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Feiro I

The 1923 Feiro I was the first Hungarian designed and built civil transport aircraft, modified in 1925 by an engine change into the Feiru Daru (Crane). Neither was a commercial success.

Feiro I
Role Four seat civil transport
National origin Hungary
Manufacturer Feigl and Rotter
Designer Lajos Rotter
First flight late 1923-early 1924
Number built 1
Developed into Feiro Daru

Design and development edit

The Feiro I was the first design of Lajos Rotter in his collaboration with the brothers Gyula and László Feigl.[1] It was also the first civil transport to be designed in Hungary, flying in the winter of 1923-4. It had four seats and was powered by a 120 hp (89 kW) Le Rhone 9J rotary engine, though it was intended that this would be replaced by Haake or Siemens-Halske radial engines of similar power in production aircraft.[2]

It was a high wing monoplane, with an aerodynamically thick (thickess/chord ratio 14%) Joukowski-Göttingen "tadpole shaped" airfoil over the whole span. The two piece, 3-ply covered wing was built around twin spruce flanged box spars with 3-ply webs. In plan it had constant chord and was unswept; the wingtips were angled and the short ailerons tapered slightly outboard. Each wing was braced to the fuselage with a parallel pair of airfoil section struts from the wing spars to the lower fuselage longerons.[2][3]

Behind the engine the fuselage was rectangular in cross-section, with four longerons and 3-ply covered. The Le Rhone rotary was partially enclosed within an open-bottomed engine cowling and was mounted on steel tube bearings. Aluminium sheet, rounded on the upper surface, covered the fuselage rearwards to the cabin. There were two firewalls between engine and cabin and the carburetter, gravity-fed fuel from a tank in the central wing, was placed in the ventilated space between them.[2]

The deep cabin of the Feiro I had two rows side-by-side seats; the front pair could both be equipped with flight controls or one of then could serve as a third passenger seat. Because the high engine fairing reached the underside of the wing leading edge, there was no central forward view from the controls; instead, there were deep openings on either side. Access to the cabin was via a port side door. Behind the cabin the fuselage tapered to the tail where a short, broad fin carried a deep rudder. The tailplane was also mounted on the fin, just above the fuselage so that it could be used to trim the aircraft by altering its angle of incidence. It had swept leading edges, square tips and carried elevators with a cut-out for rudder movement. The fixed tail surfaces were ply skinned and the control surfaces fabric covered.[2]

The Feiro I had a tailskid undercarriage with mainwheels 2 m (6 ft 7 in) apart and rubber sprung on a single axle, its ends supported by longitudinal V-struts and positioned laterally by a steel V-strut; all struts were from the lower fuselage longerons.[2][4]

The first flight was late in 1923 or in January 1924, though the exact date is not known. Some testing had been done by mid-February, establishing good handling and a take-off distance of around 46 m (150 ft) but detailed performance figures had yet to be established.[2] By March an estimated maximum speed of 160 km/h (99 mph) had been confirmed.[3] Feiro's resources were limited and they had difficulty obtaining some important raw materials, even in small quantities, receiving no public support for the Feiro I's development.[4] Hungary's manufacturers lost many of their material suppliers when the country's boundaries were shrunk by the Treaty of Trianon after the end of World War I.

Despite these problems, two years later and after their innovative high aspect ratio biplane trainer aircraft, the Feiro Dongó, Feiro flew a Feiro I production development, largely unchanged but with a more modern, 180 hp (134 kW) Hispano-Suiza 8A water-cooled V-8 engine in a revised nose which provided better forward visibility through a front-facing windscreen.[4] This was given the name Feiro Daru. Other differences between it and the Feiro I were the addition of about 2º of sweep to the wing, moving the center of pressure rearwards, and a revised tail similar in shape to that used on the Feiro Dongó, with a straight edged fin and deep, curved, balanced rudder. Its empty weight was increased by 70 kg (154 lb) but its useful load also increased by 30 kg (66 lb). It was faster, with a maximum speed increased by 10–20 km/h (6–12 mph), climbed to 1,000 m (3,281 ft) in 8 minutes and had a ceiling of 1,000 m (3,281 ft).[4] Despite the improvements the Daru still failed to find customers and only one was built; this may have originally been the sole Feiro I.

After these commercial failures with powered designs, Rotter became instead a successful glider pilot and designer. Flying his first such design, the 1933 Karakan, Rotter became Hungary's first "Silver C" glider pilot.[5]

Variants edit

 
Feiro Daru
Feiro I
1923 version with 120 hp (89 kW) Le Rhone 9J rotary engine.[2]
Feiro Daru
1925 version with 180 hp (134 kW) Hispano-Suiza 8A water-cooled V-8 engine, a slightly swept wing and revised vertical tail.

Specifications (Feiro I) edit

Data from Flight 14 February 1924, pp.86-7[2]

General characteristics

  • Crew: One pilot
  • Capacity: Three passengers
  • Length: 8.83 m (29 ft 0 in)
  • Wingspan: 14.25 m (46 ft 9 in)
  • Wing area: 26 m2 (280 sq ft)
  • Airfoil: Joukowski-Göttingen, thickness/chord ratio=14%[3]
  • Empty weight: 750 kg (1,653 lb)
  • Gross weight: 1,200 kg (2,646 lb)
  • Powerplant: 1 × Le Rhone 9J 9-cylinder rotary engine, 89 kW (120 hp)
  • Propellers: two-bladed

Performance

  • Maximum speed: 160 km/h (99 mph, 86 kn) [3]
  • Time to altitude: 6 min to1,000 m (3,300 ft)[6]
  • Take-off distance: 45 m (148 ft)[6]

References edit

  1. ^ "Hungarian Gliders 1933-2000". Retrieved 17 November 2012.
  2. ^ a b c d e f g h "The Feiro I Commercial Monoplane". Flight. Vol. XVI, no. 7. 14 February 1924. pp. 86–7.
  3. ^ a b c d "La vie aéronautique - un avion de transport hongrois". L'Aéronautique. 6 (68): 65. March 1924.
  4. ^ a b c d "L'Avion Feiro, type "Daru"". Les Ailes. 5 (230): 2. 12 November 1925.
  5. ^ Simons, Martin (2006). Sailplanes 1920-1945 (2nd revised ed.). Königswinter: EQIP Werbung & Verlag GmbH. pp. 192–4. ISBN 3-9806773-4-6.
  6. ^ a b "Le monoplan Feiro, type "Daru"". Les Ailes. 4 (1400): 2. 21 February 1924.

feiro, 1923, first, hungarian, designed, built, civil, transport, aircraft, modified, 1925, engine, change, into, feiru, daru, crane, neither, commercial, success, role, four, seat, civil, transport, national, origin, hungary, manufacturer, feigl, rotter, desi. The 1923 Feiro I was the first Hungarian designed and built civil transport aircraft modified in 1925 by an engine change into the Feiru Daru Crane Neither was a commercial success Feiro I Role Four seat civil transport National origin Hungary Manufacturer Feigl and Rotter Designer Lajos Rotter First flight late 1923 early 1924 Number built 1 Developed into Feiro Daru Contents 1 Design and development 2 Variants 3 Specifications Feiro I 4 ReferencesDesign and development editThe Feiro I was the first design of Lajos Rotter in his collaboration with the brothers Gyula and Laszlo Feigl 1 It was also the first civil transport to be designed in Hungary flying in the winter of 1923 4 It had four seats and was powered by a 120 hp 89 kW Le Rhone 9J rotary engine though it was intended that this would be replaced by Haake or Siemens Halske radial engines of similar power in production aircraft 2 It was a high wing monoplane with an aerodynamically thick thickess chord ratio 14 Joukowski Gottingen tadpole shaped airfoil over the whole span The two piece 3 ply covered wing was built around twin spruce flanged box spars with 3 ply webs In plan it had constant chord and was unswept the wingtips were angled and the short ailerons tapered slightly outboard Each wing was braced to the fuselage with a parallel pair of airfoil section struts from the wing spars to the lower fuselage longerons 2 3 Behind the engine the fuselage was rectangular in cross section with four longerons and 3 ply covered The Le Rhone rotary was partially enclosed within an open bottomed engine cowling and was mounted on steel tube bearings Aluminium sheet rounded on the upper surface covered the fuselage rearwards to the cabin There were two firewalls between engine and cabin and the carburetter gravity fed fuel from a tank in the central wing was placed in the ventilated space between them 2 The deep cabin of the Feiro I had two rows side by side seats the front pair could both be equipped with flight controls or one of then could serve as a third passenger seat Because the high engine fairing reached the underside of the wing leading edge there was no central forward view from the controls instead there were deep openings on either side Access to the cabin was via a port side door Behind the cabin the fuselage tapered to the tail where a short broad fin carried a deep rudder The tailplane was also mounted on the fin just above the fuselage so that it could be used to trim the aircraft by altering its angle of incidence It had swept leading edges square tips and carried elevators with a cut out for rudder movement The fixed tail surfaces were ply skinned and the control surfaces fabric covered 2 The Feiro I had a tailskid undercarriage with mainwheels 2 m 6 ft 7 in apart and rubber sprung on a single axle its ends supported by longitudinal V struts and positioned laterally by a steel V strut all struts were from the lower fuselage longerons 2 4 The first flight was late in 1923 or in January 1924 though the exact date is not known Some testing had been done by mid February establishing good handling and a take off distance of around 46 m 150 ft but detailed performance figures had yet to be established 2 By March an estimated maximum speed of 160 km h 99 mph had been confirmed 3 Feiro s resources were limited and they had difficulty obtaining some important raw materials even in small quantities receiving no public support for the Feiro I s development 4 Hungary s manufacturers lost many of their material suppliers when the country s boundaries were shrunk by the Treaty of Trianon after the end of World War I Despite these problems two years later and after their innovative high aspect ratio biplane trainer aircraft the Feiro Dongo Feiro flew a Feiro I production development largely unchanged but with a more modern 180 hp 134 kW Hispano Suiza 8A water cooled V 8 engine in a revised nose which provided better forward visibility through a front facing windscreen 4 This was given the name Feiro Daru Other differences between it and the Feiro I were the addition of about 2º of sweep to the wing moving the center of pressure rearwards and a revised tail similar in shape to that used on the Feiro Dongo with a straight edged fin and deep curved balanced rudder Its empty weight was increased by 70 kg 154 lb but its useful load also increased by 30 kg 66 lb It was faster with a maximum speed increased by 10 20 km h 6 12 mph climbed to 1 000 m 3 281 ft in 8 minutes and had a ceiling of 1 000 m 3 281 ft 4 Despite the improvements the Daru still failed to find customers and only one was built this may have originally been the sole Feiro I After these commercial failures with powered designs Rotter became instead a successful glider pilot and designer Flying his first such design the 1933 Karakan Rotter became Hungary s first Silver C glider pilot 5 Variants edit nbsp Feiro Daru Feiro I 1923 version with 120 hp 89 kW Le Rhone 9J rotary engine 2 Feiro Daru 1925 version with 180 hp 134 kW Hispano Suiza 8A water cooled V 8 engine a slightly swept wing and revised vertical tail Specifications Feiro I editData from Flight 14 February 1924 pp 86 7 2 General characteristicsCrew One pilot Capacity Three passengers Length 8 83 m 29 ft 0 in Wingspan 14 25 m 46 ft 9 in Wing area 26 m2 280 sq ft Airfoil Joukowski Gottingen thickness chord ratio 14 3 Empty weight 750 kg 1 653 lb Gross weight 1 200 kg 2 646 lb Powerplant 1 Le Rhone 9J 9 cylinder rotary engine 89 kW 120 hp Propellers two bladed Performance Maximum speed 160 km h 99 mph 86 kn 3 Time to altitude 6 min to1 000 m 3 300 ft 6 Take off distance 45 m 148 ft 6 References edit Hungarian Gliders 1933 2000 Retrieved 17 November 2012 a b c d e f g h The Feiro I Commercial Monoplane Flight Vol XVI no 7 14 February 1924 pp 86 7 a b c d La vie aeronautique un avion de transport hongrois L Aeronautique 6 68 65 March 1924 a b c d L Avion Feiro type Daru Les Ailes 5 230 2 12 November 1925 Simons Martin 2006 Sailplanes 1920 1945 2nd revised ed Konigswinter EQIP Werbung amp Verlag GmbH pp 192 4 ISBN 3 9806773 4 6 a b Le monoplan Feiro type Daru Les Ailes 4 1400 2 21 February 1924 Retrieved from https en wikipedia org w index php title Feiro I amp oldid 1082315844, wikipedia, wiki, book, books, library,

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