Blériot 67: Difference between revisions
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{{short description|French WW1 bomber aircraft}} |
{{short description|French WW1 bomber aircraft}} |
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{|{{Infobox aircraft begin |
{|{{Infobox aircraft begin |
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| name=Blériot 67 |
| name=Blériot Bl.67 B.3 |
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| image=Blériot 67 01.jpg |
| image=Blériot 67 01.jpg |
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| caption= |
| caption= |
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}}{{Infobox aircraft type |
}}{{Infobox aircraft type |
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| type= |
| type=Heavy bomber |
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| national origin=France |
| national origin=France |
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| manufacturer=[[Blériot Aéronautique|Blériot]] |
| manufacturer=[[Blériot Aéronautique|Blériot]] |
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| designer= |
| designer= |
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| first flight=18 September 1916 |
| first flight=18 September 1916 |
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| introduced= |
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| retired= |
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| status= |
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| produced= |
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| primary user= |
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| number built=1 |
| number built=1 |
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| developed |
| developed into=[[Blériot 71]] |
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| variants with their own articles= |
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| developed into= |
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}} |
}} |
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The '''Blériot 67''' was a [[First World War]] [[France|French]] heavy bomber designed and built by [[Blériot Aéronautique|Blériot]] for a 1916 competition ''Concours des Avions Puissants''.<ref name="orbis" /> Only a single prototype was built.<ref name="orbis" /> |
The '''Blériot Bl.67 B.3''' was a [[First World War]] [[France|French]] biplane heavy bomber designed and built by [[Blériot Aéronautique|Blériot]] for a 1916 competition ''Concours des Avions Puissants''.<ref name="orbis" /> Only a single prototype was built.<ref name="orbis" /> |
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The Blériot 67 was a large equal-span biplane with a fuselage braced between the two wings, the four {{ |
The Blériot Bl.67 was a large equal-span biplane with a fuselage braced between the two wings, the four {{cvt|100|hp|order=flip}} Gnome 9B rotary engines above each other, with two on the upper wing leading edge and two on the lower wing on each side of the fuselage..<ref name="orbis" /> It had a biplane tail with three fins and a fixed conventional landing gear with twin-wheel main units.<ref name="orbis" /> It was first flown on 18 September 1916 but crashed on landing and was destroyed. |
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==Specifications== |
==Specifications== |
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|ref=<ref name=Aviafrance/> |
|ref=<ref name=Aviafrance/> |
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|prime units?= met |
|prime units?= met |
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<!-- |
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General characteristics |
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--> |
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|genhide= |
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|crew=3 |
|crew=3 |
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|length m=11.80 |
|length m=11.80|span m=19.60 |
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|span m=19.60 |
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|height m= |
|height m= |
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|height ft= |
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|height in= |
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|height note= |
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|wing area sqm=89.00 |
|wing area sqm=89.00 |
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|aspect ratio=<!-- sailplanes --> |
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|airfoil= |
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|empty weight kg=1800 |
|empty weight kg=1800 |
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|gross weight kg=3500 |
|gross weight kg=3500 |
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<!-- Powerplant --> |
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|max takeoff weight kg= |
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|eng1 number=4|eng1 name=[[Gnome Monosoupape 9 Type B-2]]|eng1 type=9-cyl. air-cooled rotary piston engine|eng1 hp=100 |
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|max takeoff weight lb= |
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|prop blade number=2|prop name=fixed-pitch wood propellers|prop dia m= |
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|max takeoff weight note= |
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<!-- Performance --> |
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|fuel capacity= |
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|more general= |
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<!-- |
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Powerplant |
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--> |
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|eng1 number=4 |
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|eng1 name=[[Gnome Monosoupape 9 Type B-2]] |
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|eng1 type=9-cyl. air-cooled rotary piston engine |
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|eng1 kw=<!-- prop engines --> |
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|eng1 hp=100 |
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|prop blade number=2 |
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|prop name=fixed-pitch propellers |
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|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
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|prop dia in=<!-- propeller aircraft --> |
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|prop dia note= |
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<!-- |
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Performance |
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--> |
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|max speed kmh= |
|max speed kmh= |
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|max speed mph= |
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|max speed kts= |
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|max speed note= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh= |
|cruise speed kmh= |
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|cruise speed mph= |
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|cruise speed kts= |
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|cruise speed note= |
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|stall speed kmh= |
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|stall speed mph= |
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|stall speed kts= |
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|stall speed note= |
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|never exceed speed kmh= |
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|never exceed speed mph= |
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|never exceed speed kts= |
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|never exceed speed note= |
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|minimum control speed kmh= |
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|minimum control speed mph= |
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|minimum control speed kts= |
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|minimum control speed note= |
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|range km= |
|range km= |
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|endurance= |
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|range miles= |
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|range nmi= |
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|range note= |
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|combat range km= |
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|combat range miles= |
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|combat range nmi= |
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|combat range note= |
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|ferry range km= |
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|ferry range miles= |
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|ferry range nmi= |
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|ferry range note= |
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|endurance=<!-- if range unknown --> |
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|ceiling m= |
|ceiling m= |
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|ceiling ft= |
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|ceiling note= |
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|g limits=<!-- aerobatic --> |
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|roll rate=<!-- aerobatic --> |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
|climb rate ms= |
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|climb rate ftmin= |
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|climb rate note= |
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|time to altitude= |
|time to altitude= |
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|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
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|sink rate note= |
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|lift to drag= |
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|wing loading kg/m2= |
|wing loading kg/m2= |
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<!-- Armament --> |
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|wing loading lb/sqft= |
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|wing loading note= |
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|disk loading kg/m2= |
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|disk loading lb/sqft= |
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|disk loading note= |
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|fuel consumption kg/km= |
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|fuel consumption lb/mi= |
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|power/mass= |
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|thrust/weight= |
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|more performance= |
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<!-- |
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Armament |
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--> |
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|armament=<!-- add bulletted list here or if you want to use the following |
|armament=<!-- add bulletted list here or if you want to use the following |
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specific parameters, remove this parameter--> |
specific parameters, remove this parameter--> |
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==References== |
==References== |
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===Citations=== |
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;Notes |
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{{reflist|refs= |
{{reflist|refs= |
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<ref name="orbis">{{cite book |title= The [[Illustrated Encyclopedia of Aircraft]] (Part Work 1982-1985)|publisher= Orbis Publishing|page=699}}</ref> |
<ref name="orbis">{{cite book |title= The [[Illustrated Encyclopedia of Aircraft]] (Part Work 1982-1985)|publisher= Orbis Publishing|page=699}}</ref> |
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}} |
}} |
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==Bibliography== |
===Bibliography=== |
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{{commons category}} |
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*{{cite journal |last1=Cony |first1=Christophe|last2=Laureau|first2=Patrick|name-list-style=amp |title=Un Blériot oublié: le bombardier LXVII de 1916 |journal=Avions: Toute l'Aéronautique et Son Histoire |date=September 1999 |issue=78 |pages=54–57 |trans-title=A Forgotten Blériot: The Model 67 Bomber of 1916|language=French |issn=1243-8650}} |
*{{cite journal |last1=Cony |first1=Christophe|last2=Laureau|first2=Patrick|name-list-style=amp |title=Un Blériot oublié: le bombardier LXVII de 1916 |journal=Avions: Toute l'Aéronautique et Son Histoire |date=September 1999 |issue=78 |pages=54–57 |trans-title=A Forgotten Blériot: The Model 67 Bomber of 1916|language=French |issn=1243-8650}} |
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*{{cite book |last1=Davilla |first1=Dr. James J. |last2=Soltan |first2=Arthur M. |title=French Aircraft of the First World War |date=January 2002 |publisher=Flying Machines Press |isbn=1-891268-09-0|name-list-style=amp}} |
*{{cite book |last1=Davilla |first1=Dr. James J. |last2=Soltan |first2=Arthur M. |title=French Aircraft of the First World War |date=January 2002 |publisher=Flying Machines Press |isbn=1-891268-09-0|name-list-style=amp}} |
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<!-- ==External links== --> |
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{{Louis Blériot aircraft}} |
{{Louis Blériot aircraft}} |
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[[Category:Rotary-engined aircraft]] |
[[Category:Rotary-engined aircraft]] |
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[[Category:Four-engined piston aircraft]] |
[[Category:Four-engined piston aircraft]] |
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[[Category:Aircraft flown once]] |
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Latest revision as of 05:50, 30 October 2024
| Blériot Bl.67 B.3 | |
|---|---|
| |
| Role | Heavy bomber |
| National origin | France |
| Manufacturer | Blériot |
| First flight | 18 September 1916 |
| Number built | 1 |
| Developed into | Blériot 71 |
The Blériot Bl.67 B.3 was a First World War French biplane heavy bomber designed and built by Blériot for a 1916 competition Concours des Avions Puissants.[1] Only a single prototype was built.[1]
The Blériot Bl.67 was a large equal-span biplane with a fuselage braced between the two wings, the four 75 kW (100 hp) Gnome 9B rotary engines above each other, with two on the upper wing leading edge and two on the lower wing on each side of the fuselage..[1] It had a biplane tail with three fins and a fixed conventional landing gear with twin-wheel main units.[1] It was first flown on 18 September 1916 but crashed on landing and was destroyed.
Specifications
[edit]Data from [2]
General characteristics
- Crew: 3
- Length: 11.80 m (38 ft 9 in)
- Wingspan: 19.60 m (64 ft 4 in)
- Wing area: 89.00 m2 (958.0 sq ft)
- Empty weight: 1,800 kg (3,968 lb)
- Gross weight: 3,500 kg (7,716 lb)
- Powerplant: 4 × Gnome Monosoupape 9 Type B-2 9-cyl. air-cooled rotary piston engine, 75 kW (100 hp) each
- Propellers: 2-bladed fixed-pitch wood propellers
Performance
References
[edit]Citations
[edit]- ^ a b c d The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. p. 699.
- ^ "Blériot 67". Retrieved 21 April 2012.
Bibliography
[edit]
Wikimedia Commons has media related to Blériot 67.
- Cony, Christophe & Laureau, Patrick (September 1999). "Un Blériot oublié: le bombardier LXVII de 1916" [A Forgotten Blériot: The Model 67 Bomber of 1916]. Avions: Toute l'Aéronautique et Son Histoire (in French) (78): 54–57. ISSN 1243-8650.
- Davilla, Dr. James J. & Soltan, Arthur M. (January 2002). French Aircraft of the First World War. Flying Machines Press. ISBN 1-891268-09-0.