EP3173630B1 - Compressor and turbocharger - Google Patents
Compressor and turbocharger Download PDFInfo
- Publication number
- EP3173630B1 EP3173630B1 EP16205770.7A EP16205770A EP3173630B1 EP 3173630 B1 EP3173630 B1 EP 3173630B1 EP 16205770 A EP16205770 A EP 16205770A EP 3173630 B1 EP3173630 B1 EP 3173630B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- scroll
- frame
- bolt
- compressor
- impeller
- 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
- 125000006850 spacer group Chemical group 0.000 description 29
- 230000003584 silencer Effects 0.000 description 24
- 238000002485 combustion reaction Methods 0.000 description 15
- 239000012634 fragment Substances 0.000 description 10
- 238000010586 diagram Methods 0.000 description 3
- 239000006096 absorbing agent Substances 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000003566 sealing material Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000009969 flowable effect Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/16—Other safety measures for, or other control of, pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/422—Discharge tongues
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
- F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/52—Outlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/39—Retaining components in desired mutual position by a V-shaped ring to join the flanges of two cylindrical sections, e.g. casing sections of a turbocharger
Definitions
- the present invention relates to a compressor and a turbocharger used for an internal combustion engine.
- a conventionally-used turbocharger for compressing air to be supplied to an internal combustion engine is equipped with a compressor including an impeller for compressing air, an air-guide cylinder for housing the impeller and guiding the air, and a scroll-chamber frame disposed adjacent to the air-guide cylinder, the scroll-chamber frame forming a scroll chamber for guiding the air having passed through the air-guide cylinder to outside.
- the turbocharger described in Patent Document 1 includes a shock-absorbing partition wall disposed between a diffuser of a compressor and a head tank storing lubricant oil for lubricating a journal bearing so as to prevent the head tank from breaking apart to bring about oil leakage when a part of the impeller bursts and scatters outwardly.
- Patent Document 2 refers to a method for attaching a turbocharger and housing to a turbocharger bearing housing, wherein the method comprises identifying complementary contact surfaces between the end housing and the bearing housing, applying a flowable sealing material to at least one of said complementary surfaces, drying and curing the sealing material to form a dried or cured solidified coating, and assembling the turbocharger such that the coating forms a gas barrier.
- patent document 3 discloses a device comprising a filter sound absorber and a casing part of a compressor belonging to a turbocharger for internal combustion engines, the filter sound absorber being fastened releasably to the casing part of the compressor with the aid of fastening elements.
- an impeller fragment may fly off outwardly in the radial direction of the impeller, and may hit the air-guide cylinder and a frame around the air-guide cylinder, for instance. If the impeller fragment hits the air-guide cylinder or a frame around the air-guide cylinder, for instance, there is a risk of generation of tensile stress in a bolt for fastening a scroll-chamber frame adjacent to the air-guide cylinder and a frame adjacent to the scroll-chamber frame, which may break the bolt.
- Patent Document 1 describes a configuration for preventing breakage of a lubricant-oil head tank upon scatter of an impeller described above, it does not disclose breakage of the bolt due to scatter of the impeller or a solution thereto.
- An object of the present invention is to provide a compressor and a turbocharger whereby it is possible to suppress breakage of a bolt that fastens a bearing frame and the scroll-chamber frame effectively, and to achieve a stable joint state between the frames.
- a compressor according to the present invention is the compressor of claim 1.
- the invention is also directed to the turbocharger of claim 10.
- the dependent claims refer to preferred embodiments.
- FIG. 1 is a schematic diagram illustrating an overall configuration of an internal combustion engine system 100 according to some embodiments.
- the internal combustion engine system 100 illustrated in FIG. 1 includes an internal combustion engine 2, a turbocharger 4 for pressurizing intake air sucked into the internal combustion engine 2, and a generator 8 driven by a turbine 6 of the turbocharger 4.
- the turbocharger 4 illustrated in FIG. 1 includes a compressor 10 of centrifugal type for pressurizing intake air sucked into the internal combustion engine 2, a turbine 6 coupled to the compressor 10 via a rotation shaft 12 and driven by exhaust gas of the internal combustion engine 2, and a silencer 13 for reducing noise that the compressor 10 generates.
- the turbocharger 4 illustrated in FIG. 1 is a supercharger of exhaust-turbine drive type, which is called a turbocharger, in which the compressor 10 is driven by the turbine 6 driven by exhaust gas of the internal combustion engine 2.
- the turbocharger 4 may be a supercharger of mechanical drive type, which is called a supercharger, in which the compressor 10 is driven by power extracted from an output shaft of the internal combustion engine 2 via a belt or the like.
- a diesel engine or a gasoline engine may be suitably selected as the internal combustion engine 2 for instance.
- FIG. 2 is a schematic cross-sectional view of a part of a turbocharger 4 according to some embodiments.
- the compressor 10 illustrated in FIG. 2 includes an impeller 14 for compressing air, an air-guide cylinder 16 housing the impeller 14 and guiding air, a scroll-chamber frame 20, and a second or bearing frame 40.
- the impeller 14 includes a hub 15 and a plurality of blades 17 disposed around the hub 15.
- the scroll-chamber frame 20 is disposed adjacent to the air-guide cylinder 16, and includes a scroll-chamber forming portion 19 which forms a scroll chamber 18 for guiding air that has passed through the air-guide cylinder 16 to outside.
- the second or bearing frame 40 includes a bearing portion 44 for pivotably supporting a rotation shaft 12 of the impeller 14.
- the silencer 13 includes a silencer frame 22 disposed adjacent to the scroll-chamber frame 20.
- a flange portion 23 of the scroll-chamber frame 20 and a flange portion 24 of the silencer frame 22 are fastened to each other by a first bolt 25.
- a spacer 28 (see FIG. 3 ) may be disposed between a head portion 26 of the bolt 25 and the scroll-chamber frame 20.
- a flange portion 46 of the bearing frame 40 and a flange portion 29 of the scroll-chamber frame 20 are fastened to each other by a second or fastening bolt 48.
- an impeller fragment may fly apart outwardly in the radial direction of the impeller 14, and may hit the air-guide cylinder 16, the scroll-chamber frame 20, or the like.
- the hit causes an inlet 32 of the air-guide cylinder 16 to move toward the silencer 13 in the direction S of the arrow (see FIG. 3 ) and hit an outlet 43 of the silencer frame 22.
- the flange portion 24 of the silencer frame 22 tries to move away from the flange portion 23 of the scroll-chamber frame 20, which leads to generation of tensile stress on the bolt 25.
- the compressor 10 and the turbocharger 4 are configured such that the spacer 28 may be disposed between the head portion 26 of the bolt 25 and the scroll-chamber frame 20, which makes it possible to fasten the scroll-chamber frame 20 and the silencer frame 22 using the bolt 25 with a shank portion 31 (see FIG. 3 ) having a large length (shank length) as compared to a case where the spacer 28 is not provided.
- a shank portion 31 see FIG. 3
- the spacer 28 is not provided, it is possible to secure a large amount of extension to which the bolt 25 can extend without breaking when receiving tensile load in the axial direction.
- the spacer 28 illustrated in FIG. 3 is formed in a sleeve shape and disposed so as to surround the shank portion 31 of the bolt 25, and the inside diameter d 1 of the spacer 28 is smaller than the diameter d 2 of the head portion 26 of the bolt 25.
- the dimension d 3 of the spacer 28 in the axial direction of the bolt 25 illustrated in FIG. 3 is greater than the dimension d 4 of the spacer 28 in the radial direction of the spacer 28.
- FIG. 3 an example in which tensile stress is generated due to breakage of the impeller 14 on the bolt 25 fastening the scroll-chamber frame 20 and the silencer frame 22 is described.
- tensile stress may be generated due to breakage of the impeller 14 on the second or fastening bolt 48 fastening the scroll-chamber frame 20 and the bearing frame 40.
- the impeller fragment enters a diffuser portion 50 illustrated in FIG. 2 and gets stuck in the diffuser portion 50, the impeller fragment presses the diffuser portion 50 to expand in the axial direction of the impeller 14.
- the scroll-chamber frame 20 and the bearing frame receive a force in a direction away from each other, and thus the scroll-chamber frame 20 deforms as illustrated in FIG. 4 and tensile stress is generated on the bolt 48.
- the spacer 28 described with reference to FIG. 3 may be disposed between the head portion 52 of the bolt 48 and the scroll-chamber frame 20 to make the shank portion 53 of the bolt 48 longer than that illustrated in FIG. 4 .
- the flange portion 29 of the scroll-chamber frame 20 is disposed so as to extend outwardly from the scroll-chamber forming portion 19 in the radial direction of the impeller 14.
- the turbocharger 4 and the compressor 10 illustrated in FIG. 2 includes a clamp 54 configured to nip the scroll-chamber frame 20 and the bearing frame 40 as illustrated in FIGs. 5 and 6 .
- FIG. 5 is a view of the flange portion 29 of the scroll-chamber frame 20 and the flange portion 46 of the bearing frame 40 as seen from direction P in FIG. 2 , illustrating the arrangement of the bolt 48 and the clamp 54.
- FIG. 6 is a schematic cross-sectional view for describing a structure of the clamp 54.
- the clamp 54 illustrated in FIGs. 5 and 6 includes a pressing bolt 56 that applies a pressing force to the bearing frame 40 from the opposite side from the flange portion 29 of the scroll-chamber frame 20.
- a pressing bolt 56 that applies a pressing force to the bearing frame 40 from the opposite side from the bearing frame 40.
- the clamp 54 is configured to nip the scroll-chamber frame 20 and the bearing frame 40. It is also possible that a clamp configured to nip the scroll-chamber frame 20 and the silencer frame 22 may be used. In this way, it is possible to join the scroll-chamber frame 20 and the silencer frame 22 stably.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Description
- The present invention relates to a compressor and a turbocharger used for an internal combustion engine.
- A conventionally-used turbocharger for compressing air to be supplied to an internal combustion engine is equipped with a compressor including an impeller for compressing air, an air-guide cylinder for housing the impeller and guiding the air, and a scroll-chamber frame disposed adjacent to the air-guide cylinder, the scroll-chamber frame forming a scroll chamber for guiding the air having passed through the air-guide cylinder to outside. The turbocharger described in Patent Document 1 includes a shock-absorbing partition wall disposed between a diffuser of a compressor and a head tank storing lubricant oil for lubricating a journal bearing so as to prevent the head tank from breaking apart to bring about oil leakage when a part of the impeller bursts and scatters outwardly.
Patent Document 2 refers to a method for attaching a turbocharger and housing to a turbocharger bearing housing, wherein the method comprises identifying complementary contact surfaces between the end housing and the bearing housing, applying a flowable sealing material to at least one of said complementary surfaces, drying and curing the sealing material to form a dried or cured solidified coating, and assembling the turbocharger such that the coating forms a gas barrier. Furthermore, patent document 3 discloses a device comprising a filter sound absorber and a casing part of a compressor belonging to a turbocharger for internal combustion engines, the filter sound absorber being fastened releasably to the casing part of the compressor with the aid of fastening elements. -
- Patent Document 1:
JP2001-132465A - Patent Document 2:
WO 2012/030783 A2 - Patent Document 3:
EP 1 186 781 A1 - If an impeller breaks apart in a compressor constituting a part of a turbocharger, an impeller fragment may fly off outwardly in the radial direction of the impeller, and may hit the air-guide cylinder and a frame around the air-guide cylinder, for instance. If the impeller fragment hits the air-guide cylinder or a frame around the air-guide cylinder, for instance, there is a risk of generation of tensile stress in a bolt for fastening a scroll-chamber frame adjacent to the air-guide cylinder and a frame adjacent to the scroll-chamber frame, which may break the bolt.
- In this regard, although Patent Document 1 describes a configuration for preventing breakage of a lubricant-oil head tank upon scatter of an impeller described above, it does not disclose breakage of the bolt due to scatter of the impeller or a solution thereto.
- An object of the present invention is to provide a compressor and a turbocharger whereby it is possible to suppress breakage of a bolt that fastens a bearing frame and the scroll-chamber frame effectively, and to achieve a stable joint state between the frames.
- A compressor according to the present invention is the compressor of claim 1. The invention is also directed to the turbocharger of
claim 10. The dependent claims refer to preferred embodiments. - (1) In some aspects of the present disclosure which are presently not claimed, the compressor comprises: an impeller for compressing air; an air-guide cylinder for housing the impeller and guiding the air; a scroll-chamber frame disposed adjacent to the air-guide cylinder, the scroll-chamber frame forming a scroll chamber for guiding the air having passed through the air-guide cylinder to outside; a first frame disposed adjacent to the scroll-chamber frame; a first bolt for fastening the scroll-chamber frame and the first frame; and a spacer disposed between a head portion of the first bolt and the scroll-chamber frame.
If an impeller breaks apart in a compressor, an impeller fragment may fly off outwardly in the radial direction of the impeller, and hit the air-guide cylinder or a frame around the air-guide cylinder, for instance. If the impeller fragment hits the air-guide cylinder or the frame around the air-guide cylinder, for instance, there is a risk of generation of tensile stress in the first bolt for fastening a scroll-chamber frame adjacent to the air-guide cylinder and the first frame adjacent to the scroll-chamber frame, which may break the first bolt.
In this regard, with the compressor according to the above (1), since the spacer is disposed between the head portion of the first bolt and the scroll-chamber frame, it is possible to fasten the scroll-chamber frame and the first frame using the first bolt with a shank portion having a large length (shank length) as compared to a case where the spacer is not provided. Thus, as compared to a case where the spacer is not provided, it is possible to secure a large amount of extension to which the first bolt can extend without breaking when tensile load in the axial direction is applied to the first bolt. In this way, even if tensile stress caused by breakage of the impeller is generated on the first bolt fastening the scroll-chamber frame and the first frame as described above, it is possible to suppress breakage of the first bolt effectively. Specifically, it is possible to achieve a stable joint state between the scroll-chamber frame and the first frame.
Further, to produce the compressor described in the above (1), it is only required to add a spacer and replace the first bolt for an existing compressor, and it is unnecessary to renew the entire configuration. That is, the compressor according to the above (1) has another merit from the perspective of manufacturability.
Further, "the first frame" of the compressor described in (1) is intended to include at least a silencer frame or a bearing frame described in the following detailed description. Still further, in a case where the first bolt is a stud bolt in the compressor described in the above (1), the head portion of the first bolt refers to a nut used for the stud bolt. - (2) In some aspects of the present disclosure which are presently not claimed, in the compressor described in the above (1), the spacer is formed in a sleeve shape and disposed so as to surround a shank portion of the first bolt. An inside diameter of the spacer is smaller than a head diameter of the first bolt.
With the compressor described in the above (2), it is possible to support the head portion of the first bolt uniformly with the spacer having a sleeve shape disposed so as to surround the shank portion of the first bolt, which makes it possible to suppress breakage of the first bolt effectively even if tensile stress is generated on the first bolt due to breakage of the impeller as described above. Thus, it is possible to achieve a stable joint state between the scroll-chamber frame and the first frame adjacent to the scroll chamber. - (3) In some aspects of the present disclosure which are presently not claimed, in the compressor described in the above (1) or (2), a dimension of the spacer in an axial direction of the first bolt is larger than a dimension of the spacer in a radial direction of the first bolt.
As in the compressor described in the above (3), using the spacer configured suitable to increase the length of the shank portion of the first bolt makes it possible to easily secure a large amount of extension to which the first bolt can extend without breaking when tensile load in the axial direction is applied to the first bolt.
In this way, even if tensile stress caused by breakage of the impeller is generated on the first bolt fastening the scroll-chamber frame and the first frame as described above, it is possible to suppress breakage of the first bolt effectively. Thus, it is possible to achieve a stable joint state between the scroll-chamber frame and the first frame adjacent to the scroll-chamber frame. - (4) In some aspects of the present disclosure which are presently not claimed the above compressor described in any one of the above (1) to (3) further comprises a silencer for reducing noise generated by the compressor, and the first frame is a frame of the silencer.
With the compressor described in the above (4), even if tensile stress caused by breakage of the impeller is generated on the first bolt fastening the scroll-chamber frame and the frame of the silencer, it is possible to suppress breakage of the first bolt effectively. As a result, it is possible to suppress detachment of the silencer from the compressor effectively. - (5) According to the invention, the compressor comprises a second or bearing frame disposed adjacent to the scroll-chamber frame; a second or fastening bolt for fastening the scroll-chamber frame and the second or bearing frame; and a clamp configured to nip the flange portion of the scroll-chamber frame and the second or bearing frame.
If an impeller breaks apart in a compressor, an impeller fragment may fly apart outwardly in the radial direction of the impeller, and hit the air-guide cylinder or the scroll-chamber frame. If the impeller fragment hits the air-guide cylinder or the scroll-chamber frame, there is a risk of generation of tensile stress in the second bolt for fastening the scroll-chamber frame and the second frame adjacent to the scroll-chamber frame, which may break the second bolt.
In this regard, according to the compressor described in the above (5), with the clamp configured to nip the scroll-chamber frame and the second frame, it is possible to suppress generation of tensile stress in the second bolt and to suppress breakage of the second bolt effectively. Thus, it is possible to achieve a stable joint state between the scroll-chamber frame and the second frame adjacent to the scroll-chamber frame. - (6) In the compressor of the invention, the second frame is a bearing frame in which a bearing part for pivotally supporting a rotation shaft of the impeller is disposed.
With the compressor described in the above (6), even if tensile stress caused by breakage of the impeller is generated on the second bolt fastening the scroll-chamber frame and the bearing frame, it is possible to suppress breakage of the second bolt effectively. As a result, it is possible to achieve a stable joint state between the scroll-chamber frame and the bearing frame. - (7) In some embodiments, in the compressor described in the above (6), the scroll-chamber frame includes: a scroll-chamber forming portion forming the scroll chamber; and a flange portion disposed so as to extend outwardly in a radial direction of the impeller from the scroll-chamber forming portion to join the scroll-chamber frame and the bearing frame. The second bolt fastens the flange portion and the bearing frame, and the clamp is configured to nip the flange portion and the bearing frame.
In a configuration such that the bearing frame is joined with the flange portion extending outwardly from the scroll-chamber forming portion in the radial direction of the impeller, it may be difficult to secure a space between the flange portion and the scroll-chamber forming portion, and it may be difficult to provide a spacer between the head portion of the second bolt and the scroll-chamber frame to prevent breakage of the second bolt.
Even in such a case, according to the compressor described in the above (7), with the clamp configured to nip the scroll-chamber frame and the bearing frame, it is possible to suppress generation of tensile stress in the second bolt and to suppress breakage of the second bolt effectively. As a result, it is possible to achieve a stable joint state between the scroll-chamber frame and the bearing frame. - (8) In the compressor of the invention, the clamp includes a pressing bolt which applies a pressing force to the bearing frame from an opposite side from the flange portion of the scroll-chamber frame.
In a configuration such that the bearing frame is joined with the flange portion extending outwardly from the scroll-chamber forming portion in the radial direction of the impeller, it may be difficult to secure a space between the flange portion and the scroll-chamber forming portion, and it may be difficult to provide a spacer between the head portion of the second bolt and the scroll-chamber frame to prevent breakage of the second bolt.
Even in such a case, with the pressing bolt for applying a pressing force to the bearing frame from the opposite side from the flange portion of the scroll-chamber frame as in the compressor described in the above (8), it is possible to suppress generation of tensile stress in the second bolt with a simplified configuration and to suppress breakage of the second bolt effectively. As a result, it is possible to achieve a stable joint state between the scroll-chamber frame and the bearing frame with a simplified configuration. - (9) A turbocharger of the present invention is the turbocharger of
claim 10 and comprises the compressor of claim 1.
With the turbocharger according to the present invention, it is possible to suppress breakage of the first bolt effectively even if tensile stress is generated due to breakage of the impeller.
Specifically, it is possible to achieve a stable joint state between the scroll-chamber frame and the first frame. - According to the present invention, it is possible to suppress breakage of a bolt fastening a bearing frame and the scroll-chamber frame effectively, and to achieve a stable joint state between the frames.
-
-
FIG. 1 is a schematic diagram illustrating an overall configuration of an internal combustion engine system according to some embodiments. -
FIG. 2 is a schematic cross-sectional view of a part of a turbocharger according to some embodiments. -
FIG. 3 is a schematic cross sectional view of a bolt for fastening a scroll-chamber frame and a silencer frame and its peripheral structure. -
FIG. 4 is a diagram illustrating a state where a scroll-chamber frame is deformed and tensile stress is generated on a bolt fastening the scroll-chamber frame and a second or bearing frame. -
FIG. 5 is a view of a flange portion of the scroll-chamber frame and a flange portion of the bearing frame as seen from direction P inFIG. 2 . -
FIG. 6 is a schematic cross-sectional view for describing a structure of a clamp according to the invention. - Embodiments and non-claimed examples will now be described with reference to the accompanying drawings. It is intended, however, that unless particularly specified, dimensions, materials, shapes, relative positions and the like of components described shall be interpreted as illustrative only and not intended to limit the scope of the present invention unless particularly specified.
-
FIG. 1 is a schematic diagram illustrating an overall configuration of an internalcombustion engine system 100 according to some embodiments. - The internal
combustion engine system 100 illustrated inFIG. 1 includes aninternal combustion engine 2, aturbocharger 4 for pressurizing intake air sucked into theinternal combustion engine 2, and a generator 8 driven by aturbine 6 of theturbocharger 4. - The
turbocharger 4 illustrated inFIG. 1 includes acompressor 10 of centrifugal type for pressurizing intake air sucked into theinternal combustion engine 2, aturbine 6 coupled to thecompressor 10 via arotation shaft 12 and driven by exhaust gas of theinternal combustion engine 2, and asilencer 13 for reducing noise that thecompressor 10 generates. - The
turbocharger 4 illustrated inFIG. 1 is a supercharger of exhaust-turbine drive type, which is called a turbocharger, in which thecompressor 10 is driven by theturbine 6 driven by exhaust gas of theinternal combustion engine 2. In another embodiment, theturbocharger 4 may be a supercharger of mechanical drive type, which is called a supercharger, in which thecompressor 10 is driven by power extracted from an output shaft of theinternal combustion engine 2 via a belt or the like. Further, as theinternal combustion engine 2, for instance, a diesel engine or a gasoline engine may be suitably selected. - Next, the specific configuration of the
turbocharger 4 will be described below with reference toFIG. 2 . -
FIG. 2 is a schematic cross-sectional view of a part of aturbocharger 4 according to some embodiments. - The
compressor 10 illustrated inFIG. 2 includes an impeller 14 for compressing air, an air-guide cylinder 16 housing the impeller 14 and guiding air, a scroll-chamber frame 20, and a second or bearingframe 40. The impeller 14 includes ahub 15 and a plurality ofblades 17 disposed around thehub 15. The scroll-chamber frame 20 is disposed adjacent to the air-guide cylinder 16, and includes a scroll-chamber forming portion 19 which forms ascroll chamber 18 for guiding air that has passed through the air-guide cylinder 16 to outside. The second or bearingframe 40 includes a bearingportion 44 for pivotably supporting arotation shaft 12 of the impeller 14. - The
silencer 13 includes asilencer frame 22 disposed adjacent to the scroll-chamber frame 20. With regard to the scroll-chamber frame 20 and thesilencer frame 22, aflange portion 23 of the scroll-chamber frame 20 and aflange portion 24 of thesilencer frame 22 are fastened to each other by afirst bolt 25. A spacer 28 (seeFIG. 3 ) may be disposed between ahead portion 26 of thebolt 25 and the scroll-chamber frame 20. - With regard to the
bearing frame 40 and the scroll-chamber frame 20, aflange portion 46 of the bearingframe 40 and aflange portion 29 of the scroll-chamber frame 20 are fastened to each other by a second orfastening bolt 48. - If the impeller 14 breaks apart in the
compressor 10 constituting a part of theturbocharger 4 illustrated inFIG. 2 , an impeller fragment may fly apart outwardly in the radial direction of the impeller 14, and may hit the air-guide cylinder 16, the scroll-chamber frame 20, or the like. - For instance, if the impeller fragment hits an
oblique section 30 of the air-guide cylinder 16, the hit causes aninlet 32 of the air-guide cylinder 16 to move toward thesilencer 13 in the direction S of the arrow (seeFIG. 3 ) and hit anoutlet 43 of thesilencer frame 22. As a result, theflange portion 24 of thesilencer frame 22 tries to move away from theflange portion 23 of the scroll-chamber frame 20, which leads to generation of tensile stress on thebolt 25. - Even if tensile stress is generated on the
bolt 25 as described above, thecompressor 10 and theturbocharger 4 are configured such that the spacer 28 may be disposed between thehead portion 26 of thebolt 25 and the scroll-chamber frame 20, which makes it possible to fasten the scroll-chamber frame 20 and thesilencer frame 22 using thebolt 25 with a shank portion 31 (seeFIG. 3 ) having a large length (shank length) as compared to a case where the spacer 28 is not provided. Thus, as compared to a case where the spacer 28 is not provided, it is possible to secure a large amount of extension to which thebolt 25 can extend without breaking when receiving tensile load in the axial direction. In this way, even if tensile stress caused by breakage of the impeller 14 is generated on thebolt 25 fastening the scroll-chamber frame 20 and thesilencer frame 22, it is possible to suppress breakage of thebolt 25 effectively. As a result, it is possible to join the scroll-chamber frame 20 and thesilencer frame 22 stably, and to suppress detachment of thesilencer 13 from theturbocharger 4 or thecompressor 10 effectively. - The spacer 28 illustrated in
FIG. 3 is formed in a sleeve shape and disposed so as to surround theshank portion 31 of thebolt 25, and the inside diameter d1 of the spacer 28 is smaller than the diameter d2 of thehead portion 26 of thebolt 25. Thus, it is possible to support thehead portion 26 of thebolt 25 uniformly with the spacer 28, which makes it possible to suppress breakage of thebolt 25 effectively if tensile stress is generated on thebolt 25 due to breakage of the impeller 14 as described above. - Further, the dimension d3 of the spacer 28 in the axial direction of the
bolt 25 illustrated inFIG. 3 is greater than the dimension d4 of the spacer 28 in the radial direction of the spacer 28. Thus, with the spacer 28 configured suitable to increase the length of theshank portion 31 of thebolt 25, it is possible to easily secure a large amount of extension to which thebolt 25 can extend without breaking when receiving tensile load in the axial direction. In this way, even if tensile stress caused by breakage of the impeller 14 is generated on thebolt 25 fastening the scroll-chamber frame 20 and thesilencer frame 22, it is possible to suppress breakage of thebolt 25 effectively. - In
FIG. 3 , an example in which tensile stress is generated due to breakage of the impeller 14 on thebolt 25 fastening the scroll-chamber frame 20 and thesilencer frame 22 is described. On the other hand, tensile stress may be generated due to breakage of the impeller 14 on the second orfastening bolt 48 fastening the scroll-chamber frame 20 and thebearing frame 40. - For instance, if the impeller fragment enters a
diffuser portion 50 illustrated inFIG. 2 and gets stuck in thediffuser portion 50, the impeller fragment presses thediffuser portion 50 to expand in the axial direction of the impeller 14. As a result, the scroll-chamber frame 20 and the bearing frame receive a force in a direction away from each other, and thus the scroll-chamber frame 20 deforms as illustrated inFIG. 4 and tensile stress is generated on thebolt 48. - To prevent breakage of the
bolt 48 due to the above tensile stress, according to a non-claimed example, the spacer 28 described with reference toFIG. 3 may be disposed between thehead portion 52 of thebolt 48 and the scroll-chamber frame 20 to make theshank portion 53 of thebolt 48 longer than that illustrated inFIG. 4 . However, as illustrated inFIG. 2 , theflange portion 29 of the scroll-chamber frame 20 is disposed so as to extend outwardly from the scroll-chamber forming portion 19 in the radial direction of the impeller 14. Thus, it is difficult to secure a space between theflange portion 29 and the scroll-chamber forming portion 19, and it may be difficult to provide a spacer between thehead portion 52 of thebolt 48 and the scroll-chamber frame 20 to prevent breakage of thebolt 48. - In view of this, the
turbocharger 4 and thecompressor 10 illustrated inFIG. 2 includes aclamp 54 configured to nip the scroll-chamber frame 20 and thebearing frame 40 as illustrated inFIGs. 5 and6 .FIG. 5 is a view of theflange portion 29 of the scroll-chamber frame 20 and theflange portion 46 of the bearingframe 40 as seen from direction P inFIG. 2 , illustrating the arrangement of thebolt 48 and theclamp 54.FIG. 6 is a schematic cross-sectional view for describing a structure of theclamp 54. - As described above, using the
clamp 54 configured to nip theflange portion 29 of the scroll-chamber frame 20 and theflange portion 46 of the bearingframe 40 makes it possible to suppress generation of tensile stress on thebolt 48 and to suppress breakage of thebolt 48 effectively, even for a configuration such that it is difficult to secure a sufficient space for providing the above described spacer between theflange portion 29 and the scroll-chamber forming portion 19. As a result, it is possible to join the scroll-chamber frame 20 and thebearing frame 40 stably. - The
clamp 54 illustrated inFIGs. 5 and6 includes apressing bolt 56 that applies a pressing force to thebearing frame 40 from the opposite side from theflange portion 29 of the scroll-chamber frame 20. In this way, even in a case where it is difficult to provide a spacer between thehead portion 52 of thebolt 48 and the scroll-chamber frame 20 as described above in order to prevent breakage of thebolt 48, it is possible to suppress generation of tensile stress on thebolt 48 with a simplified configuration, and to suppress breakage of thebolt 48 effectively. As a result, it is possible to join the scroll-chamber frame 20 and thebearing frame 40 stably with a simplified configuration. Further, in another embodiment, a pressing bolt that applies a pressing force to theflange portion 29 of the scroll-chamber frame 20 from the opposite side from the bearingframe 40 may be used. - In the embodiment described with reference to
FIG. 6 , theclamp 54 is configured to nip the scroll-chamber frame 20 and thebearing frame 40. It is also possible that a clamp configured to nip the scroll-chamber frame 20 and thesilencer frame 22 may be used. In this way, it is possible to join the scroll-chamber frame 20 and thesilencer frame 22 stably. -
- 2 Internal combustion engine
- 4 Turbocharger
- 6 Turbine
- 8 Generator
- 10 Compressor
- 12 Rotation shaft
- 13 Silencer
- 14 Impeller
- 16 Air-guide cylinder
- 17 Blade
- 18 Scroll chamber
- 19 Scroll-chamber forming portion
- 20 Scroll-chamber frame
- 22 Silencer frame
- 23, 24, 29, 46 Flange portion
- 25,48 Bolt
- 26, 52 Head portion
- 28 Spacer
- 30 Oblique section
- 31 Shank portion
- 32 Inlet
- 40 Bearing frame
- 43 Outlet
- 44 Bearing portion
- 50 Diffuser portion
- 54 Clamp
- 56 Pressing bolt
- 100 Internal combustion engine system
- d1 Inside diameter
- d2 Diameter
- d3, d4 Dimension
Claims (10)
- A compressor (10) of centrifugal type comprising:an impeller (14) for compressing air;an air-guide cylinder (16) for housing the impeller (14) and guiding the air;a scroll-chamber frame (20) disposed adjacent to the air-guide cylinder (16), the scroll-chamber frame (20) forming a scroll chamber (18) for guiding the air having passed through the air-guide cylinder to outside, the scroll-chamber frame (20) including a flange portion (29) disposed as to extend outwardly in a radial direction of the impeller (14);a first frame (22) disposed adjacent to the scroll-chamber frame (20);a bearing frame (40) in which a bearing part (44) for pivotally supporting a rotation shaft (12) of the impeller (14) is disposed, the bearing frame (40) being disposed adjacent to the scroll-chamber frame (20);
anda clamp (54) configured to nip the flange portion (29) of the scroll-chamber frame (20) and the bearing frame (40),characterized in that the compressor further comprisesa fastening bolt (48) for fastening the scroll-chamber frame (20) and the bearing frame (40); and in that the clamp (54) includes a pressing bolt (56) which applies a pressing force to the bearing frame (40) from an opposite side from the flange portion (29) of the scroll-chamber frame (20) or a pressing force to the flange portion (29) of the scroll-chamber frame (20) from an opposite side from the bearing frame (40). - The compressor (10) according to claim 1,
wherein the tip of the pressing bolt (56) abuts in the axial direction to the scroll-chamber frame (20) or the bearing frame (40) to apply a pressing force in the axial direction of the impeller (14) relative to the scroll chamber frame (20) or the bearing frame (40). - The compressor (10) according to claim 2,
wherein the tip of the pressing bolt (56) abuts in the axial direction to the bearing frame (40) from an opposite side from the scroll chamber frame (20). - The compressor (10) according to claim 1,
wherein the bearing frame (40) includes a flange portion (46) disposed so as to extend outwardly in a radial direction of the impeller (14),
wherein the fastening bolt (48) fastens the flange portion (29) of the scroll chamber frame (20) and the flange portion (46) of the bearing frame (40), and
wherein the clamp (54) is configured to nip the flange portion (29) of the scroll-chamber frame (20) and the flange portion (46) of the bearing frame (40). - The compressor (10) according to claim 1,
wherein the fastening bolt (48) and the clamp (54) are provided at different positions each other in the circumferential direction of the impeller (14). - The compressor (10) according to claim 1,
wherein the clamp (54) is provided on each of at least three locations in a circumferential direction of the impeller (14). - The compressor (10) according to claim 1,
wherein the clamp (54) includes:a first portion extending in a radial direction of the impeller (14) along the scroll chamber frame (20);a second portion extending in the radial direction of the impeller (14) along the bearing frame (40); anda third portion extending in the axial direction of the impeller (14) so as to connect the first portion with the second portion. - The compressor (10) according to claim 7,
wherein the pressing bolt (56) is configured to penetrate the second portion in the axial direction from the opposite side of the first portion and abut on the bearing frame (40). - The compressor (10) according to claim 1,
wherein the fastening bolt (48) and the pressing bolt (56) are provided from the side opposite to each other in the axial direction. - A turbocharger (4) comprising the compressor (10) according to any one of claims 1 to 9.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2013198638A JP6097188B2 (en) | 2013-09-25 | 2013-09-25 | Turbocharger |
EP14849505.4A EP3009633B1 (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
PCT/JP2014/067415 WO2015045541A1 (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
Related Parent Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14849505.4A Division-Into EP3009633B1 (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
EP14849505.4A Division EP3009633B1 (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3173630A1 EP3173630A1 (en) | 2017-05-31 |
EP3173630B1 true EP3173630B1 (en) | 2018-08-15 |
Family
ID=52742699
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14849505.4A Active EP3009633B1 (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
EP16205770.7A Active EP3173630B1 (en) | 2013-09-25 | 2014-06-30 | Compressor and turbocharger |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14849505.4A Active EP3009633B1 (en) | 2013-09-25 | 2014-06-30 | Compressor and supercharger |
Country Status (5)
Country | Link |
---|---|
EP (2) | EP3009633B1 (en) |
JP (1) | JP6097188B2 (en) |
KR (1) | KR101799707B1 (en) |
CN (1) | CN107701298B (en) |
WO (1) | WO2015045541A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3053384B1 (en) * | 2016-06-30 | 2018-07-27 | Safran Aircraft Engines | FIXING ASSEMBLY OF A DISTRIBUTOR TO A STRUCTURAL ELEMENT OF A TURBOMACHINE |
JP6517386B2 (en) * | 2018-02-13 | 2019-05-22 | 三菱重工業株式会社 | Centrifugal compressor and supercharger |
JP7562357B2 (en) * | 2020-09-30 | 2024-10-07 | 三菱重工マリンマシナリ株式会社 | Rotating Machinery |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2948398A1 (en) * | 1979-12-01 | 1981-06-04 | Skf Kugellagerfabriken Gmbh, 8720 Schweinfurt | EXHAUST TURBOCHARGER |
JPS5939930A (en) * | 1982-08-27 | 1984-03-05 | Nissan Motor Co Ltd | Turbocharger |
JPH0195536U (en) * | 1987-12-18 | 1989-06-23 | ||
JPH03129731U (en) * | 1990-04-09 | 1991-12-26 | ||
AU1584092A (en) * | 1991-03-18 | 1992-10-21 | Ralph A. Moody Iii | Apparatus regulating exhaust flow to increase back pressure in an internal combustion engine |
DE59207544D1 (en) * | 1992-06-17 | 1997-01-02 | Asea Brown Boveri | Filter silencer |
US5295785A (en) * | 1992-12-23 | 1994-03-22 | Caterpillar Inc. | Turbocharger having reduced noise emissions |
EP0646699B1 (en) * | 1993-09-03 | 1998-04-22 | Asea Brown Boveri Ag | Method for adapting the radial turbine of a turbocharger on an internal combustion engine |
JPH1122568A (en) * | 1997-07-08 | 1999-01-26 | Aisan Ind Co Ltd | Intake device for internal combustion engine |
DE19745659C1 (en) * | 1997-10-17 | 1999-05-06 | Man B & W Diesel Ag | Turbo-supercharger for internal combustion engine |
DE19818873C2 (en) * | 1998-04-28 | 2001-07-05 | Man B & W Diesel Ag | Reciprocating internal combustion engine |
JP4359798B2 (en) | 1999-11-05 | 2009-11-04 | 株式会社Ihi | Exhaust turbine turbocharger |
EP1186781B2 (en) * | 2000-09-08 | 2012-05-30 | ABB Turbo Systems AG | Filter silencer mounting device for turbo charger inlet |
DE102004028133C5 (en) * | 2004-06-09 | 2017-10-26 | Man Diesel & Turbo Se | Turbomachine, in particular exhaust gas turbocharger |
DE102004055429B3 (en) * | 2004-11-17 | 2006-08-10 | Man B & W Diesel Ag | Sealing device for a particularly lubricated at standstill bearing a rotor shaft |
DE102005039820B4 (en) * | 2005-08-22 | 2007-06-28 | Man Diesel Se | Containment safety device for turbomachinery with radial flow compressor wheel |
KR200422136Y1 (en) * | 2006-05-04 | 2006-07-24 | 남순선 | Clamp coupling the gas pipe |
EP1860284A1 (en) * | 2006-05-23 | 2007-11-28 | ABB Turbo Systems AG | Casings assembling |
JP2010501770A (en) * | 2006-08-24 | 2010-01-21 | アーベーベー ターボ システムズ アクチエンゲゼルシャフト | Filter muffler mounting equipment |
JP4826417B2 (en) * | 2006-09-29 | 2011-11-30 | 株式会社ジェイテクト | Supercharger |
JP5526999B2 (en) * | 2010-05-10 | 2014-06-18 | 株式会社Ihi | Silencers and turbochargers |
DE102010028975A1 (en) * | 2010-05-14 | 2012-03-29 | Abb Turbo Systems Ag | Additional compressor housing |
DE112011102932T5 (en) * | 2010-09-03 | 2013-07-18 | Borgwarner Inc. | Turbocharger housing seal |
DE102011010673A1 (en) * | 2011-02-08 | 2012-08-09 | Voith Patent Gmbh | Housing for an exhaust gas turbocharger or a turbocompound system |
JP2011174477A (en) * | 2011-06-17 | 2011-09-08 | Jtekt Corp | Supercharger |
US8857178B2 (en) * | 2011-06-28 | 2014-10-14 | Caterpillar Inc. | Nozzled turbocharger turbine and associated engine and method |
KR101990880B1 (en) * | 2012-02-17 | 2019-06-19 | 보르그워너 인코퍼레이티드 | Multi-segment turbocharger bearing housing and methods therefor |
CN202614598U (en) * | 2012-05-21 | 2012-12-19 | 上海大学 | High-intensity steel plate stretching auxiliary clamping device |
CN102650296A (en) * | 2012-06-11 | 2012-08-29 | 重庆江增船舶重工有限公司 | High-speed and small-flow centrifugal type compressor set |
-
2013
- 2013-09-25 JP JP2013198638A patent/JP6097188B2/en active Active
-
2014
- 2014-06-30 KR KR1020167002207A patent/KR101799707B1/en active IP Right Grant
- 2014-06-30 EP EP14849505.4A patent/EP3009633B1/en active Active
- 2014-06-30 WO PCT/JP2014/067415 patent/WO2015045541A1/en active Application Filing
- 2014-06-30 CN CN201710818678.4A patent/CN107701298B/en active Active
- 2014-06-30 EP EP16205770.7A patent/EP3173630B1/en active Active
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
EP3009633B1 (en) | 2020-02-05 |
CN107701298B (en) | 2020-03-27 |
JP2015063956A (en) | 2015-04-09 |
JP6097188B2 (en) | 2017-03-15 |
CN107701298A (en) | 2018-02-16 |
WO2015045541A1 (en) | 2015-04-02 |
EP3009633A4 (en) | 2016-09-14 |
KR20160023893A (en) | 2016-03-03 |
EP3009633A1 (en) | 2016-04-20 |
CN105531460A (en) | 2016-04-27 |
EP3173630A1 (en) | 2017-05-31 |
KR101799707B1 (en) | 2017-11-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2317421C2 (en) | Turbosupercharger and device for axial fixing of shaft | |
JP5906356B2 (en) | Apparatus and method for assembling damper bearing assembly | |
JP5894203B2 (en) | Supercharger manufacturing method | |
US7001155B2 (en) | Compressor impeller with stress riser | |
EP2110531A1 (en) | Exhaust gas turbocharger | |
RU2599219C2 (en) | Fan rotor blade of jet engine for aircraft | |
EP3324053B1 (en) | Compression device and supercharger | |
KR20060045627A (en) | Compressor housing | |
EP3173630B1 (en) | Compressor and turbocharger | |
CN103806960B (en) | Turbomachinery bearing assembly pre-load arrangement | |
US9206733B2 (en) | Turbocharger assembly with direct-mounted bearing housing | |
US20160208821A1 (en) | Exhaust gas turbocharger | |
JP6284637B2 (en) | compressor | |
JP5254426B2 (en) | compressor | |
JP5230590B2 (en) | Exhaust inlet casing of exhaust turbine supercharger | |
KR101914425B1 (en) | Assembly method of impeller assembly, supercharger and impeller assembly | |
US11060453B2 (en) | Turbocharger with predetermined breaking point for an internal combustion engine | |
WO2017094546A1 (en) | Attachment mechanism and supercharger | |
JP6933301B2 (en) | Rotating body and supercharger | |
JP2011080453A (en) | Fastening member and supercharger | |
JP7143028B2 (en) | Exhaust turbocharger bearing structure | |
KR102646973B1 (en) | Bearing structure, supercharger equipped with the same, and method of assembling the supercharger | |
KR20080034698A (en) | Compression protecting snap ring | |
RU2553889C1 (en) | Gas turbine engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED |
|
AC | Divisional application: reference to earlier application |
Ref document number: 3009633 Country of ref document: EP Kind code of ref document: P |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20171024 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20180508 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F02B 39/00 20060101ALN20180420BHEP Ipc: F02M 35/12 20060101ALN20180420BHEP Ipc: F04D 29/62 20060101ALI20180420BHEP Ipc: F04D 29/42 20060101AFI20180420BHEP |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AC | Divisional application: reference to earlier application |
Ref document number: 3009633 Country of ref document: EP Kind code of ref document: P |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: GB Ref legal event code: FG4D Ref country code: AT Ref legal event code: REF Ref document number: 1030117 Country of ref document: AT Kind code of ref document: T Effective date: 20180815 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602014030698 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20180815 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 1030117 Country of ref document: AT Kind code of ref document: T Effective date: 20180815 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20181115 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20181115 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20181116 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20181215 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602014030698 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20190516 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20181215 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20140630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20180815 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20230702 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20240509 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20240507 Year of fee payment: 11 |