GB2108243A - Thermal insulation of blade wheel of turbo-machine - Google Patents

Thermal insulation of blade wheel of turbo-machine Download PDF

Info

Publication number
GB2108243A
GB2108243A GB08229060A GB8229060A GB2108243A GB 2108243 A GB2108243 A GB 2108243A GB 08229060 A GB08229060 A GB 08229060A GB 8229060 A GB8229060 A GB 8229060A GB 2108243 A GB2108243 A GB 2108243A
Authority
GB
United Kingdom
Prior art keywords
blade wheel
flange
machine
aturbo
shaft
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.)
Withdrawn
Application number
GB08229060A
Inventor
Georg Wahl
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.)
Voith Turbo GmbH and Co KG
Original Assignee
Voith Turbo GmbH and Co KG
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 Voith Turbo GmbH and Co KG filed Critical Voith Turbo GmbH and Co KG
Publication of GB2108243A publication Critical patent/GB2108243A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D57/00Liquid-resistance brakes; Brakes using the internal friction of fluids or fluid-like media, e.g. powders
    • F16D57/04Liquid-resistance brakes; Brakes using the internal friction of fluids or fluid-like media, e.g. powders with blades causing a directed flow, e.g. Föttinger type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D33/00Rotary fluid couplings or clutches of the hydrokinetic type
    • F16D33/18Details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H41/00Rotary fluid gearing of the hydrokinetic type
    • F16H41/24Details
    • F16H41/30Details relating to venting, lubrication, cooling, circulation of the cooling medium

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Braking Arrangements (AREA)

Abstract

A blade wheel 11 of a turbo- machine, especially a hydrodynamic coupling or brake, comprises a ring of blades 13 and a flange 14 located radially within the latter. This flange 14 serves for fastening the blade wheel 11 to a shaft 19, hub or the like. Such a blade wheel 11 rotates at very high speeds under certain circumstances; it is also occasionally subjected to a high heat load. In order to reduce the high material stresses resulting from this in the transitional region between the ring of blades 13 and the flange 14, a thermal insulation layer 16 is provided between the flange 14 and a flange 15 located on the shaft 19. <IMAGE>

Description

SPECIFICATION Turbo-machine The invention relates to turbo-machines, and is concerned particularly although not exclusively with blade wheels of hydrodynamic couplings, brakes and torque converters.
Hydrodyanamic couplings are known, for example from German Patent Specifications 883987 and 1 600 974. Although the blade wheels of such hydrody namic couplings rotate at very high speeds under certain circumstances and are therefore stressed severely, these couplings have proved to be of great value for decades. An essential advantage of a hydrodynamic coupling is that, when it is used to transmit force from a prime moverto a working machine, very gentle starting can be achieved even when heavy masses are to be accelerated. At the same time, the prime mover can, at first, run up with only a slight load, after which the hydrodynamic coupling accelerates the working machine at an essentially constant torque.
Consequently, in such a starting operation, the hydrodynamic coupling initially works with a high slip. This means that for a certain period of time there is an energy loss which becomes noticeable in heating the working fluid of the hydrodynamic coupling.
Similar conditions prevail in a hydrodynamic brake, although, as is known, this operates constant lywitha 100% slip.
To eliminate the heat due to energy loss, it is known, for example, to provide an external cooling circuit for the working fluid. That is to say, some of the working fluid is constantly extracted from the coupling or brake and re-cycled via a cooling device.
In many cases, however, especially as regards hydrodynamic couplings, the outlay for an external cooling circuit is unreasonably high. Many known hydrodynamic couplings are therefore operated without an external cooling circuit. But, in this case, operation with a high clutch slip must be kept within limits so as to prevent an excessive incidence of heat. At the same time, for safety purposes, there may be an automatic emptying device which, when a specific temperature is exceeded, causes the working fluid to flow off outwards. However, this means an interruption of operation, which is in many cases undesirable.
Afurther problem arising in the operation of hydrodynamic couplings (or brakes) is that it is customary for the blade wheel to have a fastening flange in the radially inner region. Investigations have shown that, in the transitional region between this flange and the ring of blades around it, such high stresses on the material arise under certain conditions that the permissible values are exceeded.
Attempts have been made to solve this problem by improved shaping or by the use of materials with a higher loading capacity, but not with the desired success.
An object of preferred embodiments of the invention is to reduce such undue material stresses in the transitional region between the flange and the ring of blades with as low an outlay as possible.
According to the present invention, there is pro vided a turbo-machine having a blade wheel mounted on another part of the machine, with insulation interposed between the blade wheel and said part.
The invention is based on the foliowing finding, which is explained by way of example, with refer ence to a hydrodynamic coupling, having two rings of blades which afford a very large surface against which working fluid flows. During a starting operation, the working fluid which heats up rapidly flows at a high velocity along the surfaces of the blade wheel. Thus, the mass of the blade wheel is heated very quickly. In contrast to this, the mass of the shaft (or hub) to which the blade wheel is fastened, by means of a flange, is heated very much more slowly because the surface of the shaft (or hub) against which the working fluid flows amounts to only a small fraction (for example, approximately 1/30) of the corresponding surface of the ring of blades.The result of this is, apparently, that the shaft (or the hub) extracts heat from the flange of the blade wheel, so that a substantially lower temperature is established in the flange than in the ring of blades. This would seem to lead, in the transitional region between the flange and ring of blades, to high thermal stresses which are added to the purely mechanical operating stresses. The unduly high material stresses mentioned above arise in this way.
The thermal insulation provided, according to the invention, between, for example, the flange of the blade wheel and, for example, the shaft (or the hub) on which the blade wheel 1 is mounted acts in such a way that when the blade wheel is heated much less heat is extracted from the flange than hitherto. That is to say, the flange assumes essentially the same temperature as the ring of blades. Thus, the occurence of thermal stress in the transitional region between the flange and the ring of blades may be at least substantially prevented and the danger of excessive stress on the material may be overcome.
For a better understanding of the invention, and to show how the same may be carried into effect, reference will now be made, by way of example, to the accompanying diagrammatic drawing, the single Figure of which shows a hydrodynamic coupling in partial longitudinal section.
The essential parts of the hydraulic coupling illustrated are a drive shaft 9, an impeller blade wheel 10 fastened to the latter, a coupling housing 12 rotating with the impeller blade wheel 10, and also a driven shaft 19 on which a turbine blade wheel 11 is mounted. The turbine blade wheel 11 comprises in the conventional way a ring of blades 13 and a fastening flange 14. A corresponding flange 15 is provided on the driven shaft 19. The two flanges 14 and 15 are connected to one another by bolts 8. A thermally insulating disc 16, the effect of which has been described above, is provided between the two flanges 14 and 15.
The inside diameter of the blade wheel flange 14 forms in a conventional way a cylindrical centering surface by means of which the blade wheel rests on the shaft 19. Theoretically, a thermally insulating ring could also be arranged here. It has been shown, however, that such an additional measure is not always essential. It may be appropriate, nevertheless, to make the axial length of the centering surface smaller than the thickness of the flange 14, in order thereby to reduce even further the transfer of heat to the shaft 19. The same purpose could also be served by inserting between the heads of the bolts 8 and the flange 14 washers which are made of a thermally insulating material.
In the coupling design illustrated, it is generally sufficient to provide a thermally insulating disc 16 on the one inner blade wheel 11 only. If required, however, the same measure can also be taken on the other blade wheel, as, for example, in the case of a design according to German Patent Specification 1 600 974.

Claims (10)

1. Aturbo-machine having a blade wheel mounted on another part of the machine, with thermal insulating interposed between the blade wheel and said part.
2. Aturbo-machine according to Claim 1,wherein in the blade wheel has a radially inner flange by means of which it is secured to said part.
3. Aturbo-machine according to Claim 1 or 2, wherein said part is a shaft.
4. A turbo-machine according to Claims 2 and 3, wherein the shaft is provided with a flange to one side of which the flange of the blade wheel is secured.
5. Aturbo-machine according to Claim 4, wherein said thermal insulation comprises a disc interposed axially between said flanged.
6. Aturbo-machine according to Claim 3,4 or 5, wherein said thermal insulation is interposed radially between the blade wheel and the shaft.
7. A turbo-machine according to Claim 3,4 or 5, wherein the blade wheel has a radially inner surface of reduced cross-section, which is mounted on the shaft.
8. Aturbo-machine according to any preceding claim, wherein said thermal insulation insulated all surfaces of the blade wheel adjacent said part.
9. Aturbo-machine according to any preceding claim, being a hydrodynamic coupling, brake, or torque converter.
10. Aturbo-machine substantially as hereinbefore described with reference to the accompanying drawing.
GB08229060A 1981-10-28 1982-10-12 Thermal insulation of blade wheel of turbo-machine Withdrawn GB2108243A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3142622 1981-10-28

Publications (1)

Publication Number Publication Date
GB2108243A true GB2108243A (en) 1983-05-11

Family

ID=6144952

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08229060A Withdrawn GB2108243A (en) 1981-10-28 1982-10-12 Thermal insulation of blade wheel of turbo-machine

Country Status (4)

Country Link
JP (1) JPS5884232A (en)
FR (1) FR2515252A1 (en)
GB (1) GB2108243A (en)
IT (2) IT8236073V0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1050664A2 (en) * 1999-05-07 2000-11-08 ROLLS-ROYCE plc Rotor-shaft connection

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE883987C (en) * 1949-06-11 1953-07-23 Voith Gmbh J M Flow coupling, especially for motor vehicle drives with internal combustion engines and for electrical transmission with squirrel cage motors
DE1600974B1 (en) * 1967-03-22 1970-06-18 Voith Getriebe Kg Emptying device for flow circuits
FR1580541A (en) * 1967-07-26 1969-09-05

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1050664A2 (en) * 1999-05-07 2000-11-08 ROLLS-ROYCE plc Rotor-shaft connection
EP1050664A3 (en) * 1999-05-07 2002-05-15 ROLLS-ROYCE plc Rotor-shaft connection
US6447252B1 (en) 1999-05-07 2002-09-10 Rolls-Royce Plc Rotor-shaft connector

Also Published As

Publication number Publication date
IT8236073V0 (en) 1982-10-15
JPS5884232A (en) 1983-05-20
FR2515252A1 (en) 1983-04-29
IT8249283A0 (en) 1982-10-15
IT1149107B (en) 1986-12-03

Similar Documents

Publication Publication Date Title
US2577134A (en) Radial spline impeller drive for turbochargers
US4986397A (en) Lock-up piston plate for recirculating flow torque converter
US3613851A (en) Segmented friction member for brake or clutch
US2412432A (en) Brake rotor
US2841262A (en) Clutch
EP0011390A1 (en) Hydraulically actuated clutch
US6929105B2 (en) Fully filled wet clutch with hydrodynamic cooling
US2464754A (en) Brake rotor
JPS61248926A (en) Heat-resistant disk brake for wheel of aircraft, etc.
US3304052A (en) Rotor structure for an elastic fluid utilizing machine
US3483953A (en) Disc element construction for disc brake
US3605441A (en) Installation for the transmission of torque between a turbine rotor and a transmission and method of manufacture thereof
GB2108243A (en) Thermal insulation of blade wheel of turbo-machine
US3746139A (en) Friction disc member for brake or clutch
US4560048A (en) Cooling system for friction clutches for vehicles
US3547235A (en) Hydrodynamic and friction coupling
US2185498A (en) Hoist
US2345410A (en) Clutch and brake mechanism
US4214651A (en) Friction disc for an aircraft brake
US2742107A (en) Brakes
US3786904A (en) Segmented friction member assembly
US3983972A (en) Friction disc apparatus
US3077334A (en) Pin-bushed turbine wheel
US3029902A (en) Hydro-kinetic brakes and couplings
US3081856A (en) Torque transmitting mechanism

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)