WO2018123405A1 - 回転機械 - Google Patents

回転機械 Download PDF

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Publication number
WO2018123405A1
WO2018123405A1 PCT/JP2017/042768 JP2017042768W WO2018123405A1 WO 2018123405 A1 WO2018123405 A1 WO 2018123405A1 JP 2017042768 W JP2017042768 W JP 2017042768W WO 2018123405 A1 WO2018123405 A1 WO 2018123405A1
Authority
WO
WIPO (PCT)
Prior art keywords
bearing
casing
rotary machine
outer ring
bearing box
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.)
Ceased
Application number
PCT/JP2017/042768
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
毅 金子
大谷　雄一
潤 宮本
長谷川　泰士
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Thermal Systems Ltd
Original Assignee
Mitsubishi Heavy Industries Thermal Systems Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Thermal Systems Ltd filed Critical Mitsubishi Heavy Industries Thermal Systems Ltd
Priority to CN201780079916.2A priority Critical patent/CN110100105B/zh
Priority to US16/472,102 priority patent/US20200096043A1/en
Publication of WO2018123405A1 publication Critical patent/WO2018123405A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/66—Special parts or details in view of lubrication
    • F16C33/6637—Special parts or details in view of lubrication with liquid lubricant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/52—Bearings with rolling contact, for exclusively rotary movement with devices affected by abnormal or undesired conditions
    • F16C19/525—Bearings with rolling contact, for exclusively rotary movement with devices affected by abnormal or undesired conditions related to temperature and heat, e.g. insulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/54—Systems consisting of a plurality of bearings with rolling friction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/66—Special parts or details in view of lubrication
    • F16C33/6637—Special parts or details in view of lubrication with liquid lubricant
    • F16C33/6659—Details of supply of the liquid to the bearing, e.g. passages or nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/042—Housings for rolling element bearings for rotary movement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/07—Fixing them on the shaft or housing with interposition of an element
    • F16C35/077—Fixing them on the shaft or housing with interposition of an element between housing and outer race ring
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C37/00—Cooling of bearings
    • F16C37/007—Cooling of bearings of rolling bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2202/00—Solid materials defined by their properties
    • F16C2202/20—Thermal properties

Definitions

  • the present invention relates to a rotating machine.
  • Priority is claimed on Japanese Patent Application No. 2016-251470, filed Dec. 26, 2016, the content of which is incorporated herein by reference.
  • the rotary machine includes a bearing that rotatably supports a rotary body such as a rotary shaft.
  • the bearing has an inner ring disposed on the rotating body side, an outer ring disposed outside the inner ring, and a plurality of rolling elements interposed between the inner ring and the outer ring.
  • the inner ring is fixed to the rotating body.
  • the outer ring is fixed to the bearing box.
  • the bearing box is housed in a casing.
  • the heat of the outer ring is easily radiated through the bearing box and the casing, but the heat of the inner ring is hardly radiated.
  • the clearance of the bearing during operation may decrease due to the difference in thermal expansion between the inner ring and the outer ring, and the life of the bearing may be reduced. was there.
  • the service life of the bearing is significantly reduced.
  • Patent Document 1 discloses that the axial length of the relief is adjusted to be larger than the axial length of the crowning portion in order to suppress the temperature rise of the inner ring which is inferior in heat dissipation.
  • Patent Document 1 is difficult and difficult to adjust.
  • an object of this invention is to provide the rotary machine which can suppress the fall of the lifetime of a bearing simply.
  • a rotary machine comprises a rotating body, an inner ring fixed to the outer peripheral surface of the rotating body, an outer ring disposed outside the inner ring, and the inner ring and the outer ring A bearing including a plurality of rolling elements interposed therebetween, a bearing box disposed outside the bearing, and a bearing box to which the outer ring is fixed, and a bearing box disposed outside the bearing box; And a temperature difference suppressing mechanism for reducing the difference between the temperature of the outer ring and the temperature of the inner ring.
  • the difference in thermal expansion between the inner ring and the outer ring can be reduced by providing the temperature difference suppressing mechanism that reduces the difference between the temperature of the outer ring and the temperature of the inner ring.
  • the temperature difference suppressing mechanism that reduces the difference between the temperature of the outer ring and the temperature of the inner ring.
  • the temperature difference suppression mechanism may include a recess provided in a portion of the casing in contact with the outer peripheral surface of the bearing housing.
  • the temperature difference suppression mechanism includes a heat insulating material provided on the outer surface of the casing, and the bearing box injects lubricating oil to the bearing. You may have a part.
  • the heat insulating material on the outer surface of the casing, the contact between the casing and the outside air can be suppressed, and the heat of the rotary machine can be kept inside the heat insulating material.
  • the temperature decrease of the outer ring is suppressed, and the difference in thermal expansion between the inner ring and the outer ring can be reduced, so that the reduction of the life of the bearing can be suppressed.
  • the bearing with the lubricating oil injection portion for injecting the lubricating oil, it is possible to cool the entire bearing using the lubricating oil. As a result, it is possible to suppress a large rise in temperature of the entire bearing.
  • the temperature difference suppressing mechanism may include a low thermal conductivity member disposed between the bearing box and the casing and having a thermoelectric coefficient lower than that of the casing. .
  • the temperature difference suppression mechanism includes a heating element which is disposed between the bearing box and the casing and heats the bearing box, and the bearing box is You may have a lubricating oil injection part which injects lubricating oil to the said bearing.
  • the heating element for heating the bearing case between the bearing case and the casing it becomes possible to heat the outer ring whose temperature is likely to decrease compared to the inner ring. This makes it possible to reduce the difference in thermal expansion between the inner ring and the outer ring, thereby suppressing the reduction in the life of the bearing. Further, by providing the bearing with the lubricating oil injection portion for injecting the lubricating oil, it is possible to cool the entire bearing using the lubricating oil. As a result, it is possible to suppress a large rise in temperature of the entire bearing.
  • the temperature difference suppression mechanism may include the rough surface.
  • the temperature difference suppression mechanism includes the rough surface. Since the contact area between the outer peripheral surface of the housing and the inner peripheral surface of the casing is reduced, it is possible to make it difficult for the heat of the bearing box in contact with the outer ring to be transmitted to the casing. As a result, the temperature decrease of the outer ring is suppressed, and the difference in thermal expansion between the inner ring and the outer ring can be reduced, so that the reduction of the life of the bearing can be suppressed.
  • the rotary machine which can suppress the fall of the lifetime of a bearing simply can be provided.
  • FIG. 1 has shown the axis line (henceforth "the axis line O" of the rotary body 11.
  • a compressor is illustrated as an example of the rotary machine 10.
  • a rotation axis is illustrated as an example.
  • the rotary machine 10 includes a rotating body 11, bearing housings 13 and 15, a plurality of bearings 16, a casing 18, a temperature difference suppression mechanism 19, a support member 21, and a seal member 22.
  • the rotating body 11 has a cylindrical shape, and is disposed to extend in a predetermined direction (the direction of the axis O).
  • the rotating body 11 has a distal end portion 11A, a proximal end portion 11B, and a bearing support portion 11C.
  • the tip end 11A is exposed from one end of the casing 18.
  • the proximal end 11 ⁇ / b> B is accommodated in the casing 18.
  • the proximal end 11 B is a portion rotatably supported by the plurality of bearings 16.
  • the bearing support portion 11C is disposed between the distal end portion 11A and the proximal end portion 11B.
  • the rotating body 11 configured as described above has an outer peripheral surface 11 a.
  • the bearing housing 13 has a bearing housing 27 and a lubricating oil injection unit 28.
  • the bearing box main body 27 is a cylindrical member.
  • the bearing box main body 27 accommodates the bearing support portion 11C in a state in which a gap capable of arranging the bearing 16 is interposed between the bearing case main body 27 and the outer peripheral surface 11a of the bearing support portion 11C.
  • the bearing box main body 27 has an outer peripheral surface 27 a and an outer ring fixing surface 27 b.
  • the outer circumferential surface 27 a is a surface in contact with the casing 18.
  • the outer peripheral surface 27 a is a surface corresponding to the outer peripheral surface 13 a of the bearing housing 13.
  • the outer ring fixing surface 27b is a ring-shaped surface to which the outer ring 16B of the bearing 16 is fixed inside.
  • a plurality of outer ring fixing surfaces 27b are arranged at predetermined intervals in the axial line O direction.
  • the lubricating oil injection unit 28 is provided inside the bearing box main body 27.
  • the lubricating oil injection portion 28 projects in the direction from the inside of the bearing box main body 27 toward the bearing support portion 11C.
  • the lubricating oil injection unit 28 is disposed between the bearings 16.
  • the lubricating oil injection unit 28 is connected to a lubricating oil supply unit (not shown).
  • the lubricating oil injection unit 28 has a function of cooling the entire bearing 16 by injecting the lubricating oil to the bearing 16.
  • the bearing case 15 has a bearing case main body 31 and a lubricating oil injection portion 32.
  • the bearing case main body 31 is a cylindrical member whose one end is a closed end and the other is an open end.
  • the bearing box main body 31 accommodates the base end portion 11B in a state in which a gap capable of arranging the bearing 16 is interposed between the bearing box main body 31 and the outer peripheral surface 11a of the base end portion 11B.
  • the bearing box main body 31 has an outer peripheral surface 31 a and an outer ring fixing surface 31 b.
  • the outer circumferential surface 31 a is a surface in contact with the casing 18.
  • the outer peripheral surface 31 a is a surface corresponding to the outer peripheral surface 15 a of the bearing housing 15.
  • the outer ring fixing surface 31b is a ring-shaped surface to which the outer ring 16B of the bearing 16 is fixed inside.
  • a plurality of outer ring fixing surfaces 31b are arranged at predetermined intervals in the axial line O direction.
  • the lubricating oil injection unit 32 is provided inside the bearing box main body 31.
  • the lubricating oil injection portion 32 protrudes in the direction from the inside of the bearing box main body 31 toward the proximal end portion 11B.
  • the lubricating oil injection unit 32 is disposed between the bearings 16.
  • the lubricating oil injection unit 32 is connected to a lubricating oil supply unit (not shown).
  • the lubricating oil injection unit 32 has a function of cooling the entire bearing 16 by injecting the lubricating oil to the bearing 16.
  • the bearing housings 13 and 15 described above are disposed outside the plurality of bearings 16.
  • a plurality of bearings 16 are provided between the bearing support portion 11C and the bearing box main body 27, and between the base end portion 11B and the bearing box main body 27.
  • the bearing 16 has an inner ring 16A, an outer ring 16B, and a plurality of rolling elements 16C.
  • the inner ring 16A is a ring-shaped member.
  • the inner ring 16A is fixed to the outer peripheral surface 11a of the rotary body 11 facing the outer ring fixing surface 27b or the outer ring fixing surface 31b.
  • the outer ring 16B is a ring-shaped member.
  • the outer ring 16B is fixed to the outer ring fixing surfaces 27b and 31b.
  • the outer ring 16B is disposed outside the inner ring 16A so as to face the inner ring 16A.
  • the plurality of rolling elements 16C are interposed between the inner ring 16A and the outer ring 16B.
  • balls or rollers can be used as the rolling elements 16C.
  • the plurality of bearings 16 configured as described above rotatably support the rotating body 11.
  • the casing 18 is a tubular member.
  • the casing 18 accommodates the rotating body 11 excluding the tip end portion 11A, the bearing housings 13, 15, and the plurality of bearings 16.
  • the casing 18 has inner circumferential surfaces 18a and 18b and an outer surface 18c.
  • the inner circumferential surface 18 a is a surface in contact with the outer circumferential surface 13 a of the bearing housing 13.
  • the inner circumferential surface 18 b is a surface in contact with the outer circumferential surface 15 a of the bearing housing 15.
  • the outer surface 18c is a surface that comes in contact with the outside air.
  • the temperature difference suppression mechanism 19 is configured of a plurality of recesses 35 and 36.
  • the plurality of recesses 35 are provided in a portion of the casing 18 that constitutes the inner circumferential surface 18 a.
  • the recess 35 may be, for example, a hole, a slit or a ring-shaped groove.
  • the plurality of recesses 36 are provided in a portion of the casing 18 that constitutes the inner circumferential surface 18 b.
  • the recess 36 may be, for example, a hole, a slit or a ring-shaped groove.
  • the support member 21 is provided at one end of the casing 18.
  • the support member 21 has a through hole 21A into which the tip end 11A is inserted. A part of the tip 11A protrudes to the outside of the support member 21.
  • the seal member 22 is a ring-shaped seal member and is provided in the through hole 21A.
  • the inner peripheral surfaces 18 a and 18 b of the casing 18 and the bearing box 13 The contact areas of the bearing housings 13 and 15 with the outer peripheral surfaces 13a and 15a are reduced, so it is possible to make it difficult for the heat of the bearing housings 13 and 15 in contact with the outer ring 16B to be transmitted to the casing 18.
  • the temperature decrease of the outer ring 16B is suppressed, and the difference in thermal expansion between the inner ring 16A and the outer ring 16B can be reduced, so that the reduction of the life of the bearing 16 can be suppressed.
  • the axial length of the relief is adjusted to be larger than the axial length of the crowning portion (when the bearing itself is adjusted)
  • the decrease in the life of the bearing 16 can be suppressed more simply.
  • FIG. 2 the same components as those shown in FIG. 1 are denoted by the same reference numerals.
  • the rotary machine 40 is configured in the same manner as the rotary machine 10 according to the first embodiment except that a temperature difference suppression mechanism 41 is provided instead of the temperature difference suppression mechanism 19.
  • the temperature difference suppression mechanism 41 is configured of a heat insulating material 42 that covers the outer surface 18 c of the casing 18 and the outer surface 21 a of the support member 21.
  • heat insulating material 42 for example, foam glass, glass wool, rock wool, calcium silicate, perlite, polystyrene foam, extruded polystyrene foam, rigid urethane foam, polyvinyl chloride foam, insulation board, sheathing board, newspaper waste insulation material, etc. are used. It is possible.
  • the rotary machine 40 of the second embodiment by providing the heat insulating material 42 covering the outer surface 18 c of the casing 18 and the outer surface 21 a of the support member 21, contact between the outer surface 18 c of the casing 18 and the outside air can be suppressed. As a result, it is possible to keep the heat of the rotary machine 40 inside the heat insulating material 42. As a result, the temperature decrease of the outer ring 16B is suppressed, and the difference in thermal expansion between the inner ring 16A and the outer ring 16B can be reduced, so that the reduction of the life of the bearing 16 can be suppressed. Further, by having the lubricating oil injection portion 28 injecting the lubricating oil in the bearing 16, it is possible to cool the entire bearing 16 by using the lubricating oil, so that the temperature of the entire bearing 16 is prevented from being greatly increased. it can.
  • the several recessed part 36 which is the temperature difference suppression mechanism 19 demonstrated in 1st Embodiment to the rotary machine 40 of 2nd Embodiment.
  • the difference in thermal expansion between the inner ring 16A and the outer ring 16B is further reduced. It is possible to further suppress the decrease in the life of the bearing 16.
  • the rotary machine 50 is configured in the same manner as the rotary machine 40 according to the second embodiment except that a temperature difference suppression mechanism 51 is provided instead of the temperature difference suppression mechanism 41.
  • the temperature difference suppression mechanism 51 is configured by low thermal conductivity members 52 and 53 having a thermoelectric coefficient lower than that of the casing 18.
  • the low thermal conductivity member 52 is disposed between the outer peripheral surface 13 a of the bearing housing 13 and the inner peripheral surface 18 a of the casing 18.
  • the low thermal conductivity member 53 is disposed between the outer circumferential surface 15 a of the bearing housing 15 and the inner circumferential surface 18 b of the casing 18.
  • a cast iron-based material can be used as the material of the casing 18.
  • FC 300 which is a cast iron-based material (thermal conductivity is 43 W / (m ⁇ K))
  • the low thermal conductivity members 52 and 53 have thermal conductivity of 43 W / (m ⁇ Use one smaller than K).
  • a stainless steel-based material having a thermal conductivity of less than 43 W / (m ⁇ K) a rubber, a resin material, or the like may be used.
  • stainless steel material for example, martensitic stainless steel, austenitic stainless steel, ferritic stainless steel or the like can be used.
  • cast iron-based material for example, gray cast iron, spheroidal graphite cast iron, white cast iron, etc. can be used.
  • Specific rubber and resin materials include, for example, natural rubber, ethylene-propylene rubber, chloroprene rubber, silicone rubber, butyl rubber, polyurethane rubber, acrylic resin, epoxy resin, vinyl chloride resin, silicone resin, fluorine resin, phenol resin, Bakelite, polyethylene resin, polycarbonate resin, polystyrene resin, polypropylene resin and the like can be used.
  • the low thermal conductivity members 52 and 53 having a thermoelectric coefficient lower than that of the casing 18 are disposed between the bearing housings 13 and 15 and the casing 18 so that the bearing housing 13 is obtained. , 15 and the casing 18, it is possible to suppress the conduction of heat. As a result, the temperature decrease of the outer ring 16B is suppressed, and the difference in thermal expansion between the inner ring 16A and the outer ring 16B can be reduced, so that the reduction of the life of the bearing 16 can be suppressed.
  • At least one temperature difference is suppressed among the temperature difference suppression mechanism 19 described in the first embodiment and the temperature difference suppression mechanism 41 described in the second embodiment.
  • the mechanisms may be combined.
  • FIG. 4 the same components as those shown in FIG. 3 are denoted by the same reference numerals.
  • the rotary machine 60 is configured in the same manner as the rotary machine 50 of the third embodiment except that the temperature difference suppression mechanism 61 is provided instead of the temperature difference suppression mechanism 51.
  • the temperature difference suppression mechanism 61 is constituted by the heat generating members 62 and 63.
  • the heat generating body 62 is disposed between the outer peripheral surface 13 a of the bearing housing 13 and the inner peripheral surface 18 a of the casing 18.
  • the heat generating body 62 heats the bearing box 13 by generating heat.
  • the heating element 63 is disposed between the outer peripheral surface 15 a of the bearing housing 15 and the inner peripheral surface 18 b of the casing 18.
  • the heating element 63 heats the bearing box 15 by generating heat.
  • a heater for example, a sheet-like heater
  • the rotary machine 60 of the fourth embodiment by arranging the heat generating members 62 and 63 for heating the bearing housings 13 and 15 between the bearing housings 13 and 15 and the casing 18, compared with the inner ring 16A.
  • the difference in thermal expansion between the inner ring 16A and the outer ring 16B can be reduced, so that the reduction in the life of the bearing 16 can be suppressed.
  • the lubricating oil injection portions 28 and 32 injecting the lubricating oil to the bearing 16 it is possible to cool the entire bearing 16 using the lubricating oil. As a result, a large rise in the temperature of the entire bearing 16 can be suppressed.
  • the rotary machine 60 of the fourth embodiment may be combined with at least one temperature difference suppression mechanism among the temperature difference suppression mechanisms 19, 41, and 51 described in the first to third embodiments.
  • the inner race 16A and the outer race Since it is possible to further reduce the difference in thermal expansion between 16B and 16B, it is possible to further suppress the decrease in the life of the bearing 16.
  • the low thermal conductivity members 52 and 53 described in the third embodiment are applied to the rotary machine 60 of the fourth embodiment, the low thermal conductivity members 52 and 53 are disposed outside the heat generating members 62 and 63. You should do it.
  • FIG. 5 the same components as those of the structure shown in FIG. Further, in FIG. 6 and FIG. 7, the same components as those of the structure shown in FIG.
  • the rotary machine 70 is configured in the same manner as the rotary machine 40 according to the second embodiment except that the temperature difference suppression mechanism 71 is replaced with the temperature difference suppression mechanisms 71 and 72.
  • the temperature difference suppression mechanism 71 is composed of an inner peripheral surface 18a of the casing 18 which is roughened (roughened surface) and an outer peripheral surface 13a of the bearing housing 13 which is roughened. With such a configuration, a gap is formed between the inner peripheral surface 18a and the outer peripheral surface 13a, so that the contact area between the inner peripheral surface 18a and the outer peripheral surface 13a can be reduced.
  • the surface roughness of the inner circumferential surface 18a and the outer circumferential surface 13a may be the same or different.
  • the temperature difference suppressing mechanism 72 is constituted by an inner peripheral surface 18b of the casing 18 which is roughened (roughened surface) and an outer peripheral surface 15a of the bearing housing 15 which is roughened. With such a configuration, a gap is formed between the inner peripheral surface 18b and the outer peripheral surface 15a, so it is possible to reduce the contact area between the inner peripheral surface 18b and the outer peripheral surface 15a.
  • the surface roughness of the inner circumferential surface 18a and the outer circumferential surface 15a may be the same or different. Further, as a method of roughening the inner peripheral surfaces 18a and 18b and the outer peripheral surfaces 13a and 15a, it is possible to use, for example, a blast method (for example, a sand blast method).
  • the roughened surface reduces the contact area between the outer peripheral surfaces 13a and 15a of the bearing housings 13 and 15 and the inner peripheral surfaces 18a and 18b of the casing 18, so that the bearing housings 13 and 15 in contact with the outer ring 16B. It is possible to make it difficult to transfer the heat to the casing 18. As a result, the temperature decrease of the outer ring 16B is suppressed, and the difference in thermal expansion between the inner ring 16A and the outer ring 16B can be reduced, so that the reduction of the life of the bearing 16 can be suppressed.
  • both the outer peripheral surfaces 13a and 15a of the bearing housings 13 and 15 and the inner peripheral surfaces 18a and 18b of the casing 18 are rough surfaces. At least one of the outer peripheral surfaces 13a and 15a of 13 and 15 and the inner peripheral surfaces 18a and 18b of the casing 18 may be rough. In this case, the same effect as that of the rotary machine 70 of the fifth embodiment can be obtained.
  • At least one temperature difference suppression mechanism among the temperature difference suppression mechanisms 19, 41, 51, 61 described in the first to fourth embodiments may be combined with the rotary machine 70 of the fifth embodiment.
  • the inner ring 16A is obtained. Since it is possible to further reduce the difference in thermal expansion between the bearing 16 and the outer ring 16B, it is possible to further suppress the reduction in the life of the bearing 16.
  • 15 and the casing 18 may be slightly loosened. With such a configuration, it is possible to reduce the pressure at which the outer peripheral surfaces 13a and 15a of the bearing housings 13 and 15 contact the inner peripheral surfaces 18a and 18b of the casing 18 (hereinafter referred to as "contact pressure"). It becomes.
  • the rotary machine configured as described above can obtain the same effect as the rotary machine 70 of the fifth embodiment described above.
  • the structure for reducing the contact pressure between the outer peripheral surfaces 13a and 15a of the bearing housings 13 and 15 and the inner peripheral surfaces 18a and 18b of the casing 18 is the rotary machine 10 according to the first to fifth embodiments described above. 40, 50, 60, 70 may be applied.
  • At least one of the current bearing housings 13 and 15 and the casing 18 is higher than the thermal conductivity of the current material (bearing housings 13 and 15, casing 18 and bearing housings 13 and 15 and casing 18) It may be made of a material having a low thermal conductivity.
  • the materials of the current bearing housings 13 and 15 and the casing 18 are SS400 (50) W / (m ⁇ K)
  • the materials of the bearing housings 13 and 15 and the casing 18 include, for example, thermal conductivity It is possible to use a SUS material with 16W / (m ⁇ K).
  • the temperature of the outer ring 16B does not easily decrease, so that the same effect as that of the rotary machine 50 of the third embodiment can be obtained. Moreover, such a material change may be applied to the rotary machines 10, 40, 50, 60, 70 of the first to fifth embodiments described above.
  • At least one of the thickness of the bearing housings 13 and 15 and the thickness of the casing 18 may be configured to be thicker than the current thickness. In this manner, at least one of the thickness of the bearing housings 13 and 15 and the thickness of the casing 18 may be configured to be thicker than the current thickness. With such a configuration, a decrease in the temperature of the outer ring 16B can be suppressed, and therefore, the same effect as that of the rotary machine 10 of the first embodiment described above can be obtained.
  • at least one of the thickness of the bearing housings 13 and 15 and the thickness of the casing 18 is A configuration that is thicker than the thickness may be applied.
  • a rotating machine having a configuration in which the heat insulating material 42 is removed from the rotating machine 40 shown in FIG. 2 (hereinafter, referred to as “a rotating machine of a comparative example”) was prepared.
  • a rotating machine of a comparative example a rotating machine having a configuration in which the heat insulating material 42 is removed from the rotating machine 40 shown in FIG. 2
  • a rotating machine of a comparative example With lubricating oil injected to the plurality of bearings 16, the temperatures of the inner ring 16A and the outer ring 16B constituting each bearing 16 (five bearings arranged in the direction of the axis O) are measured, and the inner ring constituting each bearing 16 The absolute value of the temperature difference between 16A and the outer ring 16B was determined. The results are shown in FIG.
  • FIG. 8 numbers (1 to 5) indicating the positions of the five bearings 16 are shown on the horizontal axis, and the vertical axis is made the absolute value (° C.) of the temperature difference between the inner ring 16A and the outer ring 16B.
  • “1” shown in FIG. 8 shows the bearing 16 disposed at the base end (end of the base end 11B) of the rotating body 11 among the five bearings 16, and "2" is adjacent to "1". And the bearing 16 is shown.
  • “5” shown in FIG. 8 indicates the bearing 16 disposed at the tip of the rotating body 11 among the five bearings 16.
  • the temperature and the outer ring of the inner ring 16A of five bearings 16 (1 to 5" shown in FIG. 9 correspond to "1 to 5" in FIG. 8) of the rotary machine of the comparative example in FIG. It shows the temperature of 16B.
  • Example 10 In the example, a rotary machine 40 shown in FIG. 2 was used.
  • the heat insulating material 42 a rock wool heat insulating material manufactured by Nichias was used. The thickness of the heat insulating material 42 was 1 cm.
  • the temperatures of the inner ring 16A and the outer ring 16B constituting each bearing 16 are measured, and the inner ring constituting each bearing 16
  • the absolute value of the temperature difference between 16A and the outer ring 16B was determined.
  • FIG. 10 shows the temperatures of the inner ring 16A and the temperature of the outer ring 16B of the five bearings (1 to 5) constituting the rotary machine of the embodiment.
  • the present invention is applicable to rotating machines.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Rolling Contact Bearings (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Compressor (AREA)
  • Support Of The Bearing (AREA)
PCT/JP2017/042768 2016-12-26 2017-11-29 回転機械 Ceased WO2018123405A1 (ja)

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US16/472,102 US20200096043A1 (en) 2016-12-26 2017-11-29 Rotary machine

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JP2016251470A JP6781625B2 (ja) 2016-12-26 2016-12-26 回転機械
JP2016-251470 2016-12-26

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GB2602958B (en) * 2020-11-02 2023-08-16 Edwards Ltd Oil feed nut and oil reservoir for a vacuum pump
EP4160034A1 (en) * 2021-10-04 2023-04-05 Hamilton Sundstrand Corporation Bearing housing

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JP2016163932A (ja) * 2016-04-08 2016-09-08 日本精工株式会社 モータビルトイン方式の主軸装置

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CN110100105A (zh) 2019-08-06
CN110100105B (zh) 2021-07-16
US20200096043A1 (en) 2020-03-26
JP6781625B2 (ja) 2020-11-04
JP2018105394A (ja) 2018-07-05

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