[原创]丝带已被正式命名和型号(国外)和最详细的数据

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大家都叫丝带(其实是5代机),也很好听的,也叫顺口了和听惯了,

干脆就叫”丝带(英语就叫SIDAI)”吧!



在国外的网站上已经给丝带命名和其型号了,

J-20 'Black Eagle'-“黑鹰”。(黑鹰?我还直升机哪。)



丝带已被正式命名和型号(国外)和最详细的数据


J-20 'Black Eagle'

J-20 “黑鹰”

Role Stealth air superiority, multirole fighter

用途 隐形优势多功能战斗机

National origin China

研发国家 中国

Manufacturer Chengdu Aircraft Corporation

制造商 成都飞机工业(集团)有限责任公司

First flight 2010-2011

首飞 2010-2011

Introduced 2017-19 (planned)

引进 2017-19(计划中)

Status In development/taxi trials

状态 发展/地面滑行测试中

Primary user People's Liberation Army Air Force

主要使用者 中国人民解放军空

Number built 2

已制造数目 2



The Chengdu J-20 is a fifth generation stealth, twin-engine fighter aircraft prototype developed by Chengdu Aircraft Corporation for the People's Liberation Army Air Force.

成都J-20是一架第5代隐形,双发战斗机,其原型机由成都飞机工业(集团)有限责任公司为中国人民解放军空军研发。

It is a multi-role, heavy fighter with stealth capability and maneuverability.

它是一架有隐形性能和高机动性的多用途,重型战斗机。



The J-20 was one of the stealth fighter programs under the codename J-XX that was launched in the late 1990s.

J-20是隐形战斗机计划中,其中一个开始与1990后,代号为J-XX的计划。

Two prototypes (#2001 & 2002) have been built as of the end of 2010.

2架原型机(编号2001和2002),已在2010底制造完成。

On December 22, 2010, the J-20 was under going high speed taxi tests at its Chengdu facility with no confirmed flight tests yet.

在2010年12月22号,J-20在它的成都工厂进行了地面高速测试,但还未有证实的飞行测试记录。

It has been reported that top level officials have come to the Chengdu facility to witness the first flight test.

测试报告已经上交给最高层,并等待最高层的到来,观看首飞测试。



丝带已被正式命名和型号(国外)和最详细的数据


The J-20, which appears to be somewhat larger and heavier than the comparable Sukhoi T-50 and Lockheed Martin F-22 Raptor, is a single-seat, twin-engine aircraft.

J-20是单座,双发飞机,大于和重于与其类似的苏凯T-50战机和洛克希德马丁的F-22猛禽战机,

It is approximately 75 feet in length, has a wingspan of 45 feet or more, and is expected to have a takeoff weight of 75,000 to 80,000 pounds (34,000 to 36,000 kg) with internal stores only.

它大约24米长,14米宽或更大,在无外部附加下,猜测其起飞重量为34顿到36顿。

It is likely powered by twin Saturn AL-31 engines provided by Russia, which have 32,000-pounds thrust coupled with thrust vectoring nozzles made in China.

它可能使用的是2台由俄罗斯制造的土星 AL-31引擎,在配合由中国制造的矢量推力喷嘴能为其制造大约14.5顿的推力。

The J-20 may have lower stealth and supercruise performance than the F-22, but has larger weapon bays and can carry more fuel.

J-20的隐形性能和机能能力也许会弱于F-22,但它有较大的武器舱和能携带更多燃料的油箱。

The J-20 has a long and wide fuselage and low jet engine intakes with a forward chine, a main delta wing, forward canards, a bubble canopy, conventional round engine exhausts, and canted all-moving fins.

J-20有一个长而宽的机身和前部有一个小突起的低喷射引擎进气口,一个大三角翼,前部鸭翼,一个水泡型座舱,传统圆形的引擎喷口。

The front section of the J-20 is modelled after the F-22 and the body and tail compare to the Sukhoi PAK FA.

J-20的前部与F-22接近,而机身和尾部类似于苏凯PAK FA.


The J-20 has been described as having a pair of all-moving tailfins and ventral stabilizing fins.

J -20被发现有一对全动垂直尾翼和固定腹翼。

It also features an F-22 style nose section, including Caret intakes but with diverterless supersonic inlet (DSI) bumps installed at the upper corners, as well as a one-piece canopy.

它的机鼻貌似F-22,貌似的还包括旁边的进气口,但它的进气口使用的是有一个鼓包状突起的无附面层隔道进气道(DSI)。

The J-20 also incorporates an advanced fly-by-wire (FBW) system fully integrated with the fire-control and the engine systems.

J-20还使用了改进过的有线制导飞行系统(FBW),并完全与武器控制和引擎系统整合一体。

Its fire-control radar is expected to be Active Electronically Scanned Array (AESA) (Type 1475/KLJ5?).

武器控制雷达估计使用的是有源电子扫描阵(AESA)(型号1475/KLJ5?)。

The aircraft may feature a "pure" glass cockpit (a single F-35 style color liquid crystal display (LCD) display and a wide-angle holographic head-up display (HUD)).

这飞机将来也许会使用纯玻璃座舱(一个单一的F-35风格彩色液晶显示屏(LCD)和一个头部广角全息屏幕(Huda)。

Many of these subsystems have been tested onboard J-10B to speed up the development.

许多子系统已经在J-10B上使用并测试过了,从而加快了研发的速度。

It was reported in November 2006 that a T/W=10 17,000kg class turbofan (WS-15/"large thrust") is being developed for J-20.

据报告,在2006年11月,T/W-10涡轮喷射发动机以达到17顿推力 (W/S-15 推力更大?),并为能在J-20上使用而进行进一步发展。

The rear of the aircraft includes underwing actuator fairings, axisymmetrical engine exhausts and the ventral fins which may increase the radar cross section (RCS).

此飞机的后部包括有水平尾翼,引擎喷口和腹翼,而腹翼也许会加大雷达反射横截面(RCS)。


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[ 转自铁血社区 http://bbs.tiexue.net/ ]

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