BDP-2A BDP-2B GYRO HORIZON
ZUX-6B FUEL QUANTITY INDICATOR ZUX-6B
(1) The input speed is general n, or less than 1500r/min (2) The speed of the gears is not greater than 20 m/s. (3) Working environment - 40 ~ 50 , the mouth is lower than 0 , before the start of lubricating oil should be preheated to 0above, the speed reducer can be used in positive and negative two directions. Characteristics: (1) The center distance, the main parameters such as the transmission ratio are optimized, the main zero and the parts are interchangeable. (2) The gears are made of high quality alloy steel, which is hardened by carburizing and hardening, and the hardness of the teeth is called hrc54-62. (3) Small size, light weight, high precision, high bearing capacity, high efficiency, long life, high reliability, stable transmission and low noise. (4) The oil pool is normally used for cooling, and when the heat power is not satisfied, the cooling coil can be cooled by circulating oil lubrication or fan. Model Marking Example: Main Types & Models: 1. DBY Type Two-stages Transmission Harden Gear Bevel Cylindrical Gear Reducer Models: -With Solid Output Shaft: DCY160, DCY180, DCY200, DCY224, DCY250, DCY280, DCY315, DCY355, DCY400, DCY450, DCY500, DCY560 -With Hollow Output Shaft: DCYK160, DCYK180, DCYK200, DCYK224, DCYK250, DCYK280, DCYK315, DCYK355, DCYK400, DCYK450, DCYK500, DCYK560 2. DCY Type Three-stages Transmission Harden Gear Bevel Cylindrical Gear Reducer Models: -With Solid Output Shaft: DCY160, DCY180, DCY200, DCY224, DCY250, DCY280, DCY315, DCY355, DCY400, DCY450, DCY500, DCY560, DCY630, DCY710, DCY800 -With Hollow Output Shaft: DCYK160, DCYK180, DCYK200, DCYK224, DCYK250, DCYK280, DCYK315, DCYK355, DCYK400, DCYK450, DCYK500, DCYK560, DCYK630, DCYK710, DCYK800 Application: This product is widely applied to fields of metallurgy, mines, hoisting, transportation, cement, architecture, chemical, textile, printing, dyeing and pharmaceutical etc.
Power Range: 4â??6000 KW Transmission Ration Range: 1.25â??450 Output Torque: top to 950 Kn.m Characteristics: Design 1.) Highly standard modular designed, more sizes with a reduced variety of parts. 2.) Higher operational reliability combined with increased power capacity. Mounting position The gear units can be supplied for either horizontal or vertical installation. Other arrangements are also possible on request. Long service life Under the condition of accurately s electing type size and the normal maintenance and use, main components (expect those easily-disabled) can last as long as up to more than 50,000 hours. Low noise All key components are finished by precisely machining; grinding the gears; designing noise-absorbing housings; accurate assembly, and finally tested, and therefore, fairly low noise is reached. Thermal conduction 1.) The gear units have a high efficiency. 2.) Through enlarged housing surface areas. 3.) Because large fans incorporating a new type of air conduction fan cowl are being used.
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Supply of China aircraft parts
Model NO.: TJ-684582 Color: Natural Color Type: Steering Gears/Shaft Auto: Automatic Applicable: Marine Trademark: TJ HS Code: 8483 Condition: New Certification: ISO, Ts16949 Material: Alloy The Delivery Time: 30-45days Transport Package: Carton, Pallet Origin: China
Our company was established in 1998 as a professional manufacturer of precise planetary gearbox,actuator and motorized pulleys etc.And our head office is in shanghai city,the factory is in dandong city ,liaoning province. The factory total covers about an area of 1000 square meters,and we can supply about ten thousand pcs gearbox every month,and about two hundred thousand pcs every year. And now we have 4 products series, our core business: gearbox; second: gearmotor, and then the actuator ,and others relevant drive & control products.
Housing stainless steel Pinion steel Output shaft alloy steel Output flange aluminum Bearing at output ball bearing Permissible motor speed 15,000 rpm Max. permissible radial load =5N Max. permissible axial load =5N Max. permissible force for press fits =20N Radial play =0.01mm Axial play =0.01mm Recommended temperature range -40 to +125?
Inion Steel output shaft stainless steel Output flange Aluminum bearing at output ball bearing Permissible motor speed 6, 000 rpm max. Permissible radial load =20n Max. Permissible axial load =20n max. Permissible force for press fits =100n Radial play =0.04mm axial play =0.04 mm Recommended temperature range -25 to +125?
Various kinds of Gearbox with different Ratio.
GICLZ Type Drum Gear Coupling Drum Gear Coupling · Model: GICLZ Type · Norminal Torque: 0.8kN. M - 3500kN. M · Allowed Rotation Sppeed: 7100rpm - 700rpm · Connection: Keyway & Shaft hole · Shaft Hole Diameter: 16mm - 600mm · Shaft Hole Length (Y): 42mm - 900mm · GEAR COUPLING Applications: Metallurgy, mining, lifting and transportation industries, petroleum, chemical, general machinery and other heavy machinery shaft drive. GICLZ-type drum gear coupling has improved the internal and external contact conditions, which avoids the drawbacks of angular displacement of the mandibular tooth edge extrusion and stress concentration, in the meanwhile improves the tooth surface friction, wear conditions, reducing noise, long maintenance cycle. The tooth end of outer teeth set is horn shape, so that the internal and external tooth assembly and disassembly is very convenient. Drum-type Gear Coupling Features (compared with the straight-type coupling): 1. High carrying capacity The bearing capacity of the drum-type gear coupling is 15 to 20% higher than that of the straight-type coupling in the same outer diameter and the maximum outer diameter of the coupling. 2. Large angular displacement compensation When the radial displacement is equal to zero, the allowable angular displacement of the straight-tooth coupling is 1°, but the allowable angular displacement of the drum gear-type coupling is 1°30", 50% increased. With the same modulus, tooth number, tooth width, the allowable angular displacement of the drum teeth is larger than of the straight teeth. 3. Drum-type gear surface has improved the internal and external contact conditions, which avoids the drawbacks of angular displacement of the mandibular tooth edge extrusion and stress concentration, in the meanwhile improves the tooth surface friction, wear conditions, reducing noise, long maintenance cycle. 4. The tooth end of outer teeth set is horn shape, so that the internal and external tooth assembly and disassembly is very convenient. 5. Transmission efficiency is up to 99.7%. Huading design and production the Flexible Coupling, Flexible Pin Coupling, Flexible Bush Coupling, Star Type Coupling, Tire Coupling, Plum Coupling, Grid Coupling, Diaphragm Coupling etc. With strictly quality control and excellent performance.
OFFROAD Vehicles Front & Rear Ring and pinion gear for Jimny,Jeep Rubicon & Sahara,Nissan Y60 Y61,Toyota ,Isuzu,Mitsubishi
Type : planetary, helical, worm Orientation : horizontal, vertical Mounting : foot, flange Input (rpm or ratio) : 750-1500 rpm Output torque (nm) : 20-300 rpm Brand : roadcon Material : cast iron, steel and bronze Application : industrial use Condition : new Power source : 5 hp to 125 hp Voltage (v) : 220v Gear tooth geometry design combines maximum efficiency with high load carrying capacity and minimal noise generation. Serviceability of the product was key in the design of the series h helical gear boxes range allowing easy maintenance for long life and reliability, which are synonymous with our field reputation.
1.Ideal choice for quick tire replacement and simple service alongside of vehicle 2.Surface mounted or movable used, with optional movable kits. 3.Special and practical platform extension design broadens your service scope. 4.Pneumatic release system decreases noise emitted during service work. 5.Configuring mechanical safety decreases noise emitted during service work. 6.Cnfiguring mechanical safety lock to ensure that lift at different heights to get the absolute security 7.Optional 24V control voltage 8.Anti-skid platform effectively prevents sudden drop-down of vehicle 9. Dynamic testing with 115% of rated capacity and static testing with 150% of rated capacity
1.Ideal choice for quick tire replacement and simple service alongside of vehicle 2.Surface mounted or movable used, with optional movable kits. 3.Special and practical platform extension design broadens your service scope. 4.Pneumatic release system decreases noise emitted during service work. 5.Configuring mechanical safety decreases noise emitted during service work. 6.Cnfiguring mechanical safety lock to ensure that lift at different heights to get the absolute security 7.Optional 24V control voltage 8.Anti-skid platform effectively prevents sudden drop-down of vehicle 9. Dynamic testing with 115% of rated capacity and static testing with 150% of rated capacity
The cirrus sr22 is a single-engine four- or five-seat composite aircraft built from 2001 by cirrus aircraft of duluth, minnesota. It is a development of the cirrus sr20, with a larger wing, higher fuel capacity, and a more powerful, 310-horsepower (231 kw) engine. The sr22 has been the world's best-selling general aviation (ga) airplane every year since 2002. It is the most-produced ga aircraft made from composite material, accounting for over 30% of the entire piston aircraft market General characteristics Crew: one Capacity: four passengers Length: 26 ft 0 in (7.92 m) Wingspan: 38 ft 4 in (11.68 m) Height: 8 ft 11 in (2.72 m) Airfoil: roncz Empty weight: 2, 225 lb (1, 009 kg) Gross weight: 3, 600 lb (1, 633 kg) Fuel capacity: 92 us gallons (348 litres) Powerplant: 1 continental io-550-n six cylinder horizontally opposed aircraft engine, 310 hp (230 kw) Propellers: 3-bladed Performance Cruise speed: 183 kn (211 mph; 339 km/h) Stall speed: 60 kn (69 mph; 111 km/h) flaps down Range: 1, 049 nmi (1, 207 mi; 1, 943 km) with reserves at 65% power Service ceiling: 17, 500 ft (5, 300 m) Rate of climb: 1, 270 ft/min (6.5 m/s)
The robinson r22 is a two-bladed, single-engine light utility helicopter manufactured by robinson helicopter company. The two-seat r22 was designed in 1973 by frank robinson and has been in production since 1979. General characteristics Crew: 1 Capacity: 2, including pilot Length: 28 ft 8 in (8.74 m) Rotor diameter: 25 ft 2.4 in (7.67 m) Tail rotor diameter: 3 ft 6 in (1.07 m) Height: 8 ft 11 in (2.72 m) Disc area: 497 (46.2 m) Empty weight: 880 lb (399 kg[23]) Loaded weight: 920 lb (417 kg) Max. Takeoff weight: 1, 370 lb (635 kg) Main tank total capacity: 19.8 us gallons (75 liters) Main tank usable capacity: 19.2 us gallons (73 liters) Optional aux tank total capacity: 10.9 us gallons (41 liters) Optional aux tank usable capacity: 10.5 us gallons (40 liters) Powerplant: 1 ã? lycoming o-320-a2b or -a2c flat 4 piston engine, 124 hp (93 kw) Performance Never exceed speed: 117 mph, 188 km/h, 102 kts Cruise speed: 110 mph, 177 km/h, 96 kts Range: 240 mi (386 km) Service ceiling: 14, 000 ft (4, 267 m) Rate of climb: 1, 200 ft/min (6.1 m/s) Disc loading: 2.61 lb/ (13.7 kg/m) Fuel consumption: 8~10 us gal/hr Power/mass: 0.095 hp/lb (0.147 kw/kg) Endurance: approx. 3 hours, with 30-minute reserve
The cessna citation mustang, model 510, is a very light jet (vlj) class business jet built by cessna aircraft company at their independence, kansas production facility. The mustang, in standard configuration, has four passenger seats in the aft cabin, a toilet, and seating for two in the cockpit. Like most other light jets, the mustang is approved for single-pilot operation. General characteristics Crew: one or two pilots Capacity: 4 to 5 passengers Length: 40 feet 7 inches (12.37 m) Wingspan: 43 feet 2 inches (13.16 m) Height: 13 feet 5 inches (4.09 m) Empty weight: 5600 lb (2540 kg) Useful load: 3130 lb (1420 kg) Max. Takeoff weight: 8645 lb (3930 kg) Powerplant: 2 pratt & whitney canada pw615f turbofans, 1460 lb thrust (6.49 kn) each Performance Maximum speed: mach 0.63 (483 mph, 777 km/h) Cruise speed: 340 ktas (390 mph, 630 km/h) Range: 1167 nmi (at max. Takeoff weight) (1, 343 mi, 2, 161 km) Service ceiling: 41000 ft (12500 m) Rate of climb: 3010 fpm (917 mpm) Thrust/weight: 0.337 (at max. Takeoff weight) Takeoff distance: 3, 110 ft (948 m) Landing distance: 2, 380 ft (729 m)
