RF-8-GAZ-98
General characteristics
& amp; nbsp; & amp; nbsp; & amp; nbsp; Two-seat offensive armored airships used by the Soviet Army during World War II. war and shortly after.
Description
& amp; nbsp; & amp; nbsp; & amp; nbsp; The sleigh had an elongated narrow, aerodynamically shaped hull open from above. It was manufactured as a fuselage - a total of 15 bulkheads, connected by side members. The unit was covered with plywood. Partitions No. 12 - 15 were transferred to a pylon with a reinforced bed, carrying a motor unit with a propeller. The hull floor was made of thick plywood. The force points carrying the hinges of the half-axles and shock absorbers were made of steel, fixed to the fuselage by screws and washers. A large car headlight was placed on the bow. The RF-8 rested on four rails, the front two of which were steerable. The suspension of the front and rear skis was independent, created as a welded sheet metal pyramid with a flange for mounting the skis on a semi-axle with legs with spring dampers, reinforced by another horizontal strut to the fuselage. The attachment of the hinge to the force points on the fuselage was done using articulated joints. the skis were fitted with brakes. These formed steel pins. passing through guide tubes and controlled by a cable transmission from the driver's pedal.
& amp; nbsp; & amp; nbsp; & amp; nbsp; Skis - mixed designs, flat, rectangular in shape. They consisted of a wooden body continuously curved at the front, with a plywood cover from above and below, and a rim of metal profiles. Metal skids were attached to the bottom, on which there were longitudinal metal rails for better driving characteristics. On the upper side of the ski, approximately in the middle of their length, was a sheet metal welded pyramid with a sleeve for threading on the semi-axle of the hinge. The pyramid was provided with a hem bent at the bottom, which was attached to the body of the ski with flat-head screws. The front and rear skis were identical, but the rear pyramid had a bracket welded to the rear to accommodate a swinging brake lever and a vertically positioned brake pin guide tube. Eyelets were welded from the side around the case at the back of the pyramid. On them, mounted on a pivoting hinge, see the guide pulley of the brake cable, which was connected to the swing handle by a fork with a clutch and a thread for regulating the tension of the cable. The traction of the aircraft propeller and the braking of the aerosani made it possible to control the speed of movement.
& amp; nbsp; & amp; nbsp; & amp; nbsp; The front skis were rope. There was a grooved drum on the steering rod, on which the rope was wound on one side and unwound on the other by turning the steering wheel. This was guided by a system of pulleys to control the skis. This was done by a similar drum placed on a steering rod connecting the two skis. It then swerved to the right or left.
& amp; nbsp; & amp; nbsp; & amp; nbsp; Two crew members sat in the fuselage behind each other in separate rooms. In front was the shooter behind him, the driver. This arrangement, similar to the first two-seater fighters from the 1st Vol. v., should allow the shooter to control as much shot space as possible. Both men protruded from the open body from the open torso, the driver wearing protective glass in front of him. A metal impeller was mounted around the shooter's station and a DT machine gun was installed on it - & # 1044; & # 1058; ( & # 1044; & # 1077; & # 1075; & # 1090; & # 1103; & # 1088; & # 1077; & # 1074; & # 1090; & # 1072; & # 1085; & # 1082; & # 1086; & # 1074; & # 1099 ; & # 1081; = Deckarev, tank) caliber 7.62 mm. The circulation of the machine gun was limited to 300 °. This 60 ° restriction made it impossible to aim the weapon backwards at the driver, engine and propeller in the heat of battle. In the horizontal plane, the machine gun moved to 14 ° from the plane. In the bow area was a supply of 10 magazines for machine guns and grenades for possible close combat.
& amp; nbsp; & amp; nbsp; & amp; nbsp; The steering column, accelerator foot pedals, brakes, machine rocking, and more were located in the driver's compartment. The driver controlled the machine using the steering wheel, brake and accelerator pedals. The mentioned rocking pedal of the machine had a special function.When the sledge stood for a long time, the skis often froze to the snow. This special pedal was connected to the ski springs on the right side. A few depresses of the pedal withdrew the springs, the machine tilted slightly to the right and when the springs were released, it bounced and tore off the ground.
& amp; nbsp; & amp; nbsp; & amp; nbsp; An 80-liter fuel tank and a starter battery were stored in the fuselage behind the driver's station. Above them was then placed a power unit - a water-cooled automobile engine GAZ M-1 with a maximum output of 50 horsepower at 2800 rpm. The engine's water-cooling radiator grille rose above the driver's head. Because it was an automobile engine, the 235 cm diameter double-bladed propeller was not attached directly to the crankshaft, but was connected to the engine via a speed reducer. The propeller gave a thrust of 205 - 215 kg To reduce the transmission of vibrations arising during engine operation, it was mounted on rubber dampers. The engine and its accessories were covered by a hood with hinged side panels. A tubular structure covering the space of rotation of the propeller was also attached to the nodal points of anchoring the motor unit. For safety reasons, it was painted bright red. The use of a metal propeller proved to be advantageous even in situations where the machines were forced to overcome areas with bushes, or to move on forest roads, where other types of aerosans were not recommended to enter. Metal propellers were less susceptible to damage from accidental contact with vegetation than wooden propellers used elsewhere.
& amp; nbsp; & amp; nbsp; & amp; nbsp; Between 1942 and 43, brothers AA Beskurnikov and IA Beskurnikov ( & # 1040 ;. & # 1040 ;. & # 1041; & # 1077; & # 1089; & # 1082; & # 1091; & # 1088; & # 1085; & # 1080; & # 1082; & # 1086; & # 1074; & # 1080; & # 1048 ;. & # 1040 ;. & # 1041; & # 1077; & # 1089; & # 1082; & # 1091; & # 1088; & # 1085; & # 1080; & # 1082; & # 1086; & # 1074;), another modified variant of these sledges, referred to as GAZ-98K. An M-11 aircraft engine with an output of 110 hp was installed in them. Although their advantage disappeared, ie the use of less deficient car engines, the sledge gained more dynamic driving characteristics. An unarmed staff modification with a fully covered limousine-type cabin was also derived from this version.
TTD
Crew - 2 men
Length - 5. 11 m
Width - 2, 528 m
Height (including propeller) - 2, 71 m
Weight - 0, 897 t
Cruising speed - 50 km/h
Armament - 1 x machine gun caliber 7, 62 mm and hand grenades.
Sources
extentech.sheetster.com
http://www.search.com/reference/RF-8
http://www.armor.kiev.ua/Tanks/WWII/sani/rf8.htm
http://fr.wikipedia.org/wiki/Aerosan
http://www.battlefield.ru/index.php?option=com
1–kroužek objímky kyvné poloosy přední lyže,2–kyvná poloosa,3–bromzová objímka,
4–kónusové šrouby páky řízení,5–páka řízení,6–kulový čep,7–poloosa s oky pro upevnění tlumiče a vzpěry,8–závěs,9–uzel upevnění na trup,10–vzpěra,11–šroubová regul. koncovka,1
1–zadní lyže,2–brzdový čep,3-závěs páky brzdy,4–páka brzdy,5–vidlička brzdy,6–regulační objímka napnutí brzd. lanka,7–táhlo brzdy,8–kladka brzd. lanka,9–brzdové lanko,10–konzola,11–objímka kyvné poloosy lyže,12–vratná pružina,13–těleso nosníku lyže,14–mat
Asi nejznámější obrázek
Pramen v textu
General characteristics
& amp; nbsp; & amp; nbsp; & amp; nbsp; Two-seat offensive armored airships used by the Soviet Army during World War II. war and shortly after.
Description
& amp; nbsp; & amp; nbsp; & amp; nbsp; The sleigh had an elongated narrow, aerodynamically shaped hull open from above. It was manufactured as a fuselage - a total of 15 bulkheads, connected by side members. The unit was covered with plywood. Partitions No. 12 - 15 were transferred to a pylon with a reinforced bed, carrying a motor unit with a propeller. The hull floor was made of thick plywood. The force points carrying the hinges of the half-axles and shock absorbers were made of steel, fixed to the fuselage by screws and washers. A large car headlight was placed on the bow. The RF-8 rested on four rails, the front two of which were steerable. The suspension of the front and rear skis was independent, created as a welded sheet metal pyramid with a flange for mounting the skis on a semi-axle with legs with spring dampers, reinforced by another horizontal strut to the fuselage. The attachment of the hinge to the force points on the fuselage was done using articulated joints. the skis were fitted with brakes. These formed steel pins. passing through guide tubes and controlled by a cable transmission from the driver's pedal.
& amp; nbsp; & amp; nbsp; & amp; nbsp; Skis - mixed designs, flat, rectangular in shape. They consisted of a wooden body continuously curved at the front, with a plywood cover from above and below, and a rim of metal profiles. Metal skids were attached to the bottom, on which there were longitudinal metal rails for better driving characteristics. On the upper side of the ski, approximately in the middle of their length, was a sheet metal welded pyramid with a sleeve for threading on the semi-axle of the hinge. The pyramid was provided with a hem bent at the bottom, which was attached to the body of the ski with flat-head screws. The front and rear skis were identical, but the rear pyramid had a bracket welded to the rear to accommodate a swinging brake lever and a vertically positioned brake pin guide tube. Eyelets were welded from the side around the case at the back of the pyramid. On them, mounted on a pivoting hinge, see the guide pulley of the brake cable, which was connected to the swing handle by a fork with a clutch and a thread for regulating the tension of the cable. The traction of the aircraft propeller and the braking of the aerosani made it possible to control the speed of movement.
& amp; nbsp; & amp; nbsp; & amp; nbsp; The front skis were rope. There was a grooved drum on the steering rod, on which the rope was wound on one side and unwound on the other by turning the steering wheel. This was guided by a system of pulleys to control the skis. This was done by a similar drum placed on a steering rod connecting the two skis. It then swerved to the right or left.
& amp; nbsp; & amp; nbsp; & amp; nbsp; Two crew members sat in the fuselage behind each other in separate rooms. In front was the shooter behind him, the driver. This arrangement, similar to the first two-seater fighters from the 1st Vol. v., should allow the shooter to control as much shot space as possible. Both men protruded from the open body from the open torso, the driver wearing protective glass in front of him. A metal impeller was mounted around the shooter's station and a DT machine gun was installed on it - & # 1044; & # 1058; ( & # 1044; & # 1077; & # 1075; & # 1090; & # 1103; & # 1088; & # 1077; & # 1074; & # 1090; & # 1072; & # 1085; & # 1082; & # 1086; & # 1074; & # 1099 ; & # 1081; = Deckarev, tank) caliber 7.62 mm. The circulation of the machine gun was limited to 300 °. This 60 ° restriction made it impossible to aim the weapon backwards at the driver, engine and propeller in the heat of battle. In the horizontal plane, the machine gun moved to 14 ° from the plane. In the bow area was a supply of 10 magazines for machine guns and grenades for possible close combat.
& amp; nbsp; & amp; nbsp; & amp; nbsp; The steering column, accelerator foot pedals, brakes, machine rocking, and more were located in the driver's compartment. The driver controlled the machine using the steering wheel, brake and accelerator pedals. The mentioned rocking pedal of the machine had a special function.When the sledge stood for a long time, the skis often froze to the snow. This special pedal was connected to the ski springs on the right side. A few depresses of the pedal withdrew the springs, the machine tilted slightly to the right and when the springs were released, it bounced and tore off the ground.
& amp; nbsp; & amp; nbsp; & amp; nbsp; An 80-liter fuel tank and a starter battery were stored in the fuselage behind the driver's station. Above them was then placed a power unit - a water-cooled automobile engine GAZ M-1 with a maximum output of 50 horsepower at 2800 rpm. The engine's water-cooling radiator grille rose above the driver's head. Because it was an automobile engine, the 235 cm diameter double-bladed propeller was not attached directly to the crankshaft, but was connected to the engine via a speed reducer. The propeller gave a thrust of 205 - 215 kg To reduce the transmission of vibrations arising during engine operation, it was mounted on rubber dampers. The engine and its accessories were covered by a hood with hinged side panels. A tubular structure covering the space of rotation of the propeller was also attached to the nodal points of anchoring the motor unit. For safety reasons, it was painted bright red. The use of a metal propeller proved to be advantageous even in situations where the machines were forced to overcome areas with bushes, or to move on forest roads, where other types of aerosans were not recommended to enter. Metal propellers were less susceptible to damage from accidental contact with vegetation than wooden propellers used elsewhere.
& amp; nbsp; & amp; nbsp; & amp; nbsp; Between 1942 and 43, brothers AA Beskurnikov and IA Beskurnikov ( & # 1040 ;. & # 1040 ;. & # 1041; & # 1077; & # 1089; & # 1082; & # 1091; & # 1088; & # 1085; & # 1080; & # 1082; & # 1086; & # 1074; & # 1080; & # 1048 ;. & # 1040 ;. & # 1041; & # 1077; & # 1089; & # 1082; & # 1091; & # 1088; & # 1085; & # 1080; & # 1082; & # 1086; & # 1074;), another modified variant of these sledges, referred to as GAZ-98K. An M-11 aircraft engine with an output of 110 hp was installed in them. Although their advantage disappeared, ie the use of less deficient car engines, the sledge gained more dynamic driving characteristics. An unarmed staff modification with a fully covered limousine-type cabin was also derived from this version.
TTD
Crew - 2 men
Length - 5. 11 m
Width - 2, 528 m
Height (including propeller) - 2, 71 m
Weight - 0, 897 t
Cruising speed - 50 km/h
Armament - 1 x machine gun caliber 7, 62 mm and hand grenades.
Sources
extentech.sheetster.com
http://www.search.com/reference/RF-8
http://www.armor.kiev.ua/Tanks/WWII/sani/rf8.htm
http://fr.wikipedia.org/wiki/Aerosan
http://www.battlefield.ru/index.php?option=com
Period | - |
Type | - |
Camouflage | - |
Country | - |
Production No. | - |
Poznávací značka / evidenční číslo | - |
Tactical marking | - |
Name | - |
Unit | - |
Date (DD.MM.RRRR) | - |
Author | - |
Print size / 300 DPI | - |
Published with authors permit | - |
Author Website | - |
1–kroužek objímky kyvné poloosy přední lyže,2–kyvná poloosa,3–bromzová objímka,
4–kónusové šrouby páky řízení,5–páka řízení,6–kulový čep,7–poloosa s oky pro upevnění tlumiče a vzpěry,8–závěs,9–uzel upevnění na trup,10–vzpěra,11–šroubová regul. koncovka,1
Period | - |
Type | - |
Camouflage | - |
Country | - |
Production No. | - |
Poznávací značka / evidenční číslo | - |
Tactical marking | - |
Name | - |
Unit | - |
Date (DD.MM.RRRR) | - |
Author | - |
Print size / 300 DPI | - |
Published with authors permit | - |
Author Website | - |
1–zadní lyže,2–brzdový čep,3-závěs páky brzdy,4–páka brzdy,5–vidlička brzdy,6–regulační objímka napnutí brzd. lanka,7–táhlo brzdy,8–kladka brzd. lanka,9–brzdové lanko,10–konzola,11–objímka kyvné poloosy lyže,12–vratná pružina,13–těleso nosníku lyže,14–mat
Period | - |
Type | - |
Camouflage | - |
Country | - |
Production No. | - |
Poznávací značka / evidenční číslo | - |
Tactical marking | - |
Name | - |
Unit | - |
Date (DD.MM.RRRR) | - |
Author | - |
Print size / 300 DPI | - |
Published with authors permit | - |
Author Website | - |
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