超级军网超过米26的直升飞机？？
来源：百度文库 编辑：超级军网 时间：2024/05/03 02:20:31
如果说你已经去过迪拜那个超级酒店，那么地球上还有一种可以飞的超五星酒店等着你，酒店基于苏制Mil V-12 改造，改装之后这部飞机将胜过美国的空军一号，奢华程度无与伦比，拥有客房服务、私人娱乐系统、温泉、瑜伽等，数码装备更是多，包括了平板电视，数码遥控，无线上网等，其长42米，高14米，最大起飞重量：105850KG，也就是105.85吨；最快速度：255KM/H ，巡航速度：237KM/H；首次飞行定于6月26日
（图片及文字皆来自于网络）
如果说你已经去过迪拜那个超级酒店，那么地球上还有一种可以飞的超五星酒店等着你，酒店基于苏制Mil V-12 改造，改装之后这部飞机将胜过美国的空军一号，奢华程度无与伦比，拥有客房服务、私人娱乐系统、温泉、瑜伽等，数码装备更是多，包括了平板电视，数码遥控，无线上网等，其长42米，高14米，最大起飞重量：105850KG，也就是105.85吨；最快速度：255KM/H ，巡航速度：237KM/H；首次飞行定于6月26日
（图片及文字皆来自于网络）
（图片及文字皆来自于网络）
如果说你已经去过迪拜那个超级酒店，那么地球上还有一种可以飞的超五星酒店等着你，酒店基于苏制Mil V-12 改造，改装之后这部飞机将胜过美国的空军一号，奢华程度无与伦比，拥有客房服务、私人娱乐系统、温泉、瑜伽等，数码装备更是多，包括了平板电视，数码遥控，无线上网等，其长42米，高14米，最大起飞重量：105850KG，也就是105.85吨；最快速度：255KM/H ，巡航速度：237KM/H；首次飞行定于6月26日 （图片及文字皆来自于网络）
欢迎来到地球！
真的假的…
愚人节的礼物
做的CG吧？看上去倒不错:D
Welcome to the Earth
How is Mars？:D
How is Mars？:D
最后一张，笔记本是DELL的，和我的一样。。
信鸽啊。。。
愚人节的礼物
愚人节的礼物
机体不是鸽子的.
从旋翼的大小看，这机机不一定能飞的起来
被忽悠了[:a10:]
YY图吧？
现实世界里的前苏联制Mil V-12 (也称Mi-12)是长这副模样
The Soviet made Mil Mi-12 (Also referred to as the V-12, NATO reporting name "Homer") is the largest helicopter ever built. The name "Mi-12" would have been the name for the production helicopter. Since the V-12 never went into production and only two prototypes were built, the name "Mi-12" was never adopted.
Contents
1 Design and deevelopment
2 Operators
3 Specifications (V-12)
4 See also
5 References
6 External links
Design and deevelopment
Development came about as a need for a heavy lift helicopter capable of carrying major missile components.[1] Production began on the V-12 prototype in 1965 with the goal of lifting no less than 30,000 kg.
The first prototype made its first lift-off on 27 June 1967. After a few oscillations in close proximity to the ground the V-12 made a rough touchdown on one wheel resulting in a burst tyre and a bent wheel disk. Even though the damage was insignificant, it was reported in the Western press that the prototype had suffered severe damage, and even to this day the rumor persists that the prototype had crashed fatally.
The V-12 features the only two-rotor transverse scheme ever built by Mil, eliminating the need for a tail rotor. The twin engines were taken together with the rotors from the Mil Mi-6 and duplicated on the V-12. Being the first time used by Mil, the twin rotor transverse scheme was not new. It was first seen in the Focke-Wulf Fw 61 the first fully controlable helicopter from 1936. Later, other helicopters used the scheme such as the Focke Achgelis Fa 223 Drache from 1940. The Soviet Kamov OKB built an experimental aircraft with the same scheme in 1958, Kamov Ka-22 Vintokryl . This aircraft had also the combined wing/rotor arrangement later used on the Mil V-12.
The first prototype, now wearing the registration CCCP-21142, made its first flight on 10 July 1968, flying from the Mil factory pad in Panki to the Mil OKB test flight facility in Lyubertsy. In February 1969, the first prototype lifted a 31,030 kg payload to 2,951m (9,682 feet). On 6 August 1969, the V-12 lifted 44,205 kg (88,636 lb) to a height of 2,255m (7,398 feet), a world record.
In May-June 1971 the first prototype V-12 CCCP-21142 made a series of flights over Europe being topped by the participation in the 29th Paris Air Show at Le Bourget wearing exhibit code H-833.
The second prototype had been assembled at the Mil experimental production facility in Panki but sat in the workshop for a full year waiting for its engines. It was not until March 1973 that the second prototype could make its first flight, being from Panki to the flight test facilities in Lyubertsy. Curiously the second prototype was also registered CCCP-21142.
The design outperformed its design specifications, set up numerous world records which still hold today, and brought its designers numerous awards such as the prestigious Sikorsky Prize awarded by the American Helicopter Society for outstanding achievements in helicopter technology. The V-12 design was recognized as an invention for which patents were issued in the USA, Great Britain and other countries.
Despite all of these achievements the Soviet Air Force refused to accept the helicopter for state acceptance trials for many reasons, the main one being the fact that the initial purpose for which V-12 had been developed no longer existed, i.e., the rapid deployment of strategic ballistic missiles. In the meantime the military concept of deploying missiles had been altered since some of the missiles had proved disappointing and were phased out. This was the same reason which led to the massive reduction in Antonov An-22 production. Another was that the design was expensive and that other lifting requirements were met with the Mi-6 and later by the more powerful Mil Mi-26.
All development on the V-12 was stopped in 1974. The first prototype remained at the Mikhail Leontyevich Mil helicopter plant in Panki-Tomilino, Lyuberetsky District near Moscow and is supposedly still there today. The second prototype was donated to Monino Air Force Museum (50 km east of Moscow) and is on public display.
Operators
Soviet Union
Soviet Air Force gave order for the project but cancelled it before going into production.
Specifications (V-12)
Data from Jane's All The World's Aircraft 1975-76[2]
General characteristics
Crew: 6 (pilot, copilot, flight engineer, electrician, navigator, radio operator)
Capacity:
VTOL 25,000 kg (55,000 lb) or
STOL 30,000 kg (66,000 lb) or
40,204.5 kg (88,636 lb) record
Length: 37.00 m (121 ft 4 in)
Rotor diameter: 2x 35.00 m (114 ft 10 in)
Height: 12.50 m (41 ft 0 in)
Loaded weight: 97,000 kg (213,850 lb)
Max takeoff weight: 105,000 kg (231,500 lb)
Powerplant: 4× Soloviev D-25VF turboshaft, 4,048 kW (6,500 shp) each
Freight compartment: 28.15x4.40x4.40 m (92 4x14 5x14 5 ft)
Performance
Maximum speed: 260 km/h (140 kt)
Range: 500 km (310 miles)
Service ceiling: 3,500 m (11,500 ft)
The Soviet made Mil Mi-12 (Also referred to as the V-12, NATO reporting name "Homer") is the largest helicopter ever built. The name "Mi-12" would have been the name for the production helicopter. Since the V-12 never went into production and only two prototypes were built, the name "Mi-12" was never adopted.
Contents
1 Design and deevelopment
2 Operators
3 Specifications (V-12)
4 See also
5 References
6 External links
Design and deevelopment
Development came about as a need for a heavy lift helicopter capable of carrying major missile components.[1] Production began on the V-12 prototype in 1965 with the goal of lifting no less than 30,000 kg.
The first prototype made its first lift-off on 27 June 1967. After a few oscillations in close proximity to the ground the V-12 made a rough touchdown on one wheel resulting in a burst tyre and a bent wheel disk. Even though the damage was insignificant, it was reported in the Western press that the prototype had suffered severe damage, and even to this day the rumor persists that the prototype had crashed fatally.
The V-12 features the only two-rotor transverse scheme ever built by Mil, eliminating the need for a tail rotor. The twin engines were taken together with the rotors from the Mil Mi-6 and duplicated on the V-12. Being the first time used by Mil, the twin rotor transverse scheme was not new. It was first seen in the Focke-Wulf Fw 61 the first fully controlable helicopter from 1936. Later, other helicopters used the scheme such as the Focke Achgelis Fa 223 Drache from 1940. The Soviet Kamov OKB built an experimental aircraft with the same scheme in 1958, Kamov Ka-22 Vintokryl . This aircraft had also the combined wing/rotor arrangement later used on the Mil V-12.
The first prototype, now wearing the registration CCCP-21142, made its first flight on 10 July 1968, flying from the Mil factory pad in Panki to the Mil OKB test flight facility in Lyubertsy. In February 1969, the first prototype lifted a 31,030 kg payload to 2,951m (9,682 feet). On 6 August 1969, the V-12 lifted 44,205 kg (88,636 lb) to a height of 2,255m (7,398 feet), a world record.
In May-June 1971 the first prototype V-12 CCCP-21142 made a series of flights over Europe being topped by the participation in the 29th Paris Air Show at Le Bourget wearing exhibit code H-833.
The second prototype had been assembled at the Mil experimental production facility in Panki but sat in the workshop for a full year waiting for its engines. It was not until March 1973 that the second prototype could make its first flight, being from Panki to the flight test facilities in Lyubertsy. Curiously the second prototype was also registered CCCP-21142.
The design outperformed its design specifications, set up numerous world records which still hold today, and brought its designers numerous awards such as the prestigious Sikorsky Prize awarded by the American Helicopter Society for outstanding achievements in helicopter technology. The V-12 design was recognized as an invention for which patents were issued in the USA, Great Britain and other countries.
Despite all of these achievements the Soviet Air Force refused to accept the helicopter for state acceptance trials for many reasons, the main one being the fact that the initial purpose for which V-12 had been developed no longer existed, i.e., the rapid deployment of strategic ballistic missiles. In the meantime the military concept of deploying missiles had been altered since some of the missiles had proved disappointing and were phased out. This was the same reason which led to the massive reduction in Antonov An-22 production. Another was that the design was expensive and that other lifting requirements were met with the Mi-6 and later by the more powerful Mil Mi-26.
All development on the V-12 was stopped in 1974. The first prototype remained at the Mikhail Leontyevich Mil helicopter plant in Panki-Tomilino, Lyuberetsky District near Moscow and is supposedly still there today. The second prototype was donated to Monino Air Force Museum (50 km east of Moscow) and is on public display.
Operators
Soviet Union
Soviet Air Force gave order for the project but cancelled it before going into production.
Specifications (V-12)
Data from Jane's All The World's Aircraft 1975-76[2]
General characteristics
Crew: 6 (pilot, copilot, flight engineer, electrician, navigator, radio operator)
Capacity:
VTOL 25,000 kg (55,000 lb) or
STOL 30,000 kg (66,000 lb) or
40,204.5 kg (88,636 lb) record
Length: 37.00 m (121 ft 4 in)
Rotor diameter: 2x 35.00 m (114 ft 10 in)
Height: 12.50 m (41 ft 0 in)
Loaded weight: 97,000 kg (213,850 lb)
Max takeoff weight: 105,000 kg (231,500 lb)
Powerplant: 4× Soloviev D-25VF turboshaft, 4,048 kW (6,500 shp) each
Freight compartment: 28.15x4.40x4.40 m (92 4x14 5x14 5 ft)
Performance
Maximum speed: 260 km/h (140 kt)
Range: 500 km (310 miles)
Service ceiling: 3,500 m (11,500 ft)
看起来有点不安全的感觉，还是固定翼的保险
做包机可以，做酒店意义不大
是愚人节的玩笑，不过概念还是不错的
楼主你的地球科考任务辛苦了
真是太豪华了!
有了也没人敢坐的[:a9:]
是美国人愚人节的恶搞。
欢迎来到地球;P
酒店直升机……好雷人呀~
新浪都说了：假的
变态的忽悠。。。。{:3_77:}
fire star bird
Mi12 的改良版？
有点意思
创意不错