WO2001031229A2 - Method and apparatus for adjusting lubricant temperature within a gearbox - Google Patents
Method and apparatus for adjusting lubricant temperature within a gearbox Download PDFInfo
- Publication number
- WO2001031229A2 WO2001031229A2 PCT/US2000/041563 US0041563W WO0131229A2 WO 2001031229 A2 WO2001031229 A2 WO 2001031229A2 US 0041563 W US0041563 W US 0041563W WO 0131229 A2 WO0131229 A2 WO 0131229A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- lubricant
- temperature
- heat exchanger
- mechanical housing
- outlet
- Prior art date
Links
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
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/04—Features relating to lubrication or cooling or heating
- F16H57/0412—Cooling or heating; Control of temperature
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
Definitions
- the present invention relates generally to the field of lubrication systems. More particularly, one embodiment of the present invention contemplates a gearbox lubrication system wherein the lubricant temperature utilized within the gearbox is adjusted to different temperatures prior to delivery to a specific gear mesh point and/or bearing.
- the present invention was developed for gas turbine engine applications, however certain applications may be outside of this field. Many gas turbine engines utilize a mechanical gearbox within their power train components to deliver power to a motive device.
- the mechanical efficiency of gearboxes has been the subject of extensive work by engineers in order to extend the performance envelope of aircraft. It is widely understood that the aircraft's range, payload and operating ceiling can be increased if the efficiency of the mechanical gearbox is increased.
- the power loss in the mechanical gearbox is a function of many parameters including sliding losses, windage losses, lubricant churning losses, rolling traction losses and material hysteretic losses.
- the sliding friction losses in the gears and bearings account for a large portion of the power loss.
- gearboxes include a lubrication system designed and developed to deliver a lubricant to the gear meshes and bearings within the gearbox.
- Prior lubrication systems typically cool the lubricant to a single uniform temperature and this uniform temperature lubricant is then delivered to cool and lubricate the gear meshes and bearings.
- a conventional design practice was to cool the lubricant to the requirement of the most critical gear mesh or bearing. This practice results in the lubricant being too cool for optimum efficiency for many of the other gear meshes and bearings within the gearbox.
- There are a variety of lubrication systems that have been conceived of over the years. While these prior lubrication systems are steps in the right direction the need for additional improvement still remains. The present invention satisfies this need in a novel and unobvious way.
- One form of the present invention contemplates a lubrication system in which the lubricant temperature is adjusted to meet the individual parameters associated with gear mesh points and/or the bearing requirements of a gearbox.
- Another form of the present invention contemplates a method for lubricating components within a gearbox.
- the method comprises: adjusting the temperature of a first quantity of the lubricant to a first temperature; delivering at least a portion of the first quantity of the lubricant at the first temperature to a first location within the gearbox; changing the temperature of a second quantity of the lubricant to a second temperature; and, delivering at least a portion of the second quantity of the lubricant at the second temperature to a second location within the gearbox.
- Another form of the present invention contemplates a system, comprising: a mechanical housing having a plurality of mesh points therein, and the mechanical housing is adapted to hold a lubricant; a first lubricant heat exchanger in heat transfer relationship with a first quantity of lubricant, the first lubricant heat exchanger is adapted to change the temperature of the first quantity of lubricant to a first temperature, wherein at least a portion of the first quantity of lubricant exits the first heat exchanger at the first temperature and is delivered to a first one of the plurality of mesh points within the mechanical housing; and, a second lubricant heat exchanger in heat transfer relationship with a second quantity of lubricant, the second lubricant heat exchanger is adapted to change the temperature of the second quantity of lubricant to a second temperature, wherein at least a portion of the second quantity of lubricant exits the second heat exchanger at the second temperature and is delivered to a second one of the plurality of mesh points within the mechanical housing
- the present invention contemplates a gearbox, comprising: a mechanical housing adapted to have a lubricant therein; a first gear set positioned within the mechanical housing, the first gear set defines a first gear mesh; a second gear set positioned within the mechanical housing, the second gear set defines a second gear mesh; a first heat exchanger having a first lubricant inlet and a first lubricant outlet, the first lubricant inlet is in fluid communication with the mechanical housing and the lubricant exiting the first lubricant outlet has had its temperature changed to a first predetermined temperature by the first heat exchanger; a second heat exchanger having a second lubricant inlet and a second lubricant outlet, the second lubricant inlet is in fluid communication with the mechanical housing and the lubricant exiting the second lubricant outlet has had its temperature changed to a second predetermined temperature by the second heat exchanger; and, a lubricant delivery system within the mechanical housing, the lubricant delivery system
- the present invention contemplates a gearbox, comprising: a mechanical housing adapted to have a lubricant therein; a first gear set positioned within the mechanical housing, the first gear set defines a first gear mesh; a second gear set positioned within the mechanical housing, the second gear set defines a second gear mesh; a first heat exchanger having a first lubricant inlet and a first lubricant outlet, the first lubricant inlet is in fluid communication with the mechanical housing and the lubricant exiting the first lubricant outlet has been cooled to a first predetermined temperature by the first heat exchanger; a second heat exchanger having a second lubricant inlet and a second lubricant outlet, the second lubricant inlet is in fluid communication with the first lubricant outlet and adapted to receive a portion of the lubricant cooled to the first predetermined temperature, and the lubricant exiting the second lubricant outlet has been cooled to a second predetermined temperature by the second heat
- FIG. 1 is an illustrative view of a typical helicopter including a lubrication temperature adjustment system of the present invention.
- FIG. 2 is a block diagram of a gas turbine engine coupled to a gearbox including a lubrication adjustment system of the present invention.
- FIG. 3 is a schematic illustration of one embodiment of the lubrication adjustment system of the present invention.
- FIG. 4 is a schematic illustration of an alternate embodiment of the lubrication adjustment system of the present invention.
- FIG. 5 is a sectional view of a gearbox including a planet output gear set.
- FIG. 1 there is illustrated a side elevational view of a helicopter 20.
- the helicopter 20 includes a main rotor 21 and a tail rotor 22.
- a gas turbine engine propulsion system 23 drives the rotors 21 and 22.
- the present invention is applicable to many fields and has particular application in the aircraft industry.
- the term aircraft is generic and includes helicopters, airplanes, missiles, unmanned space devices and other substantially similar devices.
- FIG 2 there is illustrated a block diagram of the gas turbine engine 23 coupled to a gear box 24.
- the gas turbine engine includes a compressor 25, a combustor 26 and a turbine 27. It is important to realize that there are a multitude of ways in which the gas turbine engine components can be linked together.
- the lubrication temperature adjustment system is designed to deliver a lubricant at a predetermined temperature to each of a plurality of points within the gearbox 24.
- the plurality of points is intended to include gear sets, bearings, and similar mechanical structures requiring lubrication and/or cooling by the lubricant within the gearbox housing.
- the lubrication temperature adjustment system will be described with reference to a gearbox having two gear mesh points, however, the present invention is useable with any number of mechanical points and is not intended herein to be limited to a gearbox having two gear mesh points. Further, while the description is set forth herein in terms of gear mesh points it is understood that the present inventions are equally applicable to other mechanical components requiring lubrication and/or cooling by the lubricant within the gearbox housing.
- the lubricant temperature adjustment system 40 includes a primary lubricant temperature adjuster 28 which receives a quantity of lubricant from within the gearbox 24.
- the lubricant delivered through input 41 into the primary lubricant temperature adjuster 28 has an initial temperature and the primary lubricant temperature adjuster 28 functions to adjust the temperature of the lubricant to a predetermined temperature prior to delivery at the gear mesh point one.
- a portion of the lubricant adjusted within and output from the primary lubricant temperature adjuster 28 is delivered to a secondary lubricant temperature adjuster 29 via input 43.
- the primary lubricant temperature adjuster 28 and the secondary lubricant temperature adjuster 29 are in fluid communication.
- the second lubricant temperature adjuster 29 adjusts the temperature of the lubricant entering through input 42 to a predetermined temperature for gear mesh point 2.
- the primary lubricant temperature adjuster 28 includes a cooler.
- the cooler includes a heat exchanger functioning to transfer energy between the lubricant and a cooling media.
- the cooling media includes but is not limited to air, and/or fuel.
- the secondary lubricant temperature adjuster 29 is connected in series with the primary lubricant temperature adjuster 28 and receives a portion of the lubricant from the primary adjuster 28.
- the secondary lubricant temperature adjuster 29 in one form includes a cooler, and more preferably is a heat exchanger functioning to transfer energy between the lubricant and a cooling media.
- the cooling media includes but is not limited to air, and/or fuel.
- the primary lubricant temperature adjuster 28 and the secondary lubricant temperature adjuster 29 are intended herein not to be limited to a specific type of cooler. Further, the present invention contemplates in one embodiment active feedback control to monitor and adjust the temperature of the lubricant being cooled by the heat exchangers.
- FIG. 4 there is illustrated an alternative embodiment of a lubricant temperature adjustment system 50.
- the lubricant temperature adjustment system 50 is substantially similar to the lubricant temperature adjustment system 40 discussed previously, however, the secondary lubricant temperature adjuster 51 is not coupled in series with the primary lubricant temperature adjuster 52.
- Each of the lubricant temperature adjusters 51 and 52 adjust the temperature of the input lubricant to a predetermined temperature necessary for the specific gear mesh point.
- the features and description of the primary lubricant temperature adjuster 52 and secondary lubricant temperature adjuster 51 are substantially similar to the description regarding FIG. 3. In one form the temperature adjustment of the lubricant by the primary lubricant adjuster 52 and the secondary lubricant adjuster 51 is taking place in a substantially parallel process.
- the lubrication temperature adjustment system includes a localized heater to heat the lubricant prior to delivery to a specific gear mesh point.
- the localized heater includes a coil type heater.
- the present invention includes heating the lubricant prior to delivery to the individual gear mesh points by other techniques, including, but not limited to mixing with uncooled oil.
- the localized heater can form part of a system that also cools lubricant for delivery to other points within the gearbox.
- a specific gear mesh or bearing has a critical lubrication temperature necessary in order to have a sufficient lubricant film thicknesses and the remaining bearing and/or gear meshes have a lower lubricant film thickness requirement.
- a portion of the lubricant within the gearbox passes through the primary lubricant temperature adjuster and its temperature is changed to a temperature suitable for all other mesh points and/or bearings except for the critical mesh point.
- a portion of the lubricant exiting from the primary temperature adjuster passes through the secondary lubricant temperature adjuster and the temperature of the lubricant is adjusted to the required temperature for the critical mesh point.
- the lubricant is not processed in series and each lubricant temperature adjuster changes the temperature of the lubricant to the temperature needed for delivery to a specific set site within the gearbox.
- gearbox and transmission will be used interchangeably unless specifically stated to the contrary and are intended to have a broad meaning and are not limited to the specific types of examples set forth in the description.
- the planet gear set is the critical mesh point from a lubrication standpoint.
- the planet output gear set mesh point needs a lubricant-in temperature of 180 degrees Fahrenheit to have sufficient lubricant film thicknesses, but all other points within the transmission need a lubrication-in temperature of 250 degrees Fahrenheit.
- the lubricant is routed through a cooler such that the lubrication-in temperature from the housing is about 250 degrees Fahrenheit for all the bearings and/or gear mesh points except the planet output gear set.
- the lubricant for the planet output gear set is routed through a supplementary cooler and cooled to 180 degrees Fahrenheit.
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU29180/01A AU2918001A (en) | 1999-10-25 | 2000-10-25 | Method and apparatus for adjusting lubricant temperature within a gearbox |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16128699P | 1999-10-25 | 1999-10-25 | |
US60/161,286 | 1999-10-25 | ||
US69439500A | 2000-10-23 | 2000-10-23 | |
US09/694,395 | 2000-10-23 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2001031229A2 true WO2001031229A2 (en) | 2001-05-03 |
WO2001031229A3 WO2001031229A3 (en) | 2001-09-13 |
Family
ID=26857694
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2000/041563 WO2001031229A2 (en) | 1999-10-25 | 2000-10-25 | Method and apparatus for adjusting lubricant temperature within a gearbox |
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WO (1) | WO2001031229A2 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4041697A (en) * | 1975-07-17 | 1977-08-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Oil cooling system for a gas turbine engine |
US4363216A (en) * | 1980-10-23 | 1982-12-14 | Lucien Bronicki | Lubricating system for organic fluid power plant |
US5054583A (en) * | 1990-05-15 | 1991-10-08 | Sundstrand Corporation | Bearing arrangement with centrifugal mist lubrication flow and isolate dead shaft conductive cooling flow |
US5465810A (en) * | 1994-10-07 | 1995-11-14 | Mobil Oil Corporation | Multi-phase lubricant and apparatus for the dispensing thereof |
-
2000
- 2000-10-25 WO PCT/US2000/041563 patent/WO2001031229A2/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4041697A (en) * | 1975-07-17 | 1977-08-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Oil cooling system for a gas turbine engine |
US4363216A (en) * | 1980-10-23 | 1982-12-14 | Lucien Bronicki | Lubricating system for organic fluid power plant |
US5054583A (en) * | 1990-05-15 | 1991-10-08 | Sundstrand Corporation | Bearing arrangement with centrifugal mist lubrication flow and isolate dead shaft conductive cooling flow |
US5465810A (en) * | 1994-10-07 | 1995-11-14 | Mobil Oil Corporation | Multi-phase lubricant and apparatus for the dispensing thereof |
Also Published As
Publication number | Publication date |
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WO2001031229A3 (en) | 2001-09-13 |
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