Potez IX: Difference between revisions
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{|{{Infobox Aircraft Begin |
{|{{Infobox Aircraft Begin |
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| name= |
| name=Potez IX |
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| image=Potez IX L'Aéronautique December 1922.jpg |
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| image= |
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| caption= |
| caption= |
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}}{{Infobox Aircraft Type |
}}{{Infobox Aircraft Type |
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| type= |
| type=Airliner |
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| national origin= |
| national origin=France |
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| manufacturer= |
| manufacturer=[[Potez]] |
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| designer= |
| designer= |
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| first flight= |
| first flight=1920 |
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| introduced= |
| introduced= |
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| retired= |
| retired= |
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| status= |
| status= |
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| primary user= |
| primary user= |
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| number built= |
| number built=30 |
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| developed from= |
| developed from= [[SEA IV]] |
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| variants with their own articles= |
| variants with their own articles= |
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}} |
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The '''Potez IX''' was an early airliner produced in France in the 1920s, a further development of the [[SEA IV]] that [[Henry Potez]] had co-designed during the First World War.<ref name="JEA">Taylor 1989, p.747</ref><ref name="IEA">''The Illustrated Encyclopedia of Aircraft'', p.2760</ref> |
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==Design and development== |
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The design mated an entirely new fuselage to the wing and tail structures of the earlier military aircraft.<ref name="JEA"/><ref name="IEA"/><ref name="Paris 841">"The Paris Aero Show 1921" 22 December 1921, p.841</ref> This fuselage was very deep, nearly filling the interplane gap, and carried within it a fully enclosed cabin with seating for four passengers.<ref name="JEA"/><ref name="IEA"/><ref name="Paris 841"/> The nose area was carefully streamlined<ref name="IEA"/> with curved aluminium,<ref name="Paris 764">"The Paris Aero Show 1921" 17 November 1921, p. [https://www.flightglobal.com/pdfarchive/view/1921/1921%20-%200764.html 764]</ref> but other aspects of the construction were conventional for the day; wooden structures skinned in plywood (the passenger cabin) or fabric (the rest of the aircraft).<ref name="Paris 842">"The Paris Aero Show 1921" 22 December 1921, p.842</ref> The pilot sat in an open cockpit aft of the cabin.<ref name="IEA"/><ref name="Paris 842"/> |
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The prototype flew in 1920,<ref name="stdp176">Stroud 1966, p. 176</ref> and was followed by around thirty production examples that differed from it in having a larger tail fin and rudder.<ref name="IEA"/> The [[Compagnie générale transaérienne]] operated Potez IXs on cross-channel air services between Paris and London.<ref name="stdp176"/> The [[Compagnie Franco-Roumaine de Navigation Aérienne]] flew these<ref name="Paris 842"/> on routes linking Paris to [[Warsaw]] via [[Strasbourg]] and [[Prague]], and from Paris to [[Budapest]] via Strasbourg and [[Vienna]], later extending its services to [[Bucharest]] and [[Constantinople]].<ref name="stdp176"/> Franco-Roumaine, and its successor airline CIDNA operated the Potez IX until 1928.<ref name="JEA"/><ref name="stdp177">Stroud 1966, p. 177</ref> |
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The '''Potez IX S''', a one-off modified version with wings of larger area,<ref name="IEA"/> flew in the Grand Prix de l'Aéro Club de France in June 1921 with [[Gustave Douchy]] at the controls.<ref name="Grand Prix">"The French Aero Club Grand Prix", p.430</ref> Douchy was disqualified in the third stage of the competition.<ref name="Grand Prix"/> |
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==Specifications |
==Specifications== |
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[[File:Potez_IX_3-view_Les_Ailes_December_29,1921.png|thumb|Potez IX 3-view Drawing from Les Ailes December 29,1921]] |
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{{aerospecs |
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{{Aircraft specs |
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|ref=<!-- reference --> |
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|ref=<!-- reference -->"The Paris Aero Show 1921" 22 December 1921, p.842 |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others. You MUST include one or the other here, or no specifications will show --> |
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|prime units? = met |
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|crew= |
|crew=One pilot |
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|capacity= |
|capacity=4 passengers |
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|length m= |
|length m=9.80 |
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|length ft= |
|length ft=32 |
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|length in= |
|length in=2 |
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|span m= |
|span m=14.00 |
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|span ft= |
|span ft=46 |
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|span in= |
|span in=0 |
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|height m=3.12 |
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|swept m=<!-- swing-wings --> |
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|height ft=10 |
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|swept ft=<!-- swing-wings --> |
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|height in=3 |
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|swept in=<!-- swing-wings --> |
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|wing area sqm=46.0 |
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|rot number=<!-- helicopters --> |
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|wing area sqft=495 |
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|rot dia m=<!-- helicopters --> |
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|empty weight kg=1,250 |
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|rot dia ft=<!-- helicopters --> |
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|empty weight lb=2,750 |
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|rot dia in=<!-- helicopters --> |
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|gross weight kg=2,050 |
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|dia m=<!-- airships etc --> |
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|gross weight lb=2,511 |
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|dia ft=<!-- airships etc --> |
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|eng1 number=1 |
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|dia in=<!-- airships etc --> |
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|eng1 name=[[Lorraine-Dietrich 12Da]] |
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|width m=<!-- if applicable --> |
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|eng1 kw=<!-- prop engines -->280 |
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|eng1 hp=<!-- prop engines -->370 |
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|max speed kmh=200 |
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|height m= |
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|max speed mph=125 |
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|height ft= |
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|ceiling m=6,100 |
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|height in= |
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|ceiling ft=20,000 |
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|wing area sqm= |
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|climb rate ms=4.2 |
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|wing area sqft= |
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|climb rate ftmin=820 |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|aspect ratio=<!-- sailplanes --> |
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|wing profile=<!-- sailplanes --> |
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|gross weight lb= |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|eng1 number= |
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|eng1 type= |
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|eng1 kw=<!-- prop engines --> |
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|eng1 hp=<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 kn-ab=<!-- afterburners --> |
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|eng1 lbf-ab=<!-- afterburners --> |
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|max speed kmh= |
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|max speed mph= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh=<!-- if max speed unknown --> |
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|cruise speed mph=<!-- if max speed unknown --> |
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|stall speed kmh=<!-- aerobatic and STOL aircraft --> |
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|stall speed mph=<!-- aerobatic and STOL aircraft --> |
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|range km= |
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|endurance h=<!-- if range unknown --> |
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|endurance min=<!-- if range unknown --> |
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|ceiling m= |
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|ceiling ft= |
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|g limits=<!-- aerobatic aircraft --> |
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|roll rate=<!-- aerobatic aircraft --> |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
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|climb rate ftmin= |
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|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
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|armament1= |
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|armament5= |
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}} |
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{{aircontent |
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==References== |
==References== |
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{{commons category|Potez IX}} |
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* {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London |pages= }} |
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*{{cite magazine |last=Coroller|first=Jean-Louis|title=Les premièrs avions Henry Potez (première partie)|magazine=Avions: Toute l'aéronautique et son histoire |date=September 1998 |issue=66|pages=8–14 |trans-title=The First Aircraft of Henry Potez|language=French |issn=1243-8650}} |
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* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= }} |
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* {{cite magazine |title=The French Aero Club Grand Prix |magazine=[[Flight International|Flight]] |date=23 June 1921 |url=https://archive.org/details/sim_flight-international_1921-06-23_13_25/page/430/mode/2up |pages=430 |access-date=2021-10-29}} |
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* {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages= }} |
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* {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London }} |
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* {{cite book| last=Stroud |first= John |title= European Transport Aircraft since 1910 |year=1966 |publisher=Putnam |location= London}} |
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<!-- ==External links== --> |
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* {{cite magazine |title=The Paris Aero Show 1921 |magazine=[[Flight International|Flight]] |date=17 November 1921 |url=https://archive.org/details/Flight_International_Magazine_1921-11-17-pdf/page/n11/mode/2up |pages=758–765|access-date=2021-10-29}} |
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* {{cite magazine |title=The Paris Aero Show 1921 |journal=[[Flight International|Flight]] |date=22 December 1921 |url=https://archive.org/details/Flight_International_Magazine_1921-12-22-pdf/page/n3/mode/2up |pages=839–842|access-date=2021-10-29}} |
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* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |isbn= 0-7106-0710-5 }} |
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*{{cite journal |last1=Warner|first1=Edward P.|title=Les avions de ligne au banc d'essai en 1921|journal=Le Fana de l'Aviation |date=May 2008 |issue=462 |pages=44–55 |issn=0757-4169 |language=fr|trans-title=Airlines on the Test Bench in 1921}} |
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{{ |
{{Potez aircraft}} |
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[[Category: ]] |
[[Category:Potez aircraft|R09]] |
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[[Category:1920s French airliners]] |
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[[Category:Aircraft first flown in 1921]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Biplanes]] |
Latest revision as of 13:03, 30 August 2022
Potez IX | |
---|---|
Role | Airliner |
National origin | France |
Manufacturer | Potez |
First flight | 1920 |
Number built | 30 |
Developed from | SEA IV |
The Potez IX was an early airliner produced in France in the 1920s, a further development of the SEA IV that Henry Potez had co-designed during the First World War.[1][2]
Design and development[edit]
The design mated an entirely new fuselage to the wing and tail structures of the earlier military aircraft.[1][2][3] This fuselage was very deep, nearly filling the interplane gap, and carried within it a fully enclosed cabin with seating for four passengers.[1][2][3] The nose area was carefully streamlined[2] with curved aluminium,[4] but other aspects of the construction were conventional for the day; wooden structures skinned in plywood (the passenger cabin) or fabric (the rest of the aircraft).[5] The pilot sat in an open cockpit aft of the cabin.[2][5]
The prototype flew in 1920,[6] and was followed by around thirty production examples that differed from it in having a larger tail fin and rudder.[2] The Compagnie générale transaérienne operated Potez IXs on cross-channel air services between Paris and London.[6] The Compagnie Franco-Roumaine de Navigation Aérienne flew these[5] on routes linking Paris to Warsaw via Strasbourg and Prague, and from Paris to Budapest via Strasbourg and Vienna, later extending its services to Bucharest and Constantinople.[6] Franco-Roumaine, and its successor airline CIDNA operated the Potez IX until 1928.[1][7]
The Potez IX S, a one-off modified version with wings of larger area,[2] flew in the Grand Prix de l'Aéro Club de France in June 1921 with Gustave Douchy at the controls.[8] Douchy was disqualified in the third stage of the competition.[8]
Specifications[edit]
Data from "The Paris Aero Show 1921" 22 December 1921, p.842
General characteristics
- Crew: One pilot
- Capacity: 4 passengers
- Length: 9.80 m (32 ft 2 in)
- Wingspan: 14.00 m (46 ft 0 in)
- Height: 3.12 m (10 ft 3 in)
- Wing area: 46.0 m2 (495 sq ft)
- Empty weight: 1,250 kg (2,750 lb)
- Gross weight: 2,050 kg (2,511 lb)
- Powerplant: 1 × Lorraine-Dietrich 12Da , 280 kW (370 hp)
Performance
- Maximum speed: 200 km/h (125 mph, 109 kn)
- Service ceiling: 6,100 m (20,000 ft)
- Rate of climb: 4.2 m/s (820 ft/min)
Notes[edit]
- ^ a b c d Taylor 1989, p.747
- ^ a b c d e f g The Illustrated Encyclopedia of Aircraft, p.2760
- ^ a b "The Paris Aero Show 1921" 22 December 1921, p.841
- ^ "The Paris Aero Show 1921" 17 November 1921, p. 764
- ^ a b c "The Paris Aero Show 1921" 22 December 1921, p.842
- ^ a b c Stroud 1966, p. 176
- ^ Stroud 1966, p. 177
- ^ a b "The French Aero Club Grand Prix", p.430
References[edit]
- Coroller, Jean-Louis (September 1998). "Les premièrs avions Henry Potez (première partie)" [The First Aircraft of Henry Potez]. Avions: Toute l'aéronautique et son histoire (in French). No. 66. pp. 8–14. ISSN 1243-8650.
- "The French Aero Club Grand Prix". Flight. 23 June 1921. p. 430. Retrieved 2021-10-29.
- The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing.
- Stroud, John (1966). European Transport Aircraft since 1910. London: Putnam.
- "The Paris Aero Show 1921". Flight. 17 November 1921. pp. 758–765. Retrieved 2021-10-29.
- "The Paris Aero Show 1921". Flight. 22 December 1921. pp. 839–842. Retrieved 2021-10-29.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. ISBN 0-7106-0710-5.
- Warner, Edward P. (May 2008). "Les avions de ligne au banc d'essai en 1921" [Airlines on the Test Bench in 1921]. Le Fana de l'Aviation (in French) (462): 44–55. ISSN 0757-4169.