Английская Википедия:Continental O-520
Шаблон:Short description Шаблон:Refimprove
The Continental O-520 is a six-cylinder, horizontally opposed aircraft engine produced by Teledyne Continental Motors. First run in 1963 as a development of the IO-346, it has been produced in versions incorporating fuel injection (IO-520), turbo-charging (TSIO-520), and gearing (GTSIO-520).
Design and development
The IO-520 series engines normally produce Шаблон:Convert and are used in numerous aircraft such as certain models of the Bellanca Viking 300 and Super Viking, the Beech Bonanza and Baron, and Cessna 185- 206-, 210-, 310-, and 400-series aircraft. The IO-520 remained in production in 2019.[1]
The turbocharged GTSIO-520's most common applications are the twin-engine Cessna 404 and 421, where it is rated at Шаблон:Convert. The 'G' prefix indicated the incorporation of propeller reduction gearing.
Variants
IO-520
- IO-520-A
- 285 hp (213 kW)[2] (Meyers 200)
- IO-520-B
- 285 hp (213 kW)[2] (Beech 35-C33A Debonair, s35, model 36 Bonanza)
- IO-520-BA
- 285 hp (213 kW)[2]
- IO-520-BB
- 285 hp (213 kW)[2]
- IO-520-C
- 285 hp (213 kW)[2]
- IO-520-CB
- 285 hp (213 kW)[2]
- IO-520-D
- 300 hp (224 kW)[2]
- IO-520-E
- 300 hp (224 kW)[2]
- IO-520-F
- 300 hp (224 kW)[2]
- IO-520-J
- 285 hp (213 kW)[2]
- IO-520-K
- 300 hp (224 kW)[2] (Bellanca Viking)
- IO-520-L
- 300 hp (224 kW)[2]
- IO-520-M
- 285 hp (213 kW)[2]
- IO-520-MB
- 285 hp (213 kW)[2]
- IO-520-N
- 300 hp (224 kW)[2]
- IO-520-NB
- 300 hp (224 kW)[2]
- L/IO-520-P
- Шаблон:Convert[2]
TSIO-520
- TSIO-520-A
- Шаблон:Convert[3]
- TSIO-520-AE
- Шаблон:Convert[3]
- LTSIO-520-AE
- Шаблон:Convert[3]
- TSIO-520-AF
- Шаблон:Convert[3]
- TSIO-520-B
- 285 hp (213 kW)[3]
- TSIO-520-BB
- 285 hp (213 kW)[3]
- TSIO-520-BE
- Шаблон:Convert[3]
- TSIO-520-C
- Шаблон:Convert[3]
- TSIO-520-CE
- Шаблон:Convert[3]
- TSIO-520-D
- 285 hp (213 kW)[3]
- TSIO-520-DB
- 285 hp (213 kW)[3]
- TSIO-520-E
- Шаблон:Convert[3]
- TSIO-520-EB
- Шаблон:Convert[3]
- TSIO-520-G
- 285 hp (213 kW)[3]
- TSIO-520-H
- Шаблон:Convert[3]
- TSIO-520-J
- 310 hp (230 kW)[3]
- TSIO-520-JB
- 310 hp (230 kW)[3]
- TSIO-520-K
- 285 hp (213 kW)[3]
- TSIO-520-KB
- 285 hp (213 kW)[3]
- TSIO-520-L
- 310 hp (230 kW)[3]
- TSIO-520-LB
- 310 hp (230 kW)[3]
- TSIO-520-M
- 285 hp (213 kW)[3]
- TSIO-520-N
- 310 hp (230 kW)[3]
- TSIO-520-NB
- 310 hp (230 kW)[3]
- TSIO-520-P
- 310 hp (230 kW)[3]
- TSIO-520-R
- 310 hp (230 kW)[3]
- TSIO-520-T
- 310 hp (230 kW)[3]
- TSIO-520-U
- Шаблон:Convert[3]
- TSIO-520-UB
- Шаблон:Convert[3]
- TSIO-520-VB
- Шаблон:Convert[3]
- TSIO-520-WB
- Шаблон:Convert[3]
GTSIO-520
- GTSIO-520-C
- Шаблон:Convert[4]
- GTSIO-520-D
- 375 hp (280 kW)[4] (Cessna 421)
- GTSIO-520-F
- Шаблон:Convert[4]
- GTSIO-520-H
- 375 hp (280 kW)[4] (Cessna 421B)
- GTSIO-520-K
- Шаблон:Convert[4]
- GTSIO-520-L
- 375 hp (280 kW)[4] (Cessna 421C)
- GTSIO-520-M
- 375 hp (280 kW)[4] (Cessna 404)
- GTSIO-520-N
- 375 hp (280 kW)[4] (Cessna 421C)
- GTSIO-520-S
- 375 hp (280 kW)[4] (Tecnam P2012 Traveller)
Applications
Specifications (GTSIO-520-D)
See also
References
External links
Шаблон:Commons category inline
Шаблон:Continental aeroengines
- ↑ Шаблон:Cite web
- ↑ 2,00 2,01 2,02 2,03 2,04 2,05 2,06 2,07 2,08 2,09 2,10 2,11 2,12 2,13 2,14 2,15 2,16 Шаблон:Cite web
- ↑ 3,00 3,01 3,02 3,03 3,04 3,05 3,06 3,07 3,08 3,09 3,10 3,11 3,12 3,13 3,14 3,15 3,16 3,17 3,18 3,19 3,20 3,21 3,22 3,23 3,24 3,25 3,26 3,27 3,28 3,29 3,30 Шаблон:Cite web
- ↑ 4,0 4,1 4,2 4,3 4,4 4,5 4,6 4,7 4,8 Шаблон:Cite web