Kowasaki TF2: Difference between revisions
Jump to navigation
Jump to search
(Created page with "{{wip}} ==Specifications (TF2-20)== {{jetspecs |ref= |type= Afterburning {{wpl|turbofan}} |length= |diameter= |weight= |compressor= |combustion= |turbine= |fueltype= |o...") |
No edit summary |
||
| (10 intermediate revisions by the same user not shown) | |||
| Line 1: | Line 1: | ||
{{wip}} | {{wip}} | ||
{|{{Infobox aircraft begin | |||
|name= TF2 | |||
|image= File:Rd-93.jpg | |||
|caption= A TF2-10 engine on display. | |||
}}{{Infobox aircraft engine | |||
|type= {{wpl|Turbofan}} | |||
|manufacturer= [[Kowasaki Heavy Industries]] | |||
|national origin= [[Chilokver]] | |||
|first run= | |||
|major applications= [[Shangtian F-8 Eagle]]<br>[[Nakajima CF-05 Goshawk]] | |||
|produced= | |||
|number built= | |||
|program cost= | |||
|unit cost= | |||
|developed from= | |||
|variants with their own articles= | |||
}} | |||
|} | |||
The '''Kowasaki TF2''' is a series of afterburning {{wpl|Turbofan|turbofan}} jet engines developed by [[Kowasaki Heavy Industries]]. | |||
==Variants== | |||
;TF2-10: Original variant of the TF2 developed for the [[Shangtian F-8 Eagle]]. | |||
==Applications== | |||
* [[Shangtian F-8 Eagle]] | |||
* [[Nakajima CF-05 Goshawk]] | |||
==Specifications (TF2-20)== | ==Specifications (TF2-20)== | ||
| Line 5: | Line 32: | ||
|ref= | |ref= | ||
|type= Afterburning {{wpl|turbofan}} | |type= Afterburning {{wpl|turbofan}} | ||
|length= | |length= {{convert|4145|mm|in|2|abbr=on}} | ||
|diameter= | |diameter= {{convert|1020|mm|in|2|abbr=on}} | ||
|weight= | |weight= {{convert|1135|kg|lb}} | ||
|compressor= | |compressor= {{wpl|Axial compressor}} with 4 low-pressure and 8 high-pressure stages | ||
|combustion= | |combustion= {{wpl|Combustor#Annular|Annular}} | ||
|turbine= | |turbine= 1 low-pressure and 1 high-pressure stage | ||
|fueltype= | |fueltype= | ||
|oilsystem= | |oilsystem= | ||
|power= | |power= | ||
|thrust= | |thrust= {{convert|56.75|kN}} dry; {{convert|86.37|kN}} with afterburner | ||
|compression= | |compression= 24:1 | ||
|bypass= | |bypass= 0.57:1 | ||
|aircon= | |aircon= | ||
|turbinetemp= | |turbinetemp= {{convert|1,377|°C|°F}} | ||
|fuelcon= | |fuelcon= | ||
|specfuelcon= | |specfuelcon= | ||
|power/weight= | |power/weight= | ||
|thrust/weight= | |thrust/weight= 5.1 (dry), 7.8 (afterburning) | ||
}} | }} | ||
==See also== | |||
===Related development=== | |||
===Comparable engines=== | |||
[[category:Chilokver]] | [[category:Chilokver]] | ||
Latest revision as of 04:37, 6 October 2019
 | This article is incomplete because it is pending further input from participants, or it is a work-in-progress by one author. Please comment on this article's talk page to share your input, comments and questions. Note: To contribute to this article, you may need to seek help from the author(s) of this page. |
| TF2 | |
|---|---|
| |
| A TF2-10 engine on display. | |
| Type | Turbofan |
| National origin | Chilokver |
| Manufacturer | Kowasaki Heavy Industries |
| Major applications | Shangtian F-8 Eagle Nakajima CF-05 Goshawk |
The Kowasaki TF2 is a series of afterburning turbofan jet engines developed by Kowasaki Heavy Industries.
Variants
- TF2-10
- Original variant of the TF2 developed for the Shangtian F-8 Eagle.
Applications
Specifications (TF2-20)
General characteristics
- Type: Afterburning turbofan
- Length: 4,145 mm (163.19 in)
- Diameter: 1,020 mm (40.16 in)
- Dry weight: 1,135 kilograms (2,502 lb)
Components
- Compressor: Axial compressor with 4 low-pressure and 8 high-pressure stages
- Combustors: Annular
- Turbine: 1 low-pressure and 1 high-pressure stage
Performance
- Maximum thrust: 56.75 kilonewtons (12,760 lbf) dry; 86.37 kilonewtons (19,420 lbf) with afterburner
- Overall pressure ratio: 24:1
- Bypass ratio: 0.57:1
- Turbine inlet temperature: 1,377 °C (2,511 °F)
- Thrust-to-weight ratio: 5.1 (dry), 7.8 (afterburning)