- prop engines --> |
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|useful load main= |
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|useful load alt= |
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|max takeoff weight main= |
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|max takeoff weight alt= |
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|engine (prop)=[[Bentley BR1]] |
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|number of props=1 |
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|power main=230 hp |
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|power alt=172 kW |
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|power original= |
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|max speed alt=110 knots, 204 km/h |
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|max speed more= at 15,000 ft (4,600 m) |
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|cruise speed alt=<!-- mph, km/h--> |
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|never exceed speed main=<!-- knots--> |
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|stall speed main=<!-- knots--> |
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|stall speed alt=<!-- mph, km/h--> |
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|range main= <!--nm--> |
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|range alt=<!-- mi, km--> |
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|ceiling alt=7,900 m |
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|climb rate main=<!-- ft/min--> |
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|climb rate alt=<!-- m/s--> |
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|loading main= lb/ft² |
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|loading alt= kg/m² |
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|thrust/weight=<!-- a unitless ratio --> |
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|power/mass main= hp/lb |
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|power/mass alt= W/kg |
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*'''Endurance:''' 3 hr |
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*'''Climb to 15,000 ft (4,600 m):''' 16 min |
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|avionics= |
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|prop blade number=2<!-- propeller aircraft --> |
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|prop name=wood fixed pitch propeller |
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|prop dia ft=|prop dia in= |
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<!--Performance--> |
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|max speed note=at {{cvt|15000|ft}} |
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|range miles= |
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|endurance=3 hr |
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|ceiling note=(absolute ceiling) |
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|time to altitude=16 min to {{cvt|15000|ft}} |
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*Bruce, J.M. ''British Aeroplanes 1914-18''. London:Putnam, 1957. |
*Bruce, J.M. ''British Aeroplanes 1914-18''. London:Putnam, 1957. |
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*Bruce, J.M. ''War Planes of the First World War: Volume One:Fighters''. London:Macdonald, 1965. |
*Bruce, J.M. ''War Planes of the First World War: Volume One:Fighters''. London:Macdonald, 1965. |
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*Mason, Francis K. ''The British Fighter since 1912''. Annapolis, USA:Naval Institute Press, 1992. ISBN |
*Mason, Francis K. ''The British Fighter since 1912''. Annapolis, USA:Naval Institute Press, 1992. {{ISBN|978-1557500823}}. |
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*"[http://www.flightglobal.com/pdfarchive/view/1916/1916%20-%201024.html New Companies Registered]". ''[[Flight International|Flight]]'', 16 November 1916. p. 1016. |
*"[http://www.flightglobal.com/pdfarchive/view/1916/1916%20-%201024.html New Companies Registered]". ''[[Flight International|Flight]]'', 16 November 1916. p. 1016. |
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{{Nieuport & General aircraft}} |
{{Nieuport & General aircraft}} |
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[[Category:British fighter aircraft |
[[Category:1910s British fighter aircraft]] |
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[[Category:Nieuport & General aircraft|B.N.1]] |
[[Category:Nieuport & General aircraft|B.N.1]] |
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[[Category:Rotary-engined aircraft]] |
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[[Category:Biplanes]] |
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[[Category:Aircraft first flown in 1918]] |
Latest revision as of 10:49, 3 May 2021
B.N.1 | |
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Role | Fighter |
National origin | United Kingdom |
Manufacturer | Nieuport & General Aircraft |
Designer | Henry Folland |
First flight | February 1918 |
Status | abandoned prototype |
Number built | 1 |
The Nieuport B.N.1 was a prototype British single-engined fighter aircraft of the First World War. It was a single-engined biplane intended to replace the Sopwith Camel, but only one was built, being destroyed in a crash. The Sopwith Snipe was built instead to replace the Camel.
Development and design
[edit]In 1917, as a result of an official Inquiry (the Burbidge Report) into the activities of the Royal Aircraft Factory, design and construction of aircraft at Farnborough ceased, and the Factory's design teams were broken up.[1] This allowed the Nieuport & General Aircraft Co Ltd, which was formed at Cricklewood, London in 1916 to license produce French Nieuport aircraft,[2] to acquire the services of Henry Folland, previously responsible for the design of the S.E.5 fighter, as chief designer.[1] His first design for Nieuport & General was another fighter, intended to meet Air Board Specification A.1.A for a replacement for the Sopwith Camel, in competition with designs submitted by Sopwith (the Sopwith Snipe), Austin Motors (the Austin Osprey) and Boulton & Paul (the Bobolink).[3]
This aircraft, designated Nieuport B.N.1 (for "British Nieuport"), was a single-engined, single seat tractor biplane of wooden construction. It had equal-span, unstaggered two bay wings, a slab-sided fuselage and was powered by a 230 hp (172 kW) Bentley BR2 rotary engine. A distinctive feature was a ventral fin, as used on the S.E.5 (which was to become a distinguishing mark of many of Folland's designs). Armament was the normal pair of synchronised Vickers machine guns together with a Lewis gun mounted on the upper wing, firing over the propeller.[4]
Three B.N.1s were ordered, the first one flying in February 1918. When it was evaluated, it demonstrated performance that was generally superior to the Snipe, with a much better ceiling. It was destroyed, however, on 10 March 1918 when its engine (only the sixth BR2 built) caught fire in the air. This caused the B.N.1 to be abandoned, with the Snipe being purchased to replace the Camel, and Folland concentrating on the design of the more advanced Nieuport Nighthawk.[5]
Specifications
[edit]Data from The British Fighter since 1912.[5]
General characteristics
- Crew: One
- Length: 18 ft 6 in (5.64 m)
- Wingspan: 28 ft 0 in (8.53 m)
- Height: 9 ft 0 in (2.74 m)
- Wing area: 260 sq ft (24 m2)
- Gross weight: 2,030 lb (921 kg)
- Fuel capacity: 36 imp gal (43 US gal; 160 L)[6]
- Powerplant: 1 × Bentley BR2 9-cylinder rotary engine, 230 hp (170 kW)
- Propellers: 2-bladed wood fixed pitch propeller
Performance
- Maximum speed: 127 mph (204 km/h, 110 kn) at 15,000 ft (4,600 m)
- Endurance: 3 hr
- Service ceiling: 26,000 ft (7,900 m) (absolute ceiling)
- Time to altitude: 16 min to 15,000 ft (4,600 m)
Armament
- Guns: 2 x forward firing, synchronised .303 in (7.7 mm) Vickers machine guns and one .303 in (7.7 mm) Lewis gun above upper wing
See also
[edit]Related development
Aircraft of comparable role, configuration, and era
References
[edit]- Bruce, J.M. British Aeroplanes 1914-18. London:Putnam, 1957.
- Bruce, J.M. War Planes of the First World War: Volume One:Fighters. London:Macdonald, 1965.
- Mason, Francis K. The British Fighter since 1912. Annapolis, USA:Naval Institute Press, 1992. ISBN 978-1557500823.
- "New Companies Registered". Flight, 16 November 1916. p. 1016.