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通化超重型pu橡胶万向脚轮批发价新闻 - 通化其它机械 - 百业招商网
通化超重型pu橡胶万向脚轮批发价新闻
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电视机挂架怎么安装呢?首先要准备好安装的材料,在购选的时候一定要注意挂架和五金件的质量。
电视挂架安装步骤二
进行电视挂架安装的时候按照说明书上的看,一般的步骤都比较简单,最主要的是动手能力。
电视挂架安装步骤三
在选择安装电视挂机的位置时,不要选择承重墙或者湿度、光度比较强的地方。
电视挂架安装步骤四
电视机挂架怎么安装比较好呢?其实电视机挂架安装并不是很难,但是在进行接线接口的处理时是需要一定的技巧的。这就需要安装的时候注意留出合适的位置
电视挂机安装注意事项
1、选择电视挂架时需注意电视机孔位是否规则,是不是四个孔位,是不是长方形或者正方形形状。
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, the . It features
fitted with , a , and a
control system. It was first flown in 1988 and certified in 1992. The basic Il-96-300 is equipped with modern Russian avionics integrating six multi-function colour LCD displays, inertial and satellite navigation systems, and a
(including mode "S"). It allows the airplane to be operated with two . The avionics correspond to modern requirements on international routes in Europe and North America (RNP-1) and allow navigation and landing under ICAO CAT III/A conditions. The Il-96 is offered in three main variants: the Il-96-300, Il-96M/T and Il-96-400.[]
The Il-96-300 has a standard passenger capacity of 262 seats in a two-class configuration with 18 seats with a
of 54 inches (140 cm) and 244 seats with a pitch of 32 inches (81 cm), of which typical seating is 3-3-3 (layout), but low density seating is 2-4-2 (layout possible).
are positioned on the upper deck, and the lower deck can accommodate 18
containers and crew rest areas.
Cockpit of an Aeroflot Il-96-300
In June 2005, the
signed a 15-year financial agreement with Ilyushin Finance Corporation (IFC) to take delivery of two new-build Il-96-400T aircraft, to be operated by Volga-Dnepr's subsidiary . The first was due to have been delivered in late 2006.
Government newspaper
announced on 3 January 2006 the first official flight of the
Il-96-300, from
On 11 August 2009 Russian Minister of Industry and Trade
announced that manufacturing of the Il-96-300 would cease. In particular, the Il-96-300 had been deemed inferior to counterparts from Boeing and Airbus, and the manufacturer could not arrange commercially viable mass production, making only one aircraft per year. The Il-96-400T cargo version was to remain in production.
On 9 October 2015, it was announced that an updated version of the Il-96 may be produced. This decision was taken due to the current diplomatic situation between Russia and the West, and the dependency of the Russian Aerospace Industry on Airbus and Boeing. In September 2017, the Vice President of Russia’s United Aircraft Corporation Aleksandr Tulyakov announced the start of development of the 250-280 seat, wide-body long-haul aircraft in partnership with Chinese builders. The aircraft is to be a development of the Russian-designed IL-96 and will be assembled in China. A new engineering center will be built in Russia to undertake technical and electronics production.
There are two variants of the Il-96. The Il-96-300 was launched in 1985 with introduction into service in 1993. The Il-96M was launched in 1993 with introduction into service in 2000.
Ilyushin Il-96-300
The Il-96-300 is the initial variant and is fitted with
turbofans with a thrust rating of 16,000
(157 , 35,300 ). Development started in mid-80s while the first prototype flew on 28 September 1988. The first Il-96 entered service with Aeroflot in 1993.[]
Range with 262 passengers and fuel reserves (for holding 75 minutes at an altitude of 450 m) in a two-class configuration is about 11,000 km (5,940 nmi), allowing flights from
cities, a far improvement over the Ilyushin Il-86. A highly customized version of the Il-96-300, called Il-96-300PU is used as the primary aircraft in the
fleet. Four were used by Russian president , and by
as VIP planes. The VIP aircraft is operated by . The
use IL-96 300.
There were plan to produce a variant dubbed Il-96-300V which would include two sets of
livery at the MAKS Airshow, August 2007
The Il-96M is a stretched variant of the Il-96-300. It features a 10 m (30 ft) fuselage stretch, is 15 tonnes (33,000 lb) heavier, is fitted with Western-style avionics, and is powered by four
engines with a thrust rating of 165 kN (37,000 lbf). Range with 312 passengers in a three-class configuration or 92 tonne (203,000 lb) payload is about 10,400 km (5,600 nmi). This turned it into a true—but vastly more capable—Il-86 successor. The Il-96M/T is broadly comparable with the
and CF, but is much cheaper. Development on the M/T variant stalled when the
suspended talks on financing the engines and avionics, following pressure from . The dispute was later settled following an Aeroflot order for ten Boeing 737-400s—placed in April 1997 in a deal worth US$440 million— that were granted a tax exemption by the R nevertheless, the financing was blocked again when four Boeing 767-300ERs also ordered by Aeroflot were not included in the accorded exemption. The deal was never realised.
This is the freighter version of the Il-96-400. It is powered by four
The Il-96-400 is similar to the Il-96M, but features Russian avionics and engines. It is powered by four
turbofans and can carry up to 436 passengers. Typical two-class configuration will have 386 passengers. Range with 315 passengers in a three-class configuration is about 10,000 km. A special version, dubbed Il-96-400VT, was reported on Friday 19 March 2010 by the Wall Street Journal to bid on the US $40 billion Air Force Tanker Program contract. In February 2013,
signed a deal for the order of three 350-seater Ilyushin Il-96-400s.
In February 2017, it was announced that Russia’s United Aircraft Corporation had signed a contract with its subsidiary Ilyushin Aviation Complex for the development of a new version of Ilyushin Il-96-400 wide-body passenger airliner. The first flight of the new aircraft is scheduled for 2019. Il-96-400M is the passenger version of the Il-96-400T cargo aircraft. Its fuselage is 9.65 m longer than the existing Il-96-300 passenger variant. The planned seating capacity is 390 passengers.
In January 2015, a new tanker variant of the Il-96, designated the Il-96-400TZ, was introduced, with an initial order for two aircraft placed by the Russian Ministry of Defense. The new tanker will be able to transfer more than 65 tons (IL-78M 40 tons) of fuel at a distance of up to ;km (Il-78M ;km). Universal aviation refueling systems ORM-1, proven on existing combat aircraft tankers Il-78/78М, will be installed on the aircraft.
costs, Ilyushin is studying a twin-engined development, powered by over 340 kN (76,000 lbf)
developed by 2025 from the , or foreign powerplants.
As of December 2016, current operators of the Ilyushin Il-96 are:
Aircraft Type
In Service
(government fleet)
Il-96-400T
Il-96-400TZ
In 2005, Russia indefinitely grounded Ilyushin 96-300 passenger aircraft after transport inspectors pointed out malfunctions in the jets’ braking systems. The decision came just weeks after a technical glitch in an Ilyushin 96-300 forced Russian President Vladimir Putin to fly in a back-up plane during a visit to Finland.
On 3 June 2014, RA-96010 of , which had been retired from service, was damaged beyond economical repair in a fire whilst parked in storage at , .
Measurement
55.3 m (181 ft 7 in)
64.7 m (212 ft 3 in)
63.939 m (209 ft 9.28 in)
60.11 m (197 ft 3 in)
350 m? (0;ft?)
Wing sweep
Flaps/Slats
I – 2°/3° (275 KIAS), II 3°/25° (264 KIAS), III – 10°/25° (243 KIAS),
IV – 25°/25° (210 KIAS) for Takeoff, V – 40°/25° (189 KIAS) for Landing
Cabin width
5.70 m (18.70 ft)
Fuselage Diameter
6.08 m (19.94 ft)
15.7 m (57 ft 7 in)
Operating Empty Weight
120,400 kg (265,198 lb)
132,400 kg (291,630 lb)
116,400 kg (256,387 lb)
122,300 kg (269,383 lb)
Max. Zero Fuel Weight
180,000 kg (403,000 lb)
208,400 kg (459,030 lb)
Max. Landing Weight
183,000 kg (403,083 lb)
220,000 kg (484,581 lb)
220,000 kg (484,581 lb)
220,000 kg (484,581 lb)
Max. Take-off Weight
250,000 kg (551,000 lb)
270,000 kg (595,000 lb)
270,000 kg (594,713 lb)
265,000 kg (583,700 lb)
Max. Payload
40,000 kg (88,105 lb)
58,000 kg (127,753 lb)
92,000 kg (202,643 lb)
58,000 kg (127,753 lb)
Takeoff Run at
2,340 m (7,677 ft)
3,000 m (9,843 ft)
2,700 m (8,858 ft)
2,700 m (8,858 ft)
Landing Run
860 m (2,821 ft)
1,800 m (5,906 ft)
1,650 m (5,511 ft)
1,650 m (5,511 ft)
Cruising speed
0.78 to 0.84
or 850 to 870 km/h TAS (459 to 469 KTAS)
Maximum speed ()
0.84 Mach or 900 km/h IAS (485 KIAS)
Service ceiling
13,100 m (43,000 Ft)
Cruise Altitude
9,000 to 12,000 m (29,527 to 39,370 Ft)
Range with max. payload
11,500 km (6,209 )
12,800 km (6,907 nmi)
5,000 km (2,699 nmi)
10,000 km (5,400 nmi)
Range with max. fuel
13,500 km (7,289 )
15,000 km (8,100 nmi)
12,000 km (6,479 nmi)
12,000 km (6,479 nmi)
Max. Fuel capacity
152,620 l (40,322 )
Engines (x4)
Aviadvigatel PS-90A1
Aviadvigatel PS-90A1
Thrust (x4)
PS-90A: 156.9 kN
(35,242 lb)
N2:10,425 RPM
170.1 kN
(38,250 lb)
N2:12,360 RPM
PW kN
(37,500 lb)
N2:12,360 RPM
PS-90A1: 170.7 kN
(38,326 lb)
Engine Dry Weight (x4)
2,950 kg
(6,497 lb)
3,314 kg
(7,300 lb)
PW kg
(7,300 lb)
2,950 kg
(6,497 lb)
Cockpit crew
Two (op. Three)
3-class Seating capacity
2-class Seating capacity
1-class Seating capacity
Cargo Capacity
F.H.1: 9,000 kg (Front)
F.H.2: 15,000 kg (Back)
F.H.3: 1,000 kg (Back)
6 LD3 (front)
10 LD3 (Rear)
580 m? main deck
114 m? front lower deck
82 m? rear lower deck
18 LD3 (Front)
14 LD3 (Rear)
114 m? front lower deck
82 m? rear lower deck
18 LD3 (Front)
14 LD3 (Rear)
Data from Ilyushin Aviation Complex, FAA Certification Document A54NM and Il-96-300 Pilot Manual
The airplane has the following systems installed, providing compliance with
recommendations and
requirements:
Integrated communication and navigation control panel and flight management system
with LCD indicators
Weather radar
Related development
Aircraft of comparable role, configuration and era
Related lists
. Новости Mail.Ru.
. Archived from
Стрюк, Игорь.
. VOLGA-DNEPR GROUP. 27 March 2005. Archived from
on October 16, .
Gómez Lluciá, Julio (January 3, 2006).
(in Spanish). Granma. Archived from
on March 4, 2008.
Kolobkov, Sergei (August 11, 2009).
(in Russian). RBC Daily. Archived from
on August 14, 2009.
. Archived from
on 1 April .
Александр, Артемьев. . www.e-reading.club.
. www.ilyushin.org.
. Ilyushin. Archived from
on September 19, 2008.
John Pike.
. Archived from
on 27 July .
. 15 August 2016.
. Flightglobal. 27 August .
. livejournal.com. Archived from
. function.mil.ru 2015.
David Kaminski-Morrow (9 Feb 2018). . Flightglobal.
. Archived from
. RadioFreeEurope/RadioLiberty.
Hradecky, Simon. . The Aviation Herald 2014.
. Flightglobal.com. Archived from
The Vmo values for military operation are higher
All the PS-90A turbofan can be upgraded to the new PS-90A2 version, with the latest generation FADEC of western design and many other improvements. The maintenance costs are reduced by 40%. The fuel consumption (SFC) of this version is equivalent to current Western turbofans. PS-90A2 variant meets the ETOPS-180 rules, ICAO-4 and AP-33 (equivalent to FAR-33/JAR-33). The Maximum thrust is 16,000 kg or 18,000 kg.
Ilyushin has not ruled out the possibility to install other engines (PW, RR, or CFM), depending on the number of requests from customers.
. ILYUSHIN a UAC company 2014.
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