请输入您要查询的百科知识:

 

词条 Peyret-Le Prieur seaplane
释义

  1. Design and development

  2. Specifications (Sergant engine)

  3. References

name=Peyret-le Prieur seaplane image= caption=

}}{{Infobox Aircraft Type

type= floatplane trainer national origin=France manufacturer=Louis Peyret designer= Louis Peyret first flight=24 August 1924 introduced= retired= status= primary user= more users= produced= number built=1 or 2 program cost= unit cost= developed from= variants with their own articles=
}}

The Peyret-le Prieur seaplane was a low power, two seat biplane floatplane trainer flown in France in 1924. It did not reach production.

Design and development

Yves Le Prieur had identified a need for a simple, economical training aircraft on which pupils could master the behaviour of seaplanes and approached the designer and constructer Louis Peyret for a suitable aircraft. The outcome was the Peyret-Le Prieur seaplane.[2]

It was a single bay biplane, with rectangular plan wings mounted without stagger and braced by two pairs of parallel, vertical interplane struts and bracing wires, with a large interplane gap of {{convert|1.90|m|ftin|abbr=on}}. The wings were wooden, two-spar, two-part structures, with spruce leading edges. Broad, full-span ailerons on upper and lower wings were externally connected.

The seaplane had a rectangular section fuselage, built around four longerons and plywood covered. It was widest under the wing leading edge, where on each side a vertical cabane strut joined the upper longeron to the forward spar, and where pupil and tutor sat side-by-side in an open cockpit. The short nose ahead of them remained wide and the engine, unusually, was mounted off-set to port. Initially a {{convert|16|hp|kW|abbr=on|order=flip}} four-cylinder inline Sergant A was used, its radiator mounted midway up the portside cabane strut. At the rear the large area empennage was conventional, with a large span, rectangular plan all-moving tail mounted on top of the fuselage. Its triangular fin carried a roughly rhomboidal rudder which reached down to the keel through an elevator cut-out.

The seaplane had simple, rectangular cross-section floats. The flat undersides curved up towards the nose, reaching just beyond the propeller and the aft ends were under the ailerons. There was no step. Each float was attached with four aluminium tube struts, two leaning inwards to the lower fuselage longeron and two outwards to the wing spars. They were constructed of wood, with ash frames and mahogany plywood covering. The tail was protected with a cylindrical float of the same construction, attached longitudinally under the fin.

Fitted with the Sergant engine, the seaplane began tests on Lake Annecy in the summer of 1924 but it was unable to reach water speeds fast enough to unstick. In response a {{convert|45|hp|kW|abbr=on|order=flip}} Anzani 6 radial engine was substituted,[2] again mounted off-set.[7] With this, the seaplane left the water easily on its first flight on 24 August 1924.[8] Further tests showed that about {{convert|25|hp|kW|abbr=on|order=flip}} was required for take-off, though once in the air, {{convert|15-20|hp|kW|abbr=on|order=flip}} was enough.[2] By mid-September nineteen flights had been made, some lasting about 30 minutes, and a passenger had been carried. The seaplane then returned to Paris, where it was fitted with a wheeled undercarriage for further tests,[7] though by January 1925 it was flying from water again, at Pecq.[11]

By September 1924 the aircraft was judged a success and a second was under construction. Le Prieur had plans for a floatplane flying school at Annecy.[7] It is not known if the second machine was completed or the school set up.

Specifications (Sergant engine)

{{Aircraft specs
|ref=Les Ailes, August 1924
|prime units?=met


|genhide=
|crew=One tutor, one student
|length m=6.96
|length note=
|span m=10.50
|span note=
|height ft=
|height in=
|height note=
|wing area sqm=37.70
|wing area note=
|aspect ratio=
|airfoil=Göttingen 358
|empty weight kg=255
|empty weight note=
|gross weight kg=340
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|15|l|Impgal USgal|abbr=on}}
|more general=


|eng1 number=1
|eng1 name=Sergant A
|eng1 type=4-cylinder inline engine, geared down 1: 2.5
|eng1 hp=16
|eng1 note=at 3,350 rpm
|power original=
|prop blade number=2
|prop name=
|prop dia m=1.95
|prop dia note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=55-60
|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=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=3 hr
|ceiling m=1,500-2,000
|ceiling note= absolute
|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=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
}}

References

1. ^{{cite journal |last=Serryer |first=J. |date=28 August 1924|title=M. Le Prieur a volé son hydravion...|journal=Les Ailes|issue=167 |pages=2|url=http://gallica.bnf.fr/ark:/12148/bpt6k96073919/f2 }}
2. ^{{cite journal |last=Serryer |first=J. |date=18 September 1924|title=Les expériences de M. Le Prieur|journal=Les Ailes|issue=170 |pages=2|url=http://gallica.bnf.fr/ark:/12148/bpt6k6556116v/f2 }}
3. ^{{cite journal |date=15 January 1925|title=Nouvaux essais de l'hydravion Le Prieur|journal=Les Ailes|issue=187 |pages=2|url=http://gallica.bnf.fr/ark:/12148/bpt6k9607238k/f2}}
4. ^{{cite journal |last= |first= |authorlink= |date=15 January 1925 |title=M. LOUIS PEYRET |journal= Flight|volume=XVI |issue=36 |pages=554 |url= https://www.flightglobal.com/pdfarchive/view/1924/1924%20-%200554.html }}
[1][2][3][4]
}}{{Peyret aircraft}}

6 : Floatplanes|Trainer aircraft|Peyret aircraft|Biplanes|Single-engined tractor aircraft|Aircraft first flown in 1924

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/13 15:23:59