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词条 Gabriel P 6
释义

  1. Design and development

  2. Variants

  3. Specifications (P 6)

  4. References

name=Gabriel P 6 image= caption=

}}{{Infobox Aircraft Type

type=Training aircraft national origin=Poland manufacturer=Pawel and Jan Gabriel designer= Pawel Gabriel first flight=late May 1924 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Gabriel P 6 was a Polish training aircraft and the P 7 a tourer. The difference between them was the wing configuration, chosen to optimise their speed range for their role, so the P 6 was a biplane and the P 7 a parasol wing aircraft.

Design and development

After their first powered design, the single seat P 5, the Gabriel brothers considered the different requirements of two seat trainers and tourers. Both needed to handle well, ideally with similar characteristics, but the trainer required lower landing speeds and the tourer higher cruise speeds. They decided that economical solutions would share engines, fuselages, landing gears and wings but that the trainer should be a biplane with a cantilever lower wing and the tourer, without the lower wing, a parasol wing monoplane. The same airframe was flown in both the biplane (P 6) and parasol (P 7) configurations. Like the Gabriel P 5, the new aircraft was strongly influenced by the Fokker D.VII.

The P 6 was an all wood aircraft. Both of its wings were tapered in plan and were built around two spars with plywood covering. The upper wing was mounted over the fuselage by a cabane of inverted V-struts from the upper fuselage and braced on each side with a parallel pair of struts from the spars to the lower longeron. The lower wing was attached to the lower longerons.

The trainer was powered by a {{convert|65-70|hp|kW|abbr=on|order=flip}} four cylinder, water-cooled inline Mercedes engine.[4] The forward part of its rectangular section fuselage was covered with aluminium sheet and the rest with plywood. There were two cockpits in tandem, equipped with dual control though with flight instruments only in the rear seat. Its empennage was externally braced, with ply-covered fin and tailplane carrying fabric covered control surfaces.

Its fixed landing gear, with a track of {{convert|1.6|m|ftin|abbr=on}}, was of the tailskid type, with mainwheels on a single axle held via rubber ring shock absorbers on V-struts from the lower longerons.

The Gabriel P 6, the first Polish designed two seat trainer, was flown for the first time in late May 1924, piloted by Jan Gabriel at Bydgoszcz. It was subsequently tested by pilots from the Bydgoszcz pilot's school, who reported that it handled well.

Later in 1924 the lower wing was removed, a straightforward alteration in the absence of interplane struts, and the aircraft was flown successfully as the Gabriel P 7. With only 63% of the P 6's wing area but slightly lighter the P 7 had both maximum and landing speeds that were {{convert|20|km/h|mph kn|abbr=on}} faster than the P 6.

The Polish aeronautical authorities showed no more interest in the P 6 and P 7 than they had in the P 5. No funding was gained and, although Pawel Gabriel had designed a new high wing, low power ultralight, the P 7 was the Gabriels' last aircraft to fly.

Variants

P 6
Biplane trainer.
P 7
Parasol wing tourer with P 6's lower wing discarded.

Specifications (P 6)

{{Aircraft specs
|ref=Cynk (1971) except where noted
|prime units?=met


|crew=One student, one instructor
|capacity=
|length m=5.8
|length note=
|span m=8.6
|span note=
|height m=2.1
|height note=[10]
|wing area sqm=16.5
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=480
|empty weight note=
|gross weight kg=720
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|120|l|Impgal USgal|abbr=on}}
|more general=


|eng1 number=1
|eng1 name=Mercedes
|eng1 type=4-cylinder, water-cooled inline
|eng1 hp=65-70
|eng1 note=
|more power=
|prop blade number=2
|prop name=Gabriel, wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=175
|max speed note=
|cruise speed kmh=150
|cruise speed note=[10]
|stall speed kmh=60
|stall speed note=[10]
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=1100
|range note=[10]
|endurance=
|ceiling m=3000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=2.6
|climb rate note=[10]
|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=
|more performance=

  • Landing speed: {{convert|60|km/h|mph kn|abbr=on}}

}}

References

1. ^{{cite book |title= Jane's All the World's Aircraft 1913|last= Jane |first= Fred T. |coauthors= |edition= |year=1969|publisher= David & Charles|location= London|isbn=0 7153 4388 2 |page=9c}}
2. ^{{cite web |url=http://www.samolotypolskie.pl/samoloty/1070/126/Gabriel-P-VI-Gabriel-P-VII-Gabriel-P-VIII2|title=Gabriel P-VI, Gabriel P-VII, Gabriel P-VIII, 1924 |access-date=22 December 2017}}
[1][2]
}}

4 : Single-engined tractor aircraft|Biplanes|Parasol-wing aircraft|Polish sport aircraft 1920–1929

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