法国微型涡轮发动机公司的TRI60系列

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牌　　号　TRI 60
用　　途　军用涡喷发动机
类　　型　涡轮喷气发动机
国　　家　法国
厂　　商　微型涡轮发动机公司
生产现状　生产
装机对象　TRI60-1-067　　　　“海鹰”反舰艇导弹。
TRI60-2-071　　　　C.22遥控飞行器、靶机。
TRI60-2-074　　　　MQM-107A/B导弹/靶机。
TRI60-2-077　　　　RBS15M反舰艇导弹。
TRI60-2-080　　　　PTA靶机。
TRI60-2-088　　　　NV-144/NV-151靶机。
TRI60-2-089　　　　RBS15F/ASM15导弹。
TRI60-3-097　　　　BQM-126靶机。

研制情况

TRI60是为70年代中期生产的小型飞机、无人靶机和导弹设计的小型涡轮喷气发动机，1974年6月第一台验证机开始台架试验，1976年选用于C.22。
TRI60的研制费用由法国政府提供。它的设计偏重于费用最低和无需维修。它是微型涡轮发动机公司第一种采用轴流压气机与环形燃烧室的发动机。TRI60的结构简单，燃烧室冒烟很少，起动方式随用途不同而异。其设计寿命为20多小时。
TRI60-1-067　早期型。采用了液压气动式燃油控制系统。
TRI60-2-071　是TRI60-1的改型。采用连续控制的电子控制系统。油门完全可调。
TRI60-2-074　结构类似于-071，但装有由燃气发生器轴直接驱动的1.5kVA的交流发电机。
TRI60-2-077　其性能类似-071型。
TRI60-3　其尺寸类似-2型。
TRI60-20　是微型涡轮发动机公司不加力涡轮喷气发动机计划中推力最大的发动机，增加了1级压气机。

法国微型涡轮发动机公司的TRI60系列

法国微型涡轮发动机公司的TRI60系列

Variants
There are many variants of this engine and it is used in many missiles and UAVs, as listed below. Aside from the known uses listed below, it is widely speculated that Iran illegally purchased many TRI-60 engines from Microturbo to assemble C-802 cruise missiles purchased from China. It is unclear which variant was purchased.

TRI 60-1
This variant produces 3.5 kN (787 lbf) of thrust, and is predicted to power the Meteor Mirach 300 and Meteor Mirach 600 remotely piloted vehicles.

TRI 60-1 067: This variant (same performance as the plain "60-1" model) powers the P3T Sea Eagle anti-ship missile.
TRI 60-2
This variant is an uprated model of the 60-1 engines, with thrust increased to 3.7 kN (832 lbf).

TRI 60-2 071: This model powers the Aerospatiale C.22 target drone, and is slight uprated to 4.0 kN (900 lbf).
TRI 60-2 074: This model powers several versions of the MQM-107 Streaker drone.
TRI 60-2 077: This model powers the RBS-15 anti-ship missile.
TRI 60-2 080: This model powered early Lakshya PTA drones.
TRI 60-2 088: This model powered the flight test vehicles of the Northop NV-144 next-generation drone.
TRI 60-2 089: This model powers the RBS-15 anti-ship missile.
TRI 60-2 206: This model powers the Aerospatiale C.22 target drone, and is slight uprated to 4.0 kN (900 lbf).
TRI 60-2 227: This model powers the RBS-15 anti-ship missile.
TRI 60-3
This variant produced 4.0 kN (900 lbf) of thrust, and was chosen to power the now-canceled Beech BQM-126 target drone. This variant of the engine was designated J403-MT-400 by the United States Navy.

TRI 60-5
This variant produces 4.4 kN (990 lbf) of thrust at a compression ratio of 4.1:1. It powers the Mk. III variant of the RBS-15 anti-ship missile as well as the Alenia Sky-X unmanned aircraft. This engine also powered (or was an option to power) the "D" and "E" variants of the MQM-107 target drone.[5] The "5+" variant powers the BQM-167 Skeeter target drone. The 5+ model also demonstrated the engine's supersonic flight capability in 2007. As of 2008, this is the last three-compressor-stage variant of the TRI 60 in production.

TRI 60-20
This variant features a 4 stage compressor (like the 60-30 variant below).It is aimed at target drone aircraft, and is essentially identical to the 60-30 except for being de-rated to 5.4 kN (1214 lbf) to extend the engine's life. As of 2008, it only existed as a prototype and was tested on a MQM-107 drone.

TRI 60-30
Like the TRI 60-20, the -30 variant features a 4 stage compressor that increased the compression ratio to 6.3:1 and increases rated thrust to 5.7 kN (1281 lbf). This engine is used in the MBDA Apache and Storm Shadow / SCALP EG cruise missiles.

官方介绍
http://www.safran-power-units.com/propulsion-systems/microturbo-european-leader-turbojet-engines
http://www.safran-power-units.com/sites/microturbo/files/microturbo_fiche_tr60-30_-_uk.pdf
http://www.safran-power-units.com/sites/microturbo/files/microturbo_fiche_tr60-5_-_uk.pdf
http://www.wikiwand.com/en/Microturbo_TRI_60

jy_jet

楼主，第一张图不是MT公司的吧？

自在飞行

jy_jet 发表于 2017-7-24 17:05
楼主，第一张图不是MT公司的吧？

终于有人回复了，

确实不是，那张是J402，用在鱼叉和战斧里的
等着被发现，哈哈，被人发现，就删了吧