Westland Westbury: Difference between revisions
MilborneOne (talk | contribs) →References: tweak cat |
|||
| (20 intermediate revisions by 16 users not shown) | |||
| Line 1: | Line 1: | ||
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
||
{{Use dmy dates|date=March 2018}} |
|||
{|{{Infobox Aircraft Begin |
|||
{{Use British English|date=March 2018}} |
|||
{|{{Infobox aircraft begin |
|||
| name=Westland Westbury |
| name=Westland Westbury |
||
| image= |
| image=Westland Westbury.jpg |
||
| caption= |
| caption= |
||
}}{{Infobox |
}}{{Infobox aircraft type |
||
| type= |
| type=[[Fighter aircraft]] |
||
| national origin=United Kingdom |
| national origin=United Kingdom |
||
| manufacturer=[[Westland Aircraft]] |
| manufacturer=[[Westland Aircraft]] |
||
| Line 20: | Line 22: | ||
|} |
|} |
||
The '''Westland Westbury''' was a |
The '''Westland Westbury''' was a British twin-engined fighter prototype of 1926. Designed by [[Westland Aircraft]] it never entered service but played a useful role in the testing of the [[COW 37 mm gun]]. Only the two prototypes were completed. |
||
==Development== |
==Development== |
||
In 1924 the |
In 1924 the British [[Air Ministry]] issued [[Air Ministry Specification|specification]] 4/24 for a twin-engined home defence fighter, which would be employed to defend Britain against night attacks by enemy heavy bombers. The aircraft had to have a top speed of at least 125 mph (201 km/h) and a landing speed of not more than 50 mph (80 km/h). In September 1925 the Air Staff amended the specification to specify the use of the 37-mm [[COW 37 mm gun|COW gun]] and supercharged engines. From the design proposals submitted by the manufacturers, two types were selected for prototypes development, the [[Bristol Bagshot]] and the Westland Westbury.<ref name="Meekcoms">Meekcoms, K.J., and Morgan, E.B; The British Aircraft Specifications File. Air-Britain, UK, 1994.</ref> Two airframes were ordered from Westland, allotted serial numbers J7765 and J7766. |
||
The Westbury was a twin-engined three-bay biplane of conventional layout, large for its day irrespective of type and remarkably so for a fighter. The first prototype, |
The Westbury was a twin-engined three-bay biplane of conventional layout, large for its day irrespective of type and remarkably so for a fighter. The first prototype, J7765 was of all-wooden construction, while the second, J7766, had a mixed construction wing with a duralumin mainspar and wooden ribs. All surfaces were covered with fabric. The wings were of equal span, with three pairs of struts on each side and wire bracing. The fuselage was deep, of rectangular cross-section, and had a blunt nose. The crew of three had open cockpits in the nose (front gunner), in front of the wing (pilot) and aft of the wing (rear gunner). The landing gear was fixed. The {{convert|450|hp|abbr=on}} [[Bristol Jupiter]] VI air-cooled radial engines were installed without cowls on nacelles that were attached on top of the lower wing, at the innermost pair of struts. Each drove a two-bladed propeller. |
||
The first aircraft J7765 was delivered to the [[Aeroplane and Armament Experimental Establishment|A&AEE]] at [[RAF Martlesham Heath]] in 1926 and 1927. J7766, delivered the following year, was distinguished by having engine nacelles that extended aft of the trailing edge of the wing, the wing with duralumin spars and a metal-covered wing centre section, and a more rounded nose shape.<ref name="Mason">Mason, Tim. British Flight Testing Martlesham Heath 1920-1939. Putnam, UK, 1993</ref> The modified nose and nacelle shapes were also introduced on the first prototype.<ref name="Green">Green, William, and Swanborough, Gordon. The Complete Book of Fighters. |
The first aircraft J7765 was delivered to the [[Aeroplane and Armament Experimental Establishment|A&AEE]] at [[RAF Martlesham Heath]] in 1926 and 1927. J7766, delivered the following year, was distinguished by having engine nacelles that extended aft of the trailing edge of the wing, the wing with duralumin spars and a metal-covered wing centre section, and a more rounded nose shape.<ref name="Mason">Mason, Tim. British Flight Testing Martlesham Heath 1920-1939. Putnam, UK, 1993</ref> The modified nose and nacelle shapes were also introduced on the first prototype.<ref name="Green">Green, William, and Swanborough, Gordon. The Complete Book of Fighters. Greenwich Editions, UK 2004.</ref> |
||
Although the Westbury was judged to have good flying characteristics, and the competing Bristol Bagshot monoplane had serious structural problems,<ref name="Mason"/> it was not put into production. It was clear that the performance of the Westbury was insufficient to make it a useful fighter aircraft. However, it did serve for several years as an armament trials platform, mostly for the 37 mm COW gun. |
Although the Westbury was judged to have good flying characteristics, and the competing Bristol Bagshot monoplane had serious structural problems,<ref name="Mason"/> it was not put into production. It was clear that the performance of the Westbury was insufficient to make it a useful fighter aircraft. However, it did serve for several years as an armament trials platform, mostly for the 37 mm COW gun. |
||
==Armament and |
==Armament and trials== |
||
The Westbury could be fitted with defensive [[Lewis gun]]s on a [[Scarff ring]] position on top of the fuselage, aft of the COW gun mounting, and in a ventral mount. Its most important gun mountings were in the nose and immediately aft of the wing, and had special fittings for the much larger and heavier COW guns. |
The Westbury could be fitted with defensive [[Lewis gun]]s on a [[Scarff ring]] position on top of the fuselage, aft of the COW gun mounting, and in a ventral mount. Its most important gun mountings were in the nose and immediately aft of the wing, and had special fittings for the much larger and heavier COW guns. |
||
The COW gun mounting in the nose was of Westland design, and allowed the gun to be trained over a wide arc. It supported the gun on the apex of a pyramidal structure, that was asymmetric to allow the gunner to have easy access to the weapon. This structure was fixed on a rotating base, which also provided the gunner with a rotating platform to stand on. The gunner could train the mount by turning a hand gear, or push on a pedal to engage a brake that locked the mount in its position. The elevation and depression of the gun were accomplished by the muscle power of the gunner. As the large ammunition clip of the COW gun prevented sighting over the barrel, a sight was installed to its left. The gun is reported to have been successfully fired in the air, also when trained to the side.<ref name="King">King, H.F. Armament of British Aircraft 1909-1939. Military Book Society, UK, 1971.</ref><ref name="Clarke">Clarke, Wallace R. British Aircraft Armament Volume 2: RAF guns and gunsights from 1914 to the present day. Patrick Stephens, UK, 1994.</ref> |
The COW gun mounting in the nose was of Westland design, and allowed the gun to be trained over a wide arc. It supported the gun on the apex of a pyramidal structure, that was asymmetric to allow the gunner to have easy access to the weapon. This structure was fixed on a rotating base, which also provided the gunner with a rotating platform to stand on. The gunner could train the mount by turning a hand gear, or push on a pedal to engage a brake that locked the mount in its position. The elevation and depression of the gun were accomplished by the muscle power of the gunner. As the large ammunition clip of the COW gun prevented sighting over the barrel, a sight was installed to its left. The gun is reported to have been successfully fired in the air, also when trained to the side.<ref name="King">King, H.F. Armament of British Aircraft 1909-1939. Military Book Society, UK, 1971.</ref><ref name="Clarke">Clarke, Wallace R. British Aircraft Armament Volume 2: RAF guns and gunsights from 1914 to the present day. Patrick Stephens, UK, 1994.</ref> |
||
The rear COW gun mounting was installed immediately aft of the wing, in a fixed mount that only allowed for a limited adjustment of the angle. A special sight for this gun was installed in the pilot's cockpit.<ref name="King"/> This armament would be aimed by the pilot from a position below the aircraft attacked, in the manner of the [[Schräge Musik]] installation used by the Germans during WWII. However, the concept was based on the theory of [[no allowance sighting]], which sought to install the gun at an angle at which the body lift of the projectile, due to the forward motion of the aircraft, would compensate for the effect of gravity, straightening the trajectory.<ref name="Sinnott">Sinnott, Colin. The Royal Air Force and Aircraft Design 1923-1939. Frank Cass, UK, 2001.</ref> The first firing trials resulted in several broken wing ribs, and a special rubber-spring shield was developed to protect the upper wing.<ref name="King"/> |
The rear COW gun mounting was installed immediately aft of the wing, in a fixed mount that only allowed for a limited adjustment of the angle. A special sight for this gun was installed in the pilot's cockpit.<ref name="King"/> This armament would be aimed by the pilot from a position below the aircraft attacked, in the manner of the ''[[Schräge Musik]]'' installation used by the Germans during WWII. However, the concept was based on the theory of [[no allowance sighting]], which sought to install the gun at an angle at which the body lift of the projectile, due to the forward motion of the aircraft, would compensate for the effect of gravity, straightening the trajectory.<ref name="Sinnott">Sinnott, Colin. The Royal Air Force and Aircraft Design 1923-1939. Frank Cass, UK, 2001.</ref> The first firing trials resulted in several broken wing ribs, and a special rubber-spring shield was developed to protect the upper wing.<ref name="King"/> |
||
Over the period of gunnery trials continued between 1927 and 1930, thirteen reports of structural damage were filed, indicating that there remained problems with absorbing the blast and recoil of the guns. The Westbury was also used to test an [[Oerlikon Contraves|Oerlikon]] cannon in the aft position, at angles adjustable between 40 and 60 degrees, but this gun was found to have inadequate serviceability.<ref name="Mason"/> |
Over the period of gunnery trials continued between 1927 and 1930, thirteen reports of structural damage were filed, indicating that there remained problems with absorbing the blast and recoil of the guns. The Westbury was also used to test an [[Oerlikon Contraves|Oerlikon]] cannon in the aft position, at angles adjustable between 40 and 60 degrees, but this gun was found to have inadequate serviceability.<ref name="Mason"/> |
||
<!-- ==Operational history== --> |
|||
<!-- ==Variants== --> |
|||
<!-- ==Units using this aircraft/Operators (choose)== --> |
|||
==Specifications== |
==Specifications== |
||
{{aircraft specifications |
|||
{{Aircraft specs |
|||
|plane or copter?=plane |
|||
|jet or prop?=prop |
|||
|ref=Brew, Alec. The Turret Fighters - Defiant and Roc. Crowood, UK, 2002. |
|ref=Brew, Alec. The Turret Fighters - Defiant and Roc. Crowood, UK, 2002. |
||
|prime units?=imp |
|||
<!-- |
|||
General characteristics |
|||
--> |
|||
|crew=3 |
|crew=3 |
||
|length ft=43 |
|||
|capacity= <!-- the number of passengers carried in the case of a commercial aircraft--> |
|||
|length in=4.75 |
|||
|payload main= |
|||
| |
|length note= |
||
|span ft=68 |
|||
|payload more= |
|||
|span in= |
|||
|length main= 13.23 m |
|||
|span note= |
|||
|length alt= 43 ft 4.75 in |
|||
|height ft=13 |
|||
|span main= 20.73 m |
|||
|height in=9 |
|||
|span alt= 68 ft |
|||
|height |
|height note= |
||
|wing area sqft=875 |
|||
|height alt= 13 ft 9 in |
|||
|area |
|wing area note= |
||
|aspect ratio=<!-- sailplanes --> |
|||
|area alt= 875 sq. ft |
|||
|airfoil= |
|airfoil= |
||
|empty weight |
|empty weight lb=4854 |
||
|empty weight |
|empty weight note= |
||
| |
|gross weight lb=7877 |
||
| |
|gross weight note= |
||
|max takeoff weight lb= |
|||
|useful load main= |
|||
|max takeoff weight note= |
|||
|useful load alt= |
|||
|fuel capacity= |
|||
|max takeoff weight main= |
|||
|max takeoff weight alt= |
|||
|max takeoff weight more= |
|||
|more general= |
|more general= |
||
<!-- |
|||
|engine (prop)= |
|||
Powerplant |
|||
|type of prop=Bristol Jupiter VI |
|||
--> |
|||
|number of props=2 |
|||
|eng1 number=2 |
|||
|power main=450 hp |
|||
|eng1 name=[[Bristol Jupiter VI]] |
|||
|power alt= |
|||
|eng1 type=9-cylinder air-cooled radial piston engine |
|||
|power original= |
|||
|eng1 hp=450 |
|||
|power more= |
|||
|eng1 note= |
|||
|max speed main=201 km/h |
|||
|max speed alt=125 mph |
|||
|prop blade number=2 |
|||
|max speed more= |
|||
|prop name=fixed-pitch propellers |
|||
|cruise speed main= |
|||
|prop dia ft=<!-- propeller aircraft --> |
|||
|cruise speed alt= |
|||
|prop dia in=<!-- propeller aircraft --> |
|||
|cruise speed more |
|||
| |
|prop dia note= |
||
<!-- |
|||
|stall speed alt= |
|||
Performance |
|||
|stall speed more= |
|||
--> |
|||
|never exceed speed main= |
|||
| |
|max speed mph=125 |
||
|max speed note= |
|||
|range main= |
|||
|cruise speed mph= |
|||
|range alt= |
|||
| |
|cruise speed note= |
||
| |
|stall speed mph= |
||
| |
|stall speed note= |
||
|never exceed speed mph= |
|||
|ceiling main= |
|||
|never exceed speed note= |
|||
|ceiling alt= 19500 ft |
|||
|minimum control speed mph= |
|||
|climb rate main= 1525 m in 4.5 min |
|||
|minimum control speed note= |
|||
|climb rate alt= 5000 ft in 4.5 min |
|||
|range miles= |
|||
|loading main= |
|||
| |
|range note= |
||
|combat range miles= |
|||
|thrust/weight= |
|||
|combat range note= |
|||
|power/mass main= |
|||
|ferry range miles= |
|||
|power/mass alt= |
|||
|ferry range note= |
|||
|endurance=<!-- if range unknown --> |
|||
|ceiling ft= |
|||
|ceiling note= |
|||
|climb rate ftmin= |
|||
|climb rate note= |
|||
|time to altitude={{cvt|5000|ft|0}} in 4 minutes 15 seconds |
|||
|wing loading lb/sqft= |
|||
|wing loading note= |
|||
|fuel consumption lb/mi= |
|||
|power/mass= |
|||
|more performance= |
|more performance= |
||
<!-- |
|||
Armament |
|||
--> |
|||
|armament=Two 37-mm COW guns and one or two 7.7 mm Lewis guns |
|armament=Two 37-mm COW guns and one or two 7.7 mm Lewis guns |
||
|avionics= |
|||
}} |
}} |
||
| Line 123: | Line 135: | ||
==References== |
==References== |
||
{{commons category|Westland Westbury}} |
|||
{{reflist}} |
{{reflist}} |
||
{{refbegin}} |
{{refbegin}} |
||
{{refend}} |
{{refend}} |
||
<!-- ==External links== --> |
|||
{{Westland aircraft}} |
{{Westland aircraft}} |
||
{{Aviation lists}} |
|||
[[Category:Biplanes]] |
[[Category:Biplanes]] |
||
[[Category: |
[[Category:1920s British fighter aircraft]] |
||
[[Category:British fighter aircraft 1920–1929]] |
|||
[[Category:Westland aircraft|Westbury]] |
[[Category:Westland aircraft|Westbury]] |
||
[[Category:Twin piston-engined tractor aircraft]] |
|||
[[Category:Aircraft with fixed conventional landing gear]] |
|||
Latest revision as of 04:34, 8 November 2024
| Westland Westbury | |
|---|---|
| |
| Role | Fighter aircraft |
| National origin | United Kingdom |
| Manufacturer | Westland Aircraft |
| First flight | 1926 |
| Primary user | Royal Air Force |
| Number built | 2 |
The Westland Westbury was a British twin-engined fighter prototype of 1926. Designed by Westland Aircraft it never entered service but played a useful role in the testing of the COW 37 mm gun. Only the two prototypes were completed.
Development
[edit]In 1924 the British Air Ministry issued specification 4/24 for a twin-engined home defence fighter, which would be employed to defend Britain against night attacks by enemy heavy bombers. The aircraft had to have a top speed of at least 125 mph (201 km/h) and a landing speed of not more than 50 mph (80 km/h). In September 1925 the Air Staff amended the specification to specify the use of the 37-mm COW gun and supercharged engines. From the design proposals submitted by the manufacturers, two types were selected for prototypes development, the Bristol Bagshot and the Westland Westbury.[1] Two airframes were ordered from Westland, allotted serial numbers J7765 and J7766.
The Westbury was a twin-engined three-bay biplane of conventional layout, large for its day irrespective of type and remarkably so for a fighter. The first prototype, J7765 was of all-wooden construction, while the second, J7766, had a mixed construction wing with a duralumin mainspar and wooden ribs. All surfaces were covered with fabric. The wings were of equal span, with three pairs of struts on each side and wire bracing. The fuselage was deep, of rectangular cross-section, and had a blunt nose. The crew of three had open cockpits in the nose (front gunner), in front of the wing (pilot) and aft of the wing (rear gunner). The landing gear was fixed. The 450 hp (340 kW) Bristol Jupiter VI air-cooled radial engines were installed without cowls on nacelles that were attached on top of the lower wing, at the innermost pair of struts. Each drove a two-bladed propeller.
The first aircraft J7765 was delivered to the A&AEE at RAF Martlesham Heath in 1926 and 1927. J7766, delivered the following year, was distinguished by having engine nacelles that extended aft of the trailing edge of the wing, the wing with duralumin spars and a metal-covered wing centre section, and a more rounded nose shape.[2] The modified nose and nacelle shapes were also introduced on the first prototype.[3]
Although the Westbury was judged to have good flying characteristics, and the competing Bristol Bagshot monoplane had serious structural problems,[2] it was not put into production. It was clear that the performance of the Westbury was insufficient to make it a useful fighter aircraft. However, it did serve for several years as an armament trials platform, mostly for the 37 mm COW gun.
Armament and trials
[edit]The Westbury could be fitted with defensive Lewis guns on a Scarff ring position on top of the fuselage, aft of the COW gun mounting, and in a ventral mount. Its most important gun mountings were in the nose and immediately aft of the wing, and had special fittings for the much larger and heavier COW guns.
The COW gun mounting in the nose was of Westland design, and allowed the gun to be trained over a wide arc. It supported the gun on the apex of a pyramidal structure, that was asymmetric to allow the gunner to have easy access to the weapon. This structure was fixed on a rotating base, which also provided the gunner with a rotating platform to stand on. The gunner could train the mount by turning a hand gear, or push on a pedal to engage a brake that locked the mount in its position. The elevation and depression of the gun were accomplished by the muscle power of the gunner. As the large ammunition clip of the COW gun prevented sighting over the barrel, a sight was installed to its left. The gun is reported to have been successfully fired in the air, also when trained to the side.[4][5]
The rear COW gun mounting was installed immediately aft of the wing, in a fixed mount that only allowed for a limited adjustment of the angle. A special sight for this gun was installed in the pilot's cockpit.[4] This armament would be aimed by the pilot from a position below the aircraft attacked, in the manner of the Schräge Musik installation used by the Germans during WWII. However, the concept was based on the theory of no allowance sighting, which sought to install the gun at an angle at which the body lift of the projectile, due to the forward motion of the aircraft, would compensate for the effect of gravity, straightening the trajectory.[6] The first firing trials resulted in several broken wing ribs, and a special rubber-spring shield was developed to protect the upper wing.[4]
Over the period of gunnery trials continued between 1927 and 1930, thirteen reports of structural damage were filed, indicating that there remained problems with absorbing the blast and recoil of the guns. The Westbury was also used to test an Oerlikon cannon in the aft position, at angles adjustable between 40 and 60 degrees, but this gun was found to have inadequate serviceability.[2]
Specifications
[edit]Data from Brew, Alec. The Turret Fighters - Defiant and Roc. Crowood, UK, 2002.
General characteristics
- Crew: 3
- Length: 43 ft 4.75 in (13.2271 m)
- Wingspan: 68 ft (21 m)
- Height: 13 ft 9 in (4.19 m)
- Wing area: 875 sq ft (81.3 m2)
- Empty weight: 4,854 lb (2,202 kg)
- Gross weight: 7,877 lb (3,573 kg)
- Powerplant: 2 × Bristol Jupiter VI 9-cylinder air-cooled radial piston engine, 450 hp (340 kW) each
- Propellers: 2-bladed fixed-pitch propellers
Performance
- Maximum speed: 125 mph (201 km/h, 109 kn)
- Time to altitude: 5,000 ft (1,524 m) in 4 minutes 15 seconds
Armament
Two 37-mm COW guns and one or two 7.7 mm Lewis guns
See also
[edit]
References
[edit]
- ^ Meekcoms, K.J., and Morgan, E.B; The British Aircraft Specifications File. Air-Britain, UK, 1994.
- ^ a b c Mason, Tim. British Flight Testing Martlesham Heath 1920-1939. Putnam, UK, 1993
- ^ Green, William, and Swanborough, Gordon. The Complete Book of Fighters. Greenwich Editions, UK 2004.
- ^ a b c King, H.F. Armament of British Aircraft 1909-1939. Military Book Society, UK, 1971.
- ^ Clarke, Wallace R. British Aircraft Armament Volume 2: RAF guns and gunsights from 1914 to the present day. Patrick Stephens, UK, 1994.
- ^ Sinnott, Colin. The Royal Air Force and Aircraft Design 1923-1939. Frank Cass, UK, 2001.