CVV 8 Bonaventura: Difference between revisions
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The Bonaventura is an all wood aircraft with a 19 m (62 ft 4 in) span, [[shoulder wing|shoulder mounted]] wing, built around a single [[spar (aviation)|spar]]. Its airfoil section is from the [[NACA airfoil|NACA laminar flow 6-series]]. Ahead of the spar, the wing is skinned with [[plywood]] laid with its grain at 45° to the centre line for strength; this goes around the nose of the wing, forming a torsion resisting D-box. Behind the spar the wing is [[aircraft fabric covering|fabric covered]]. The plan is essentially double straight tapered, though a short centre section has a [[leading edge]] normal to the [[fuselage]] centre line, and a [[trailing edge]] slightly more forward sweep than outboard. Long, narrow [[chord (aircraft)|chord]] [[aileron]]s occupy about half the span; [[air brake (aircraft)|airbrakes]] are placed immediately inboard of the ailerons at mid-chord. These consist of seven rotating blades on each side which project both above and below the wing when deployed, counter-rotating away on chord-wise axes.<ref name=IVS/> |
The Bonaventura is an all wood aircraft with a 19 m (62 ft 4 in) span, [[shoulder wing|shoulder mounted]] wing, built around a single [[spar (aviation)|spar]]. Its airfoil section is from the [[NACA airfoil|NACA laminar flow 6-series]]. Ahead of the spar, the wing is skinned with [[plywood]] laid with its grain at 45° to the centre line for strength; this goes around the nose of the wing, forming a torsion resisting D-box. Behind the spar the wing is [[aircraft fabric covering|fabric covered]]. The plan is essentially double straight tapered, though a short centre section has a [[leading edge]] normal to the [[fuselage]] centre line, and a [[trailing edge]] slightly more forward sweep than outboard. Long, narrow [[chord (aircraft)|chord]] [[aileron]]s occupy about half the span; [[air brake (aircraft)|airbrakes]] are placed immediately inboard of the ailerons at mid-chord. These consist of seven rotating blades on each side which project both above and below the wing when deployed, counter-rotating away on chord-wise axes.<ref name=IVS/> |
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The fuselage is a ply shell, [[ovoid]] in cross section and built around a series of frames and [[stringer (aircraft)|stringer]]s. The [[tandem]] seats are enclosed ahead of the wing leading edge under a [[starboard]] hinged, continuous [[canopy (aircraft)|canopy]]. The Bonaventura has no wheeled undercarriage, but took off from a wheeled, drop-off dolly and landed on a simple, rubber sprung skid extending from nose to mid chord, aided by a sprung tail skid. The fuselage becomes slim towards the tail, where the double straight tapered horizontal tail is mounted on top of it, far enough forward that its trailing edge is at the [[rudder]] hinge. The [[elevator (aircraft)|elevators]] are fabric covered and the starboard one carries a [[trim tab]]. [[Fin]] and rudder are also straight tapered and the tall, fabric covered, [[balanced rudder|unbalanced rudder]] reaches down to the keel.<ref name=IVS/> |
The fuselage is a ply n, shell, [[ovoid]] in cross section and built around a series of frames and [[stringer (aircraft)|stringer]]s. The [[tandem]] seats are enclosed ahead of the wing leading edge under a [[starboard]] hinged, continuous [[canopy (aircraft)|canopy]]. The Bonaventura has no wheeled undercarriage, but took off from a wheeled, drop-off dolly and landed on a simple, rubber sprung skid extending from nose to mid chord, aided by a sprung tail skid. The fuselage becomes slim towards the tail, where the double straight tapered horizontal tail is mounted on top of it, far enough forward that its trailing edge is at the [[rudder]] hinge. The [[elevator (aircraft)|elevators]] are fabric covered and the starboard one carries a [[trim tab]]. [[Fin]] and rudder are also straight tapered and the tall, fabric covered, [[balanced rudder|unbalanced rudder]] reaches down to the keel.<ref name=IVS/> |
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==Operational history== |
==Operational history== |
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Revision as of 11:35, 4 November 2014
| Bonaventura | |
|---|---|
| Role | Two seat competition glider |
| National origin | Italy |
| Manufacturer | Centro Volo a Vela, Milan (CVV) |
| Designer | Ermenegildo Preti |
| First flight | 29 December 1957 |
| Number built | 15 |
The CVV 8 Bonaventura (English: Good Adventure) was a two seat competition glider designed and built in Italy during the 1950s. Fifteen were produced.
Design and development
The Bonaventura was designed at the Centro Volo a Vela (CVV), or Experimental Soaring Centre, of the Royal Polytechnic of Milan by Gildo Preti; though construction was started in 1952, the prototype was not completed until 1957. The first flight took place on 14 December that year. It was named after the fortunate eponymous protagonist of an Italian children's comic strip, Signor Bonaventura.[1]
The Bonaventura is an all wood aircraft with a 19 m (62 ft 4 in) span, shoulder mounted wing, built around a single spar. Its airfoil section is from the NACA laminar flow 6-series. Ahead of the spar, the wing is skinned with plywood laid with its grain at 45° to the centre line for strength; this goes around the nose of the wing, forming a torsion resisting D-box. Behind the spar the wing is fabric covered. The plan is essentially double straight tapered, though a short centre section has a leading edge normal to the fuselage centre line, and a trailing edge slightly more forward sweep than outboard. Long, narrow chord ailerons occupy about half the span; airbrakes are placed immediately inboard of the ailerons at mid-chord. These consist of seven rotating blades on each side which project both above and below the wing when deployed, counter-rotating away on chord-wise axes.[1]
The fuselage is a ply n, shell, ovoid in cross section and built around a series of frames and stringers. The tandem seats are enclosed ahead of the wing leading edge under a starboard hinged, continuous canopy. The Bonaventura has no wheeled undercarriage, but took off from a wheeled, drop-off dolly and landed on a simple, rubber sprung skid extending from nose to mid chord, aided by a sprung tail skid. The fuselage becomes slim towards the tail, where the double straight tapered horizontal tail is mounted on top of it, far enough forward that its trailing edge is at the rudder hinge. The elevators are fabric covered and the starboard one carries a trim tab. Fin and rudder are also straight tapered and the tall, fabric covered, unbalanced rudder reaches down to the keel.[1]
Operational history
Two Bonaventura prototypes were built by CVV, followed by a short production run of thirteen from Avionautica Rio.[1] These went to Italian gliding clubs. Three Bonaventuras survive in museum collections, though none were on public display in 2010.[2]
Specifications
Data from Italian Vintage Sailplanes[1]
General characteristics
- Crew: One
- Length: 7.91 m (25 ft 11 in)
- Wingspan: 19.0 m (62 ft 4 in)
- Wing area: 20 m2 (220 sq ft)
- Aspect ratio: 18
- Airfoil: NACA 653618[3]
- Empty weight: 295 kg (650 lb)
- Gross weight: 475 kg (1,047 lb)
Performance
- Never exceed speed: 220 km/h (140 mph, 120 kn) [3]
- Maximum glide ratio: estimated 36.7:1
- Wing loading: 24 kg/m2 (4.9 lb/sq ft)
References
- ^ a b c d e Pedrielli, Vincenzo; Camastra, Francesco (2011). Italian Vintage Sailplanes. Königswinter: EQIP Werbung & Verlag GmbH. pp. 111, 128–9. ISBN 978-3-9808838-9-4.
- ^ Ogden, Bob (2009). Aviation Museums and Collections of Mainland Europe. Air Britain (Historians). ISBN 978-0-85130-418-2.
- ^ a b "CVV 8 Bonaventura". Retrieved 30 November 2012.
