CN205025809U - Turbine compressor unit's novel lubricating oil system - Google Patents
Turbine compressor unit's novel lubricating oil system Download PDFInfo
- Publication number
- CN205025809U CN205025809U CN201520654333.6U CN201520654333U CN205025809U CN 205025809 U CN205025809 U CN 205025809U CN 201520654333 U CN201520654333 U CN 201520654333U CN 205025809 U CN205025809 U CN 205025809U
- Authority
- CN
- China
- Prior art keywords
- base
- oil system
- compressor unit
- supporting seat
- bearing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model relates to a novel lubricating oil system that turbine compressor unit used, its characterized in that: the square ring spare that the base was formed by a plurality of bearing H -beams and a plurality of apron fixed connection, the oil tank is fixed in the inside of base, and oily ystem installation is surface department on the base, on the bearing H -beam of base upper surface, be equipped with fan supporting seat, gear box supporting seat and motor supporting seat, fan, gear box, motor are installed respectively on the fan supporting seat, gear box supporting seat and the motor supporting seat that correspond. This lubricating oil system, compact structure, little, systematic high, the simple to operate of intensity of area to the inside problem that is difficult to fixed connection of oil tank has been solved. Along with the miniaturized development trend of compressor unit, should prize the mainstream configuration that dress formula lubricant station will become small -size compressor unit gradually.
Description
Technical field
The utility model relates to turbo compressor machine technology, specifically the lubrication system new technology of turbo compressor unit.
Background technique
With the centrifugal or Axial Flow Compressor of steam turbine or motoring, be called for short turbo compressor unit.Turbo compressor unit is a kind of dynamic compressors with high-speed rotating impeller, is widely used in conveying air or other gas, and improves its pressure, have the advantages that running efficiency is high, energy consumption is low, good in economic efficiency.
In turbo compressor unit, lubricating oil system is the indispensable auxiliary system for turbo compressor unit each lubricating point fuel feeding, and this lubricating oil system is primarily of fuel tank and the composition such as base, oil system.Each compressor auxiliary equipment is positioned on base, forms a complete compressor bank by parts such as fuel tank, oil system, compressors.Tradition fuel tank is square or bulge, the cushion block usually having band silk hole to fix in bottom, is used for connecting.Base is one piece of flat board meeting intensity that welded steel becomes, and fuel tank is positioned on base and is connected with base by bolt or welding.Tradition fuel tank, base and turbine set placement location are comparatively far away, and middle by the connection of longer pipeline, fuel tank is bolted on base; Oil system is a general designation of the parts such as pump, cooler, oil purifier, valve, pipeline, on stent support and base.Traditional lubricating oil system and unit bay are comparatively far away, and base integration is poor, arranges loose, and take up room large, lubricant oil need by a large amount of pipeline transmission, and unit moves integrally inconvenience.
Summary of the invention
In order to solve, lubricating oil system skid base level of integration in existing turbine installation is not high, intensity difference, fuel tank internal are not easy to fix, move integrally the problems such as inconvenience, the purpose of this utility model is: provide a kind of integration good, structural strength is high, be convenient to mobile, installation and maintenance are novel lubricating oil system easily.
the technical solution adopted in the utility model is:
The lubricating oil system of this turbo compressor unit, comprising: fuel tank 1, base 2, load-bearing I-shape beam 6, oil system 7, blower fan 8, gear-box 9 and motor 10; It is characterized in that:
The frame structure that base 2 is encircled a city for welded steel ] be formed by fixedly connecting with multiple cover plate 11 by multiple load-bearing I-shape beam 6, cover plate 11 is spliced into the upper surface of base by load-bearing I-shape beam 6.
Turbo compressor unit is positioned on this base.
Fuel tank 1 is fixed on the inside of base 2-fuel tank and base are united two into one, and more traditional petrol station more saves space; Oil system 7 is arranged on surface on base 2-so structure, both meets operating conditions, and additionally reduces delivery stroke, and reduced duct pressure loss.
On the load-bearing I-shape beam 6 of base 2 upper surface, be provided with blower fan supporting base 3, gear-box supporting base 4 and motor supporting base 5; Blower fan 8, gear-box 9, motor 10 are arranged on corresponding blower fan supporting base 3, gear-box supporting base 4 and motor supporting base 5 respectively.
The beneficial effect of this lubricating oil system is:
1. the parts that in the unit such as blower fan, gear-box, motor, weight is larger are by the supporting base on the load-bearing I-shape beam of base upper surface, weight is directly delivered to ground, reduce unit weight to the pressure of whole skid susceptor surface, make the intensity optimization of whole skid base, meet the requirement of strength of overall unit operation.
2. load-bearing I-shape beam and cover plate adopt different thickness of slab to interfix, and play guarantee effect to the overall tightness of fuel tank, reduce the generation of fuel tank leakage of oil; Solve the problem that fuel tank internal cannot carry out welding.
3. oil system is directly arranged in skid submounts and is connected with each oil-feeding points of unit, reduces lubricant oil stroke, and reduce pressure loss, minimizing takes up room.
4. the lubricating oil system skid base of this turbo compressor unit, is integrated base, is applicable to the turbo compressor unit of various different technologies requirement.
Below in conjunction with drawings and Examples, the utility model is described further.
Accompanying drawing explanation
Fig. 1. be overall shape, the structural representation of the skid lubricating oil system of the present embodiment;
Fig. 2. be the shape of the base of the present embodiment, structural representation;
Fig. 3. be the bedframe structural drawing of the present embodiment;
Fig. 4. be the load-bearing structural I-beam schematic diagram of the present embodiment;
Fig. 5. be the connection diagram between the load-bearing structural I-beam of the present embodiment and cover plate.
In figure: 1. fuel tank; 2. base; 3. blower fan supporting base; 4. gear-box supporting base; 5. motor supporting base; 6. load-bearing I-shape beam; 7. oil system; 8. blower fan; 9. gear-box; 10. motor; 11. cover plates.
Embodiment
The novel lubricating oil system of a kind of turbo compressor unit of embodiment
fig. 1show shape, structure that the skid lubricating oil system of the present embodiment is overall
Blower fan supporting base 3, gear-box supporting base 4, motor supporting base 5, oil system 7, cover plate 11 are welded in base 2 upper surface; Blower fan 8, gear-box 9, motor 10 are installed on the supporting base that base 2 upper surface corresponds respectively.
fig. 2the shape of the base of the present embodiment, structural drawing
Base 2 is welded with multiple cover plate 11 by multiple load-bearing I-shape beam 6.Cover plate 11 by with the welding of load-bearing structural I-beam 6 one side, complete the integrity of whole base upper surface;
It is inner that fuel tank 1 is welded in base 2; Blower fan supporting base 3, gear-box supporting base 4, motor supporting base 5, oil system 7, cover plate 11 are welded in base 2 upper surface; Blower fan 8, gear-box 9, motor 10 are installed on the supporting base that base 2 upper surface corresponds respectively.
Oil system 7 is arranged on the upper surface of base 2.
fig. 3it is the bedframe structural drawing of the present embodiment
The frame structure surrounded by riser and transverse slat material.
fig. 4the structure of the load-bearing I-shape beam of display the present embodiment
Load-bearing I-shape beam 6 welds integrally welded with base 2, cover plate 11.
fig. 5connection between the load-bearing I-shape beam of display the present embodiment and cover plate
Load-bearing I-shape beam (6) and cover plate (11) one side are spelled integrally welded.
Claims (1)
1. the novel lubricating oil system of turbo compressor unit, comprising: fuel tank (1), base (2), load-bearing I-shape beam (6), oil system (7), blower fan (8), gear-box (9) and motor (10); It is characterized in that:
Base (2) is the square ring that a surrounding stave sheet fences up, and be formed by fixedly connecting by multiple load-bearing I-shape beam (6) and multiple cover plate (11), cover plate (11) is spliced into the upper surface of base by load-bearing I-shape beam (6);
Turbo compressor unit is positioned on base (2);
Fuel tank (1) is fixed on the inside of base (2); Oil system (7) is arranged on surface on base (2);
On the load-bearing I-shape beam (6) of base (2) upper surface, be provided with blower fan supporting base (3), gear-box supporting base (4) and motor supporting base (5); Blower fan (8), gear-box (9), motor (10) are arranged on corresponding blower fan supporting base (3), gear-box supporting base (4) and motor supporting base (5) respectively.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520654333.6U CN205025809U (en) | 2015-08-28 | 2015-08-28 | Turbine compressor unit's novel lubricating oil system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520654333.6U CN205025809U (en) | 2015-08-28 | 2015-08-28 | Turbine compressor unit's novel lubricating oil system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205025809U true CN205025809U (en) | 2016-02-10 |
Family
ID=55258347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201520654333.6U Active CN205025809U (en) | 2015-08-28 | 2015-08-28 | Turbine compressor unit's novel lubricating oil system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205025809U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108797777A (en) * | 2018-05-10 | 2018-11-13 | 西安长庆科技工程有限责任公司 | A kind of environment-friendly and energy-efficient sledge seat |
-
2015
- 2015-08-28 CN CN201520654333.6U patent/CN205025809U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108797777A (en) * | 2018-05-10 | 2018-11-13 | 西安长庆科技工程有限责任公司 | A kind of environment-friendly and energy-efficient sledge seat |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP2017158246A (en) | Generator, foundation base for generator, and maintenance method for generator | |
CN104564717B (en) | Direct driven high-speed turbine vacuum pump and operation method thereof | |
CN105121792A (en) | Lifting tool for rotary shaft and lifting method for rotary shaft | |
CN103291738A (en) | Journal bearing device | |
CN102840142B (en) | The multi-stage shield pump that a kind of motor is put | |
CN205025809U (en) | Turbine compressor unit's novel lubricating oil system | |
CN202914322U (en) | Multi-stage canned pump with motor arranged on upper portion | |
CN104009578B (en) | Vertical asynchronous machine high thrust derivation shaft bearing structure | |
CN207064349U (en) | A kind of hydraulic pump station | |
CN2937487Y (en) | Floor-mounted setting structure for turbine low pressure inner cylinder | |
CN201025222Y (en) | Push force bearing cooling structure for vertical water wheel generation unit | |
CN202955024U (en) | Long-axis pump with reverse auxiliary impeller | |
CN201982581U (en) | Hydraulic motor combined power transmission mechanism and hydraulic water pump | |
CN205297954U (en) | Steel pump electromotor | |
CN201187456Y (en) | Large-scale vertical water pump for factory of nuclear power station | |
CN205026326U (en) | Supplementary atmospheric pressure support sled of LNG plunger pump | |
CN203603988U (en) | Lubricating oil double-tank system arranged in high-low mode | |
CN206636721U (en) | The frame of reciprocating compressor and there is its reciprocating compressor | |
CN201934348U (en) | Gear speeding-up compressor unit for 20000 air separating device | |
CN205534152U (en) | Axle center height -adjustable's gear box bearing structure | |
CN106337775A (en) | Multi-dimensional floating block type sea wave power generation device | |
CN206309615U (en) | A kind of small-sized efficient centrifugal compressor | |
CN207930582U (en) | Multistage fuel pump assembling tool | |
CN201003383Y (en) | Hydraulic lifting device for oil well operation under pressure | |
CN216842258U (en) | Large-scale low-noise anti-vibration constant-stability water intake pump ship |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |