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Contents

   



(Top)
 


1 Design and development  





2 Specifications  





3 See also  





4 References  














Blériot 110






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From Wikipedia, the free encyclopedia
 


Blériot 110
Role Long-distance research aircraft
Manufacturer Blériot Aéronautique
Designer Filippo Zappata
First flight 16 May 1930
Number built 1

The Blériot 110 (orBlériot-Zappata 110) was a French aircraft built in 1930 to attempt new world aerial distance records.

Design and development

[edit]

Built specifically at the request of the ordered by the Service Technique of the French Air Ministry. it was a two-seat high-wing monoplane constructed of wood.[1] The fuselage was a stressed-skin structure with a teardrop-shaped cross section, with two upper longerons and a ventral keel: the load-bearing covering consisted of three layers of whitewood strips.[2]

It was fitted with six fuel tanks in the wings and four in the fuselage, holding a total of 6,000 L (1,319 Imperial gallons or 1,585 US gal). Because the pilot and co-pilots seats were behind the fuselage fuel tanks, a periscope was fitted for take-offs and landings. A sleeping couch was fitted behind the co-pilot's station so one of the crew members could sleep on long-distance flights.[3]

The aircraft's first flight on 16 May 1930 was cut short by a fuel supply problem, although no damage was sustained. After repairs, it was taken to Oran, Algeria, to make an attempt on the closed-circuit distance record. Between 15 November and 26 March 1932, the Blériot 110, flown by Lucien Bossoutrot and Maurice Rossi, broke this record three times; on the final occasion staying aloft for 76 hours 34 minutes and covering a distance of 10,601 km (6,587 mi). By this time, the aircraft had been named Joseph Le Brix in honour of the pilot who had died flying the 110's rival, the Dewoitine D.33.

On 5 August 1933, Paul Codos and Maurice Rossi set a new straight-line distance record, flying from New YorktoRayak, Lebanon – a distance of 9,105 km (5,658 mi). Further records were attempted over the next two years, but these were proved unsuccessful, and the 110 was scrapped.

Specifications

[edit]
Bleriot 110 3-view drawing from NACA Aircraft Circular No.138

General characteristics

Performance

See also

[edit]

Aircraft of comparable role, configuration, and era

References

[edit]
Notes
  • ^ NACA circular no.138: the Bleriot 110 Pierre Léglise. National Advisory Committee for Aeronautics, Washington, 1931 1931.https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930090426.pdf
  • ^ "Mirrors Help Record Ship Take-Off and Land." Popular Mechanic, December 1933, p. 807.
  • Bibliography

    Retrieved from "https://en.wikipedia.org/w/index.php?title=Blériot_110&oldid=1209254646"

    Categories: 
    High-wing aircraft
    Single-engined tractor aircraft
    1930s French experimental aircraft
    Blériot aircraft
    Aircraft first flown in 1930
    Hidden categories: 
    Articles with short description
    Short description is different from Wikidata
    Commons category link is on Wikidata
     



    This page was last edited on 21 February 2024, at 01:02 (UTC).

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