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Laki visenamenski ( skolsko -sportski ) helikopter( izdelie 300) , NATO naziva `Hermit` nastao je po zahtevima DOSAAF /Добровольное общество содействия армии, авиации и флоту (ДОСААФ)/ kao zamena za Mi-1 i Mi-2.
U sastavu sovjetskog DOSAAF
Inace siroko poznat po svojim izuzetnim letnim i manevarskim sposobnostima( izvodi `valjak` i `petlju` bez problema ) imao je prvi let jos 17.nov 1986g. Vec sledece godine biva prvi put i javno prikazan na Le Burzeu ( Pariz ) .
Do sada je proizvedeno oko 30 komada ( 2 izgubljena u udesima ) a jedan od najvecih kupaca je bila Nigerija .
TTK sa ruske wiki
Citat:Ми-34 - лёгкий четырёхместный многоцелевой вертолёт. Двигатель - М-14.
Первый полёт опытный Ми-34 01-черный совершил 17 ноября 1986 года.
Серийное производство началось на ААК Прогресс (г. Арсеньев) в 1993 году, приостановлено в 2002 году.
В настоящее время ведётся работа по восстановлению производства модифицированных вариантов Ми-34С1 с двигателем М9ФВ и Ми-34С2 с двигателем Arrius-2F.
Citat:Технические характеристики
Экипаж: 1-2
Пассажировместимость: 2-3
Длина: 8,851 м (без учёта несущего и рулевого винтов)
Диаметр несущего винта: 10,0 м
Диаметр рулевого винта: 1,48 м
Высота: 2,75 м (по втулке несущего винта)
Масса снаряжённого: 1137 кг
Максимальная взлётная масса: 1450 кг
Масса топлива во внутренних баках: 131 кг
Силовая установка: 1 × ПД М-14В26В
Мощность двигателей: 1 × 325 л.с.
Лётные характеристики
Максимально допустимая скорость: 200 км/ч (при полётной массе более 1350 кг)
Крейсерская скорость: 155 км/ч (при полётной массе более 1350 кг)
Практическая дальность: 349 км
Практический потолок: 4000 м (при взлётной массе 1280 кг)
Статический потолок: 900 м
Varijante sa engl ( bolja pojasnjenja )
Citat:
Variants
Mi-34S - four seat production model powered by a 239 kW (325 hp) Vedeneyev (VOKBM) M-14V-26V nine-cylinder, air-cooled, radial engine mounted sideways in the fuselage, and equipped with modern avionics. A few aircraft were purchased by the Moscow police.
Mi-34S2 "Sapsan" - turbine version of the Mi-34. It will be able to accommodate up to 4 passengers and the first deliveries are planned by the end of 2011. It will be powered by Turbomeca Arrius-2F
Mi-34L - proposed version powered by a 261 kW (350 hp) Textron Lycoming TIO-540J piston engine. None built.
Mi-34P Patrulnyi (English: patrol) - Police patrol version for Moscow Mayor Office.
Mi-34A - Luxury version, intended to be powered by an Allison 250-C20R turboshaft engine. None built.
Mi-34M1 and Mi-34M2 - Proposed twin-turbine, six-passenger versions.
Mi-34UT - trainer with dual control.
Mi-34V or Mi-34VAZ or Mi-234 - proposed version powered by two VAZ-4265 rotary piston engines.
Mi-44 - proposed development with TV-O-100 engine and refined aerodynamics. A mockup was built in 1987.
Interesantno je da se jedan primerak nalazi u sastavu OS BiH ali je on veci duzi period neoperativan
Citat:The sole Mi-34 'Hermit' still awaiting its fate, the aircraft was acquired from Russia for training but was soon grounded and has not flown since.
 
Registar
Pеестр вертолётов типа Миль Ми-34
 http://russianplanes.net/planelist/Mil/Mi-34
Po podacima od 2011 varijanta S2 `Sapsan` kosta 1 `milku` / US $1 million (Mi-34S2, 2011)/
izvori
http://en.wikipedia.org/wiki/Mil_Mi-34
Odlicna manevribilnost se moze gledati na ovom snimku
Mi-34 helicopter aerobatics
Citat:This is the best aerobatics helicopter. Actually, the only one in it's class. Mil' design burau, MI-34C.
The pilot is Sergei Barkov.
http://www.youtube.com/watch?v=_7ag_dVC9MM
Ovaj sajt daje podatak da kosta svega 450.000dol ( bazicna varijanta )
http://www.aircraftcompare.com/helicopter-airplane/MIL-Mi-34-Hermit/285
Jos malo interesantnih podataka sa sl. sajta
Citat:Trials in 1999 by civil pilot training school at Omsk showed Mi-34 to be 2.8 times cheaper and more effective to operate than current fleet; school to acquire three Mi-34Cs and obtain up to 10 more in long term. Other schools expected to replace ageing Mi-2 with Mi-34.
Mi-34S: Basic version; marketed in Russia as Mi-34; certified by Interstate Aviation Committee Aviation Register (initially at 1,350kg max take-off weight), with helicopter, engine and noise type certificates; meets FAR Pt 27 requirements.
DESiGN FEATURES: Acrobatic helicopter; intended initially for training and international competition flying; conventional pod and boom configuration; piston engine of same basic type as that in widely used Yakovlev fixed-wing training aircraft and Kamov Ka-26 helicopters; suitable also for light utility, mail delivery, observation and liaison duties, and border patrol; later developments concentrate on light transport role.
Aerobatic capabilities include looping; backwards flight at 130km/h; and rotation about main rotor axis at 120 degrees/s.
FLYING CONTROLS: Manual, with no hydraulic boost.
STRUCTURE: Semi-articulated four-blade main rotor with flapping and cyclic pitch hinges, but natural flexing in lead/lag plane; blades of GFRP with CFRP reinforcement, attached by flexible steel straps to head like that of Boeing MD 500; two-blade tail rotor of similar composites construction, on starboard side; riveted light alloy fuselage; sweptback tailfin with small unswept T tailplane.
COSTS: US$400,000, fully equipped (2003).
http://www.aviastar.org/helicopters_eng/mi-34.php
Kabina
http://www.avia-russia.com/mil-mi-34.html
http://www.airliners.net/aircraft-data/stats.main?id=282
Motor
 
http://www.assegaitrading.co.za/airplane/mi34c.html
Novi radijalni motor -M9FV engine for Mi-34
U sluzbi Moskovske Milicije
 
Nigerijski svojevremeno imali problema
Gearbox failures lead Nigerian Air Force to sell Mi-34 fleet
Citat:The problem has centred on the main rotor gearboxes, which have a maintenance schedule of 1500 hours from the manufacturer. However, the experience of the Nigerian Air Force is that the bulk of these gearboxse have failed within 300 hours, and have consequently the Mi-34 fleet became hangar-bound.
http://helihub.com/2011/07/27/gearbox-failures-lea.....-34-fleet/
a od kraja prosle godine se nalaze u N.Zelandu kome su i prodani
Citat:24 Mar, 14
The Nigerian Air Force procured Mil Mi-34C (NATO code Hermit) helicopters around 2002 with the intention of using them for ab initio training. In July 2011, HeliHub.com reported that they had all been withdrawn from use - reportedly due to main gearbox issues - with the intention of disposing of them. The Mi-34C is powered by a Vedeneyev M14V nine-cylinder radial engine developing 325hp.
By December 2013, six of the original batch (variously reported as 8 or 12 in total) arrived in New Zealand after they had been acquired by an unnamed purchaser.
http://helihub.com/2014/03/24/nigerian-air-force-m.....w-zealand/
Na MAKS-2009 je prezentovan `Sapsan`
http://de.ria.ru/photolents/20090814/122706742.html
 
Citat:The Sapsan (Russian for peregrine falcon) is a five-seater, lightweight utility and training helicopter. It is similar to a Mi-34, with its combustion engine replaced by the French Turbomeca Arrius-2F turbo shaft engine. This adds a lot of power along with an engine weight reduction by a factor of two. The Turbomeca Arrius-2F engine also has a good international reputation, and is widely used in light helicopter models. These factors should all contribute to a second life for the Mi-34S2 Sapsan.
The Mi-34S2 will have to compete with models like Eurocopter's EC120. First deliveries are planned for 2016, but Russian Helicopters has stated that it will only start production when it has received enough orders. The Sapsan can be ordered with Russian or Western avionics.
http://www.helistart.com/helicopters/Mil/Mi-34S2_Sapsan
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