LVG B.I

LVG B.I
LVG B.I
General information
Type	Two-seat reconnaissance biplan
National origin	Germany
Manufacturer	Luft-Verkehrs-Gesellschaft
Primary user	Luftstreitkräfte

The LVG B.I was a 1910s German two-seat reconnaissance biplane designed by Luft-Verkehrs-Gesellschaft for the Luftstreitkräfte.

Development

LVG had been involved in the operation of dirigibles before it started design, in 1912, of the company's first original design, the B.I. The B.I was an unequal-span two-seat biplane with a fixed tailskid landing gear. It was powered by a nose-mounted 80 kW (100 hp) Mercedes D.I engine. After entering service an improved variant, the B.II was developed with a cut-out in the upper wing to improve visibility for the pilot in the rear cockpit to help spot ground infantry and fitted with a 90 kW (120 hp) Mercedes D.II engine. The B.II entered service in 1915 and although mainly used as a trainer it was also used for unarmed reconnaissance and scouting duties. A further variant was the B.III which had structural strengthening to allow it to be used as a trainer.

The Euler company built the B.I and B.II under license as the Euler B.I and Euler B.II respectively. The B.III was likewise built under license by Euler as the Euler B.III.^[1]^[2]

Variants

B.I - Production variant powered by an 80 kW (100 hp) Mercedes D.I engine.
- Otto B.I/LVG B.I(Ot) - Otto-built B.I.^[3]
B.II - Improved variant powered by a 90 kW (120 hp) Mercedes D.II engine.
- Lebedev IX - Captured B.II rebuilt by Lebed and supplied to the Imperial Russian Air Force
B.III - Training variant with strengthened structures.

Operators

File:Flag of Bulgaria.svg Bulgaria

Bulgarian Air Force

File:Flag of Denmark.svg Denmark

Royal Danish Air Force

File:Flag of the German Empire.svg German Empire

Luftstreitkrafte

File:Flag of Turkey.svg Turkey

Ottoman Air Force

Specifications (B.I)

Data from ^[4]

General characteristics

Crew: 2 (pilot, observer)
Length: 8.30 m (27 ft 2.75 in)
Wingspan: 12.12 m (39 ft 9.25 in)
Height: 2.95 m (9 ft 8.25 in)
Wing area: 35.40 m² (381.05 sq ft)
Empty weight: 726 kg (1,600 lb)
Gross weight: 1,075 kg (2,370 lb)
Powerplant: 1 × Mercedes D.I inline piston engine , 75 kW (100 hp)

Performance

Maximum speed: 105 km/h (65 mph, 56 kn)
Endurance: 4 hours 0 minutes

References

Notes

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^ Herris, Jack, 2019. Otto, AGO, and BFW Aircraft of WWI: A Centennial Perspective on Great War Airplanes (Great War Aviation Centennial Series). Aeronaut Books.
^ Orbis 1985, page 2277

Bibliography

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[3] Herris, Jack, 2019. Otto, AGO, and BFW Aircraft of WWI: A Centennial Perspective on Great War Airplanes (Great War Aviation Centennial Series). Aeronaut Books.

[4] Orbis 1985, page 2277

[1]

[2]

[3]

[4]

v t e Idflieg B-class aircraft designations
AEG	B.I B.II B.III
Albatros	B.I B.II B.III
Aviatik	B.I B.II B.III
DFW	B.I B.II
Euler	B.I B.II B.III
Germania	B.I
Gotha	B.I B.II
Halberstadt	B.I B.II B.III
Kondor	B.I
LVG	B.I B.II B.III
NFW	B.I
Otto	B.I
Rumpler	B.I
Sablatnig	B.I
Siemens-Schuckert	B.I

v t e World War I aircraft of the Central Powers
Fighters	AEG D.I AEG Dr.I Albatros D.I Albatros D.II Albatros D.III Albatros D.V Aviatik D.I Aviatik C.VI Daimler L.6 Euler D.I Euler D.II Fokker D.I Fokker D.II Fokker D.III Fokker D.IV Fokker D.V Fokker D.VI Fokker D.VII Fokker D.VIII Fokker Dr.I Fokker E.I Fokker E.II Fokker E.III Fokker E.IV Fokker E.V Halberstadt D.II Hannover CL.II Hannover CL.III Hannover CL.IV Hannover CL.V Hansa-Brandenburg W.12 Hansa-Brandenburg W.29 Junkers D.I Kondor D.6 Kondor E.III Naglo D.II Pfalz D.III Pfalz D.XII Pfalz Dr.I Pfalz E.I Pfalz E.II Phönix D.I LFG Roland D.II LFG Roland D.VI Siemens-Schuckert D.I Siemens-Schuckert D.II Siemens-Schuckert D.III Siemens-Schuckert D.IV Zeppelin-Lindau D.I
Bombers and ground attack	AEG DJ.I AEG G.I AEG G.II AEG G.III AEG G.IV AEG G.V AEG J.I AEG J.II AEG R.I Friedrichshafen G.II Friedrichshafen G.III Gotha G.I Gotha G.II Gotha G.III Gotha G.IV Gotha G.V Gotha GL.VII Gotha G.IX Hannover CL.II Junkers CL.I Junkers J.I Rumpler G.I Rumpler G.II Rumpler G.III Siemens-Schuckert L.I Zeppelin-Lindau Rs.II Zeppelin-Lindau Rs.III Zeppelin-Lindau Rs.IV Zeppelin-Staaken R.VI
Reconnaissance	AEG B.I AEG B.II AEG B.III AEG C.I AEG C.II AEG C.III AEG C.IV AEG C.V AEG C.VI AEG C.VII AEG C.VIII AGO C.I AGO C.II AGO C.III AGO C.IV AGO C.VII AGO C.VIII Albatros B.I Albatros B.II Albatros C.I Albatros C.III Albatros C.V Albatros C.VII Albatros C.IX Albatros C.X Albatros C.XII Aviatik B.I Aviatik B.II Aviatik C.I Aviatik C.VI DFW C.V LFG Roland C.II LVG B.I LVG C.II Rumpler C.I Rumpler C.IV Rumpler Taube
Trainers	Euler D.I
Prototypes	Albatros C.II Fokker V.1 Fokker V.2 Junkers J 1 Junkers J 2 Zeppelin-Lindau Rs.I

LVG B.I

Contents

Development

Variants

Operators

Specifications (B.I)

See also

References

Notes

Bibliography

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LVG B.I

Development

Variants

Operators

Specifications (B.I)

See also

References

Notes

Bibliography

Navigation menu

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