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词条 Tampier Avion-Automobile
释义

  1. Design and development

  2. Specifications

  3. References

  4. External links

name=Tampier Avion-Automobile image=Tampier Avion automobile L'Aéronautique December,1922.jpg caption=

}}{{Infobox Aircraft Type

type=Roadable aircraft national origin=France manufacturer= designer=and builder, René Tampier first flight=1921 introduced= retired= status= primary user= more users= produced= number built=2 program cost= unit cost= developed from= variants with their own articles=
}}

The Tampier Avion-Automobile was a French roadable aircraft designed and built by René Tampier in 1921. Only two were built.

In 1921 René Tampier tackled the problem of designing an aircraft that was self-propelled and steerable on roads by including a second, low-powered engine driving the main landing wheels through a standard car-type transmission. The roadwheels were completed with a retractable pair nearer the tail. These were steerable, so on the road the Tampier Avion-Automobile, with its wings and tailplane folded, travelled tail first.

Design and development

Apart from its roadworthy landing gear the Avion-Automobile was a largely conventional two bay biplane, with thin-section, two-spar wings mounted without stagger, sweep or dihedral. Though upper and lower wings had equal spans the lower one had a narrower chord so that it could be folded against the fuselage, at the same time allowing the trailing edges of the upper wings to meet above the fuselage. Only the lower wings carried ailerons. Each bay was defined by pairs of parallel, vertical interplane struts, with an extra pair at the inner end of the folding sections.[3]

In aircraft configuration the Avion-Automobile was powered by a {{convert|300|hp|kW|abbr=on|order=flip}} Hispano-Suiza 8F water-cooled V8 engine in the nose. The {{convert|10|hp|kW|abbr=on|order=flip}} four-cylinder, {{convert|500|cm3|cuin |abbr=on}} ancillary engine for road use, which shared the flight engine's water-cooling and radiator, was behind and below it, so to help keep the centre of gravity (c.g.) over mid-chord the honeycomb radiator was mounted centrally on the leading edge of the upper wing. Behind the engine the rectangular section fuselage was flat-sided with the tailplane on top and braced from below by a pair of parallel struts on each side. All three fixed tail surfaces were triangular and carried balanced control surfaces.[3]

As an aircraft, the Avion-Automobile's tailskid undercarriage was conventional, with mainwheels on an axle supported at each end by a faired V-strut. On the ground, they were driven by the ancillary engine via a car-type four-speed plus reverse gearbox, clutch and differential. The second set of wheels were retracted into the rear fuselage in flight, moving forward to keep the c.g. under the wings. After they were lowered on the ground for road use they were steered with the rudder pedals, the Avion-Automobile travelling tail first. Because of the change in direction of travel between flight and road configuration, its open cockpit placed pilot and driver facing each other, each equipped with appropriate controls. As an automobile, the Tampier was {{convert|2.45|m|ftin|abbr=on}} wide and {{convert|8.50|m|ftin|abbr=on}} long, with a wheel track of {{convert|1.45|m|ftin|abbr=on}}.[3]

In November 1921 two examples of the Avion-Automobile were displayed at the seventh Salon de l'Aéronautique, the only aircraft to arrive by road and drive onto their display stands. By the time of the show the Tampiers had flown satisfactorily and had also done many miles on the road, with a maximum speed of about {{convert|25|mph|km/h|abbr=on}}, though a later report of a trip gives top speed of {{convert|25-30|km/h|mph|abbr=on}} and only {{convert|18|km/h|mph|abbr=on}} on poor surfaces.[9] It was also at the Bourget lightplane meeting in May 1922, demonstrating its good ground handling.[10]

The ability to manoeuvre on the ground and travel along roads came with the penalty of carrying largely dead weight in the air. Tampier saw the Avion-Automobile more as a demonstration of a system that would come into its own on large aircraft, where the auxiliary motor's weight would be a smaller fraction of the total. Ground mobility independent of the flight engine would make it easier to return an airliner that had force-landed in a field with engine problems to an aerodrome equipped for repair work. Similarly, if a transport was forced to land away from its fog-bound destination, it could complete its journey by road. Flight remarked in 1922 that "it is not inconceivable that in years to come such arrangements will be found on most commercial machines."

Specifications

{{Aircraft specs
|ref=Les Ailes, January 1922[3]
|prime units?=met


|genhide=
|crew=One
|capacity=one passenger
|length m=8.50
|length note=
|span m=13
|span note=
|height m=2.80
|height note=
|wing area sqm=31
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=1300
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Hispano-Suiza 8F
|eng1 type=
|eng1 hp=300
|eng1 note=
|eng2 number=1
|eng2 name=Unknown
|eng2 type=water-cooled, 4-cylinder, {{convert|500|cm3|cuin |abbr=on}}
|eng2 hp=10
|eng2 note= for on-road use
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=170
|max speed note= approximately
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=42
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=0.31 kW/kg (0.1 hp/lb)
|more performance=
}}

References

1. ^{{cite journal |last=Lémonon |first=E-H |date=12 January 1922|title=L'avion-auto René Tampier|journal=Les Ailes|issue=30 |pages=2-3|url=http://gallica.bnf.fr/ark:/12148/bpt6k6555976k/f2 }}
2. ^{{cite journal |last=Lémonon |first=E-H |date=9 March 1922|title=A bord de l'avion-auto|journal=Les Ailes|issue=38 |pages=2|url=http://gallica.bnf.fr/ark:/12148/bpt6k65559844/f2 }}
3. ^{{cite journal |last=Frachet |first=André |date=9 March 1922|title=Le meeting du Bourget|journal=Les Ailes|issue=50 |pages=1|url=http://gallica.bnf.fr/ark:/12148/bpt6k6555996b/f1}}
[1][2][3]
}}

External links

  • Photo of the Tampier Avion-Automobile

2 : French sport aircraft 1920–1929|Roadable aircraft

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