Focke-Wulf GL 18
Focke-Wulf GL 18 | |
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Focke-Wulf GL 18 "Helgoland" ( D-967 , W.Nr. 28) from Luft Hansa |
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Type: | Experimental and commercial aircraft |
Design country: | |
Manufacturer: | |
First flight: |
August 9, 1926 |
Number of pieces: |
3 |
The Focke-Wulf GL 18 is a German airliner from the 1920s.
history
The GL 18 was the second model developed by Focke-Wulf after the company was founded in 1924. The contract to build a twin-engine aircraft was placed by Junkers in 1925 , who in turn received it from the Turkish government, but for various reasons could not perform. The pattern was intended to be used for experimentation in order to research the flow behavior of the tail unit in multi-engine aircraft in various flight conditions. The motors of GL 18 should therefore be kept adjustable to the longitudinal axis in order to make the flow angle changeable.
Henrich Focke took over the fuselage of the A 16 for the construction and equipped it with an enlarged tail unit with horn compensation and a wing with a larger span. Two air-cooled L-1-a motors from Junkers were used as propulsion , which were placed under the wings. When the GL 18 flew in, which took place in 1925, several problems arose. When the engine power was reduced, there was a stall in the rear of the engine and the resulting top-heaviness with the associated sudden loss of altitude. The cause of the problem was identified and eliminated from the shape of the engine cowling. However, the examinations had taken a long time, so that although the test results were handed over to Junkers on November 25, 1925, together with a price proposal of RM 36,000, the official acceptance did not take place until August 10 and 11, 1926 at the DVL in Adlershof took place. The flights were also restricted by difficulties with the engines developed in 1925. Regardless of this, the model was successfully demonstrated and was adopted by Junkers as the GL 18 a .
Focke-Wulf then built another aircraft called the GL 18 a . An A 16 a with a lengthened and widened fuselage served as the starting model, so that the number of passengers increased from three to four. Two Sh-11 motors from Siemens served as the drive. The last to appear in 1926 was the enlarged GL 18 c with a closed cockpit, twin controls and more powerful Sh 12 engines . It was used by DVS with the registration number D – 1097 . As a further development, the GL 22 appeared in 1927 .
Technical specifications
The GL 18 data were flown by Focke-Wulf in 1925 and handed over to Junkers together with the cost estimate on November 5, 1925. The data flown with the aircraft subsequently designated by Junkers as the GL 18 a can be found in the second column.
Parameter | GL 18 | GL 18 a (Junkers) |
GL 18 a (Focke-Wulf) |
GL 18 c |
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crew | 1 | |||
Passengers | 3 | 4th | ||
length | 8.50 m | 9.10 m | ||
span | 16.00 m | |||
height | 2.30 m | 2.60 m | ||
Wing area | 32.00 m² | 34.50 m | 32.00 m² | |
Wing extension | 8.00 | 7.40 | 8.00 | |
Preparation mass | 890 kg | 915 kg | 1100 kg | |
Payload | 296 kg | 220 kg | 290 kg | |
Payload | 460 kg | 496 kg | 550 kg | |
Takeoff mass | 1350 kg | 1411 kg | 1650 kg | |
Wing loading | 42.18 kg / m² | 44.09 kg / m² | 47.43 kg / m² | 51.56 kg / m² |
Engines | two Junkers L 1 a | two Siemens & Halske Sh 11 | two Siemens & Halske Sh 12 | |
power | 55 kW (75 PS) each | 60 kW (82 PS) each | 79 kW (107 PS) each | |
Top speed close to the ground |
150 km / h | 160 km / h | 140 km / h | |
Cruising speed close to the ground |
135 km / h | 145 km / h | 127 km / h | |
Rate of climb | 1.50 m / s | 1.40 m / s | 1.85 m / s | 2.20 m / s |
Service ceiling | 3000 m | 4000 m | 5000 m | |
Range | 400 km | 580 km | 380 km | |
maximum flight time | 3 h | 4 h | 3 h | |
Take-off / landing runway | 160 m / 100 m | 170 m / 150 m | 160 m / 100 m |
literature
- Wolfgang Wagner: Der Deutschen Luftverkehr - The Pioneering Years 1919–1925 (= Die deutsche Luftfahrt . Volume 11 ). Bernard & Graefe, Koblenz 1987, ISBN 3-7637-5274-9 , pp. 185-189 .
Web links
- Photos and dates. Retrieved January 8, 2016 .
Remarks
- ↑ The official first flight date, which refers to the start of the acceptance flights at the DVL in Adlershof. Unofficially, however, the GL 18 was flown in at Focke-Wulf in Bremen the year before.