| Název: Name: | Klimov VK-105PF (M-105PF) | Klimov VK-105PF (M-105PF) |
| Originální název: Original Name: | Климов ВК-105ПФ (М-105ПФ) | |
| Kategorie: Category: | vidlicový motor | vee engine |
| Výrobce: Producer: | Štátny letecký priemysel ZSSR | |
| Období výroby: Production Period: | DD.MM.1942-DD.MM.1945 | |
| Vyrobeno kusů: Number of Produced: | 28000 | |
| Prototyp vyroben: Prototype Built: | DD.MM.RRRR | |
| Použití: Use: | Lavočkin LaGG-3, Jakovlev Jak-1, Petljakov Pe-2, Jakovlev Jak-7, Gorbunov "105" | |
| Technické údaje: Technical Data: | ||
| Počet válců: Number of Cylinders: | 12 | |
| Hmotnost: Weight: | 620 kg | 1367 lb |
| Celková délka: Overall Length: | ? mm | ? |
| Celková šířka / Průměr: Overall Width / Diameter: | ? mm | ? |
| Celková výška: Overall Height: | ? mm | ? |
| Vrtání: Bore: | ? mm | ? |
| Zdvih: Stroke: | ? mm | ? |
| Zdvihový objem: Swept Volume: (l/cu in) | 35 l | 2135.83 cu in |
| Palivo: Fuel: | ? | ? |
| Příprava palivové směsi: Carburation or Injection: | ? | ? |
| Kompresní poměr: Compression Ratio: | 7,1:1 | 7,1:1 |
| Plnění válců: Mixture Charging: | - | - |
| Chlazení: Cooling: | vodou | water |
| Výkony: Performance: | ||
| Výkon: Power: | 889.9 kW při 2700 ot/min | 1193.4 bhp at 2700 rpm |
| Poznámka: Note: | vzletový režim: - výkon: 890 kW (1210 k) pri otáčkach (ot/min) : 2600 nominálny režim: - výkon: pri zemi: 890 kW (1210 k) pri otáčkach (ot/min) : 2700 vo výške 700 m: 927 kW (1260 k) vo výške 2700 m: 868 kW (1180 k) | - |
| Zdroje: Sources: | www.klimov.ru | |
Klimov VK-105PF (M-105PF)
Климов ВК-105ПФ (М-105ПФ)
VK-105PF (M-105PF)
ВК-105ПФ (М-105ПФ)
- in-line piston engine
The M-105PF engine, from 1943 designated VK-105PF after the name of its designer, was a liquid-cooled twelve-cylinder piston engine with V-cylinders, designed in the V.J.It was a modification of the M-105P engine (ОКБ В.Я.Климова), specifically to increase its power. Hence the F designation after the engine number, which stands for Forsirovanyj (Фоорсироованный), i.e., with increased power. The substantial increase in performance came at the cost of a slight reduction in altitude compared to the M-105P. For series production, which began in 1942, the piston pins were strengthened, the crankshaft and ďother assemblies were reworked. This modification was characterized by its ease of mass production.
During World War II, approximately 91,000 M-105 engines of various modifications were produced, of which 28,000 were of the M-105PF version.
It was mounted on LavochkinLaGG-3, Yakovlev Yak-1, Petlyakov Pe-2, Yakovlev Yak-7, Gorbunov "105" and ďothers.
sources:
www.klimov.ru
ВК-105ПФ (М-105ПФ)
- in-line piston engine
The M-105PF engine, from 1943 designated VK-105PF after the name of its designer, was a liquid-cooled twelve-cylinder piston engine with V-cylinders, designed in the V.J.It was a modification of the M-105P engine (ОКБ В.Я.Климова), specifically to increase its power. Hence the F designation after the engine number, which stands for Forsirovanyj (Фоорсироованный), i.e., with increased power. The substantial increase in performance came at the cost of a slight reduction in altitude compared to the M-105P. For series production, which began in 1942, the piston pins were strengthened, the crankshaft and ďother assemblies were reworked. This modification was characterized by its ease of mass production.
During World War II, approximately 91,000 M-105 engines of various modifications were produced, of which 28,000 were of the M-105PF version.
It was mounted on LavochkinLaGG-3, Yakovlev Yak-1, Petlyakov Pe-2, Yakovlev Yak-7, Gorbunov "105" and ďothers.
sources:
www.klimov.ru
Reklama
VK-105PF with 20 mm kanónom ŠVAK umiestneným between blokmi motora and strieľajúcim cez dutú os of the propeller..
Diskuse
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Reklama
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avia.academic.ru
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Inak máš na mysli TÚTO knihu - https://www.valka.cz/-t20517 ? Kolegovia si ju pred rokmi nevedeli vynachváliť.
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Triumph and tragedy - Dymič, V .; Šedivý, M.
Page 99 above reads: "In 1941, a group of designers (AE Nudelman, AS Suranov, ... under the leadership of AE Nudelman and AS Suranov, designed the NS-37 air cannon ... Constructor AE Nudelman was arrested soon after and later executed. "
"The continuation of this successful design was the air cannon OKB-16-45 (sometimes incorrectly referred to as NS-45, Nudelman already as a prisoner participated in the design work in the development of this weapon, but was accepted into service only after his death)."
On page 103 below, it reads: "In 1935, Nazarov worked on the introduction of series production of the Gnome-Rhone Mistral Major licensed engine, an 626 kW air-cooled two-star fourteen-cylinder ... Nazarov was arrested at the end of the year while completing the M-88A engine. and executed. OKB Plant No. 29 was then started by CIAM employee Konstantin Tumansky. "
On the other hand, what I read about the engines for Soviet fighters, it fits, because I have verified it in other books, encyclopedias of aircraft, wikipedia and also here.
Page 99 above reads: "In 1941, a group of designers (AE Nudelman, AS Suranov, ... under the leadership of AE Nudelman and AS Suranov, designed the NS-37 air cannon ... Constructor AE Nudelman was arrested soon after and later executed. "
"The continuation of this successful design was the air cannon OKB-16-45 (sometimes incorrectly referred to as NS-45, Nudelman already as a prisoner participated in the design work in the development of this weapon, but was accepted into service only after his death)."
On page 103 below, it reads: "In 1935, Nazarov worked on the introduction of series production of the Gnome-Rhone Mistral Major licensed engine, an 626 kW air-cooled two-star fourteen-cylinder ... Nazarov was arrested at the end of the year while completing the M-88A engine. and executed. OKB Plant No. 29 was then started by CIAM employee Konstantin Tumansky. "
On the other hand, what I read about the engines for Soviet fighters, it fits, because I have verified it in other books, encyclopedias of aircraft, wikipedia and also here.
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