US20200025208A1 - Variable pitch fan assembly with blade pitch indication - Google Patents

Variable pitch fan assembly with blade pitch indication Download PDF

Info

Publication number
US20200025208A1
US20200025208A1 US16/042,250 US201816042250A US2020025208A1 US 20200025208 A1 US20200025208 A1 US 20200025208A1 US 201816042250 A US201816042250 A US 201816042250A US 2020025208 A1 US2020025208 A1 US 2020025208A1
Authority
US
United States
Prior art keywords
fan
rotation axis
piston
crank arm
variable pitch
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.)
Abandoned
Application number
US16/042,250
Inventor
Shaun J. Miller
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.)
Deere and Co
Original Assignee
Deere and Co
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 Deere and Co filed Critical Deere and Co
Priority to US16/042,250 priority Critical patent/US20200025208A1/en
Assigned to DEERE & COMPANY reassignment DEERE & COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MILLER, SHAUN J.
Priority to BR102019009976A priority patent/BR102019009976A2/en
Priority to CN201910530445.3A priority patent/CN110748501A/en
Publication of US20200025208A1 publication Critical patent/US20200025208A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/002Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by varying geometry within the pumps, e.g. by adjusting vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/34Blade mountings
    • F04D29/36Blade mountings adjustable
    • F04D29/362Blade mountings adjustable during rotation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P7/00Controlling of coolant flow
    • F01P7/02Controlling of coolant flow the coolant being cooling-air
    • F01P7/06Controlling of coolant flow the coolant being cooling-air by varying blade pitch
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/001Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/50Kinematic linkage, i.e. transmission of position

Definitions

  • the present disclosure relates to a variable pitch fan assembly.
  • the fan may be used to cool various components of the vehicle, such as the engine and coolers or other heat exchangers.
  • a variable pitch fan assembly comprises a fan configured to rotate about a fan rotation axis and comprising blades with a pitch that is variable, a piston connected to the fan and configured to move axially relative to the fan rotation axis to change the pitch of the blades, a rotary crank arm yieldably biased toward the piston, and a motion transmitter positioned in communication with the piston and the crank arm to transmit motion axially therebetween relative to the fan rotation axis, and a sensor positioned to detect an angular position of the crank arm, the angular position indicative of the pitch of the blades.
  • the variable pitch fan assembly may be included in a vehicle.
  • the sensor may generate a position signal indicative of the angular position and thus indicative of the blade pitch.
  • a control system of the vehicle may determine the blade pitch based on the position signal, and command the fan to a desired blade pitch to modulate airflow to a desired level. The control system may do so by controlling the axial position of the piston relative to the fan rotation axis.
  • FIG. 1 is an elevation view of a vehicle with a portion broken away showing a variable pitch fan assembly
  • FIG. 2 is a perspective view showing the variable pitch fan assembly
  • FIG. 3 is a partially exploded perspective view, taken along section lines 3 - 3 (with some portions remaining in solid);
  • FIG. 4 is an elevational view of the section of FIG. 3 , with some portions removed;
  • FIG. 5 is an enlarged view of a portion of FIG. 4 ;
  • FIG. 6 is an enlarged view of another portion of FIG. 4 .
  • a vehicle 10 comprises a variable pitch fan assembly 12 .
  • the fan assembly 12 is configured for cooling components of the vehicle 10 , such as the engine and various coolers or other heat exchangers.
  • the vehicle 10 may be any of a wide variety of vehicles, including, without limitation, agricultural, construction, or forestry vehicles.
  • the vehicle 10 is a cotton harvester.
  • the fan assembly 12 comprises a fan 14 with blades 16 (e.g., 9 blades).
  • the blades 16 have a pitch that is variable to modulate airflow to a desired level.
  • the fan 14 with its blades 16 is configured to rotate about a fan rotation axis 17 , and may be driven for rotation about the axis 17 in a conventional manner, such as, for example, hydraulically or pneumatically.
  • the fan 14 comprises a hub 18 and a sheave 20 , the hub 18 and the sheave 20 included in a fan housing 21 of the fan 14 .
  • the blades 16 are mounted to the hub 18 in, for example, a conventional manner to rotate with the hub 18 about the fan rotation axis 15 .
  • the sheave 20 is fastened to the hub 18 in fixed relation thereto.
  • the sheave 20 is mounted to a housing 22 of the fan assembly 12 via a bearing 23 (e.g., double tapered roller bearing), positioned between the housing 22 and the sheave 20 , for rotation relative to the housing 22 about the fan rotation axis 15 .
  • the bearing 23 is captured between a snap ring for the outer race and a retainer ring threaded onto the housing 22 . As such, the fan 14 is supported for rotation relative to the housing 22 about the fan rotation axis 15 .
  • the fan assembly 12 comprises a piston 24 connected to the blades 16 to change the pitch of the blades 16 .
  • the piston is configured to rotate with the fan 14 about the fan rotation axis, and is configured to move axially relative to the fan rotation axis 15 to change the pitch of the blades 16 .
  • the piston 24 moves in first and second axial directions 26 , 28 relative to the axis 15 to change the pitch of the blades 16 .
  • the piston 24 may be actuated fluidly, such as hydraulically, in the first axial direction 26 relative to the axis 15 .
  • the piston 24 may be actuated pneumatically, or in another manner, in the first axial direction 26 .
  • the piston 24 is yieldably biased in the second axial direction 28 opposite to the first axial direction 26 by a plurality of springs 29 positioned about the axis 15 between the piston 24 and the fan housing 21 (e.g., the sheave 20 of the fan housing 21 ) and in respective spring-receiving pockets of the piston 24 .
  • Movement of the piston 24 in either direction 26 , 28 causes the blades 16 to rotate correspondingly about their respective axes of rotation to change their pitch.
  • a rack and a pinion may be associated with each blade 16 to rotate the blade 16 (racks and pinions not shown).
  • each rack may be mounted to the piston 24 for axial movement therewith relative to the axis 15 , and each blade 16 may be over-molded or otherwise connected to a respective pinion that meshes with a respective rack.
  • Axial movement of the piston 24 and the racks mounted thereto causes the pinions and the blades 16 mounted respectively thereto to rotate and thereby change the pitch of the blades 16 .
  • the fan assembly 12 comprises a rotary crank arm 30 , a motion transmitter 32 , and a sensor 34 ( FIG. 3 ).
  • the crank arm 30 is yieldably biased toward the piston 24 in the first axial direction 26 and mounted to the housing 22 to rotate relative to the housing 22 about a crank rotation axis 36 .
  • the motion transmitter 32 is positioned in communication with the piston 24 and the crank arm 30 to transmit motion axially therebetween relative to the fan rotation axis 15 .
  • the sensor 34 is positioned to detect an angular position of the crank arm 30 relative to the crank rotation axis 36 . The angular position is indicative of the pitch of the blades 16 .
  • the fan assembly 12 comprises a bearing 38 mounted to the motion transmitter 32 for the piston 24 .
  • the piston 24 is connected to the motion transmitter 32 via the bearing 38 such that the piston 24 is configured to rotate relative to the motion transmitter 32 with the fan 14 about the fan rotation axis 15 .
  • the fan assembly 12 comprises a spacer 40 .
  • the spacer 40 contacts the bearing 38 and the piston 24 , with a biaser 60 urging the spacer 40 in the second axial direction 28 into contact with the piston 24 .
  • the spacer 40 contacts the outer race 42 of the bearing 38 , and spaces the piston 24 axially apart from the inner race 44 of the bearing 38 relative to the fan rotation axis 15 .
  • the spacer 40 is supported on the outer race 42 .
  • a ring 46 of the spacer 40 surrounds the outer race 42 .
  • a lip 48 of the spacer 40 extends radially from the ring 46 relative to the fan rotation axis 15 and axially between the bearing 38 and the piston 24 relation to the fan rotation axis 14 so as to space the piston 24 axially apart from the inner race 44 relative to the fan rotation axis 15 .
  • the spacer 40 is configured, for example, as a cap pressed onto the outer race 42 to establish an interference fit therebetween, and is made, for example, of steel.
  • the housing 22 comprises a cavity 50 and a bore 52 extending from the cavity 50 axially relative to the fan rotation axis 15 .
  • the crank arm 30 is positioned in the cavity 50 .
  • the motion transmitter 32 is positioned in the bore 52 for linear movement therein along the fan rotation axis 15 in the first and second axial directions 26 , 28 .
  • Two bushings 54 of the fan assembly 12 made, for example, of bronze, are pressed into the bore 52 so as to be positioned in the bore 52 in spaced apart relation to one another.
  • the motion transmitter 32 is positioned in the bushings 54 so as to be supported thereby in the bore 52 for axial and rotational movement relative to the fan rotation axis 15 and relative to the bushings 54 and the housing 22 .
  • Rotation of the motion transmitter 32 may be induced by rotation of the piston 24 mounted to the motion transmitter 32 via the bearing 38 and the spacer 40 .
  • the motion transmitter 32 is mounted for both axial and rotational movement about the fan rotation axis 15 .
  • the motion transmitter 32 is positioned to transmit motion linearly between the piston 24 and the crank arm 30 along the fan rotation axis 15 .
  • the motion transmitter 32 may be configured, for example, as a rod or other suitable linear member for such linear movement.
  • the crank arm 30 is positioned in the cavity 50 , and is mounted to the housing 22 for rotation about the crank rotation axis 36 .
  • the crank arm 30 is integrated with an axle 56 to form a one-piece construction, although in other embodiments the crank arm 30 and the axle 56 may be separate components.
  • the axle 56 is mounted for rotation about the crank rotation axis 36 via two bearings 58 (e.g., needle roller bearings). Each bearing 58 is mounted in a corresponding small bore of the housing 22 .
  • the crank arm 30 extends radially from the axle 56 relative to the crank rotation axis 36 .
  • a biaser 60 yieldably biases the crank arm 30 toward the piston 24 .
  • the biaser 60 is configured, for example, as a torsion spring.
  • one end of the biaser 60 presses against a post 62 mounted to the crank arm 30 (e.g., threaded or pressed into the crank arm 30 ), and the opposite end of the biaser 60 presses against a tab 64 of the housing 22 positioned in the cavity 50 (the portion of the tab 64 that the biaser 60 contacts is not actually shown but is indicated in FIG. 4 and would be understood by one of ordinary skill in the art).
  • the motion transmitter 32 and the crank arm 30 are positioned in slidable contact with one another.
  • the motion transmitter 32 and the crank arm 30 cooperate to provide a spherical interface 66 therebetween.
  • the spherical interface 66 inhibits axial play of the crank arm 30 and the axle 56 along the crank rotation axis 36 , and accommodates rotation of the motion transmitter 32 about the fan rotation axis 15 .
  • the crank arm 30 comprises a groove 68
  • the motion transmitter 32 comprises an end portion 60 received in the groove 68
  • the end portion 70 is spherical
  • the groove 68 is a spherical groove receiving the spherical end portion 70 .
  • the groove 68 extends lengthwise along a periphery 72 of the crank arm 30 , and lies in an imaginary plane 74 perpendicular to the crank rotation axis 36 (the plane 74 (the plane 74 coincides with the section plane of FIG. 6 and is indicated in FIG. 6 as a dashed box for sake of illustration).
  • the groove 68 may be machined into the periphery 72 .
  • the spherical interface 66 may be wear resistant.
  • the motion transmitter 32 may be made, for example, of stainless steel so as to be anti-corrosive.
  • the crank arm 30 and axle 56 may be made, for example, of hardened steel (e.g., heat-treated) so as to be wear-resistant and not wear prematurely.
  • the motion transmitter 32 and the crank arm 30 slide against one another when the motion transmitter 32 and the piston 24 move along the fan rotation axis 15 in the first and second axial directions 26 , 28 .
  • motion is converted between rotary motion of the crank arm 30 and linear motion of the motion transmitter 32 and the piston 24 .
  • the blades 16 rotate proportionally to this axial and linear movement of the motion transmitter 32 and piston 24 .
  • the axle 56 and the sensor 34 are connected to one another such that rotation of the crank arm 30 about the crank rotation axis 36 is detected by the sensor 34 via corresponding rotation of the axle 56 about the crank rotation axis 36 .
  • the axle 56 and the sensor 34 may be keyed to one another such that rotation of the axle 56 causes rotation of a corresponding sleeve of the sensor 34 .
  • a key of the sleeve may be received by a keyway of the axle 56 .
  • the axle 56 and the sleeve may have the key and the keyway, respectively.
  • the axle 56 and the sensor 34 may be connected to one another in other ways (e.g., splined, or interference fit).
  • the sensor 34 detects the angular position of the crank arm 30 relative to the crank rotation axis 36 , with the angular position being indicative of the pitch of the blades 16 .
  • the sensor 34 may be configured, for example, as a rotary potentiometer that outputs a position signal (e.g., analog), proportional to the pitch of the blades 16 .
  • the position signal is proportional to the angular position of the crank arm 30 and thus the blade pitch. As such, the position is indicative the angular position and the blade pitch.
  • the position signal may be used in by a control system on board the vehicle 10 to control the blades 16 to a desired blade pitch to modulate airflow to a desired level.
  • the control system e.g., a controller thereof
  • the control system may receive the position signal and determine the blade pitch based on the position signal.
  • the control system may then control the blade pitch via the axial position of the piston 24 relative to the fan rotation axis 15 .

Abstract

A variable pitch fan assembly comprises a fan configured to rotate about a fan rotation axis and comprising blades with a pitch that is variable, a piston connected to the fan and configured to move axially relative to the fan rotation axis to change the pitch of the blades, a rotary crank arm yieldably biased toward the piston, and a motion transmitter positioned in communication with the piston and the crank arm to transmit motion axially therebetween relative to the fan rotation axis, and a sensor positioned to detect an angular position of the crank arm, the angular position indicative of the pitch of the blades.

Description

    FIELD OF THE DISCLOSURE
  • The present disclosure relates to a variable pitch fan assembly.
  • BACKGROUND OF THE DISCLOSURE
  • It is common for vehicles to employ a fan for cooling purposes. The fan may be used to cool various components of the vehicle, such as the engine and coolers or other heat exchangers.
  • SUMMARY OF THE DISCLOSURE
  • According to an aspect of the present disclosure, a variable pitch fan assembly comprises a fan configured to rotate about a fan rotation axis and comprising blades with a pitch that is variable, a piston connected to the fan and configured to move axially relative to the fan rotation axis to change the pitch of the blades, a rotary crank arm yieldably biased toward the piston, and a motion transmitter positioned in communication with the piston and the crank arm to transmit motion axially therebetween relative to the fan rotation axis, and a sensor positioned to detect an angular position of the crank arm, the angular position indicative of the pitch of the blades.
  • The variable pitch fan assembly may be included in a vehicle. The sensor may generate a position signal indicative of the angular position and thus indicative of the blade pitch. A control system of the vehicle may determine the blade pitch based on the position signal, and command the fan to a desired blade pitch to modulate airflow to a desired level. The control system may do so by controlling the axial position of the piston relative to the fan rotation axis.
  • The above and other features will become apparent from the following description and accompanying drawings.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The detailed description of the drawings refers to the accompanying figures in which:
  • FIG. 1 is an elevation view of a vehicle with a portion broken away showing a variable pitch fan assembly;
  • FIG. 2 is a perspective view showing the variable pitch fan assembly;
  • FIG. 3 is a partially exploded perspective view, taken along section lines 3-3 (with some portions remaining in solid);
  • FIG. 4 is an elevational view of the section of FIG. 3, with some portions removed;
  • FIG. 5 is an enlarged view of a portion of FIG. 4; and
  • FIG. 6 is an enlarged view of another portion of FIG. 4.
  • DETAILED DESCRIPTION OF THE DRAWINGS
  • Referring to FIG. 1, a vehicle 10 comprises a variable pitch fan assembly 12. The fan assembly 12 is configured for cooling components of the vehicle 10, such as the engine and various coolers or other heat exchangers. The vehicle 10 may be any of a wide variety of vehicles, including, without limitation, agricultural, construction, or forestry vehicles. Illustratively, the vehicle 10 is a cotton harvester.
  • Referring to FIG. 2, the fan assembly 12 comprises a fan 14 with blades 16 (e.g., 9 blades). The blades 16 have a pitch that is variable to modulate airflow to a desired level. The fan 14 with its blades 16 is configured to rotate about a fan rotation axis 17, and may be driven for rotation about the axis 17 in a conventional manner, such as, for example, hydraulically or pneumatically.
  • The fan 14 comprises a hub 18 and a sheave 20, the hub 18 and the sheave 20 included in a fan housing 21 of the fan 14. The blades 16 are mounted to the hub 18 in, for example, a conventional manner to rotate with the hub 18 about the fan rotation axis 15. The sheave 20 is fastened to the hub 18 in fixed relation thereto. The sheave 20 is mounted to a housing 22 of the fan assembly 12 via a bearing 23 (e.g., double tapered roller bearing), positioned between the housing 22 and the sheave 20, for rotation relative to the housing 22 about the fan rotation axis 15. The bearing 23 is captured between a snap ring for the outer race and a retainer ring threaded onto the housing 22. As such, the fan 14 is supported for rotation relative to the housing 22 about the fan rotation axis 15.
  • Referring to FIGS. 3 and 4, the fan assembly 12 comprises a piston 24 connected to the blades 16 to change the pitch of the blades 16. The piston is configured to rotate with the fan 14 about the fan rotation axis, and is configured to move axially relative to the fan rotation axis 15 to change the pitch of the blades 16.
  • The piston 24 moves in first and second axial directions 26, 28 relative to the axis 15 to change the pitch of the blades 16. The piston 24 may be actuated fluidly, such as hydraulically, in the first axial direction 26 relative to the axis 15. In other embodiments, the piston 24 may be actuated pneumatically, or in another manner, in the first axial direction 26. The piston 24 is yieldably biased in the second axial direction 28 opposite to the first axial direction 26 by a plurality of springs 29 positioned about the axis 15 between the piston 24 and the fan housing 21 (e.g., the sheave 20 of the fan housing 21) and in respective spring-receiving pockets of the piston 24.
  • Movement of the piston 24 in either direction 26, 28 causes the blades 16 to rotate correspondingly about their respective axes of rotation to change their pitch. A rack and a pinion may be associated with each blade 16 to rotate the blade 16 (racks and pinions not shown). In such a case, each rack may be mounted to the piston 24 for axial movement therewith relative to the axis 15, and each blade 16 may be over-molded or otherwise connected to a respective pinion that meshes with a respective rack. Axial movement of the piston 24 and the racks mounted thereto causes the pinions and the blades 16 mounted respectively thereto to rotate and thereby change the pitch of the blades 16.
  • The fan assembly 12 comprises a rotary crank arm 30, a motion transmitter 32, and a sensor 34 (FIG. 3). The crank arm 30 is yieldably biased toward the piston 24 in the first axial direction 26 and mounted to the housing 22 to rotate relative to the housing 22 about a crank rotation axis 36. The motion transmitter 32 is positioned in communication with the piston 24 and the crank arm 30 to transmit motion axially therebetween relative to the fan rotation axis 15. The sensor 34 is positioned to detect an angular position of the crank arm 30 relative to the crank rotation axis 36. The angular position is indicative of the pitch of the blades 16.
  • Referring to FIGS. 3-5, the fan assembly 12 comprises a bearing 38 mounted to the motion transmitter 32 for the piston 24. The piston 24 is connected to the motion transmitter 32 via the bearing 38 such that the piston 24 is configured to rotate relative to the motion transmitter 32 with the fan 14 about the fan rotation axis 15.
  • Referring to FIGS. 4 and 5, the fan assembly 12 comprises a spacer 40. The spacer 40 contacts the bearing 38 and the piston 24, with a biaser 60 urging the spacer 40 in the second axial direction 28 into contact with the piston 24. The spacer 40 contacts the outer race 42 of the bearing 38, and spaces the piston 24 axially apart from the inner race 44 of the bearing 38 relative to the fan rotation axis 15.
  • The spacer 40 is supported on the outer race 42. A ring 46 of the spacer 40 surrounds the outer race 42. A lip 48 of the spacer 40 extends radially from the ring 46 relative to the fan rotation axis 15 and axially between the bearing 38 and the piston 24 relation to the fan rotation axis 14 so as to space the piston 24 axially apart from the inner race 44 relative to the fan rotation axis 15. The spacer 40 is configured, for example, as a cap pressed onto the outer race 42 to establish an interference fit therebetween, and is made, for example, of steel.
  • Referring to FIGS. 3, 4, and 6, the housing 22 comprises a cavity 50 and a bore 52 extending from the cavity 50 axially relative to the fan rotation axis 15. The crank arm 30 is positioned in the cavity 50. The motion transmitter 32 is positioned in the bore 52 for linear movement therein along the fan rotation axis 15 in the first and second axial directions 26, 28. Two bushings 54 of the fan assembly 12, made, for example, of bronze, are pressed into the bore 52 so as to be positioned in the bore 52 in spaced apart relation to one another. The motion transmitter 32 is positioned in the bushings 54 so as to be supported thereby in the bore 52 for axial and rotational movement relative to the fan rotation axis 15 and relative to the bushings 54 and the housing 22. Rotation of the motion transmitter 32 may be induced by rotation of the piston 24 mounted to the motion transmitter 32 via the bearing 38 and the spacer 40. As such, the motion transmitter 32 is mounted for both axial and rotational movement about the fan rotation axis 15.
  • The motion transmitter 32 is positioned to transmit motion linearly between the piston 24 and the crank arm 30 along the fan rotation axis 15. The motion transmitter 32 may be configured, for example, as a rod or other suitable linear member for such linear movement.
  • Referring to FIG. 6, the crank arm 30 is positioned in the cavity 50, and is mounted to the housing 22 for rotation about the crank rotation axis 36. The crank arm 30 is integrated with an axle 56 to form a one-piece construction, although in other embodiments the crank arm 30 and the axle 56 may be separate components. The axle 56 is mounted for rotation about the crank rotation axis 36 via two bearings 58 (e.g., needle roller bearings). Each bearing 58 is mounted in a corresponding small bore of the housing 22. The crank arm 30 extends radially from the axle 56 relative to the crank rotation axis 36.
  • A biaser 60 yieldably biases the crank arm 30 toward the piston 24. The biaser 60 is configured, for example, as a torsion spring. In such a case, one end of the biaser 60 presses against a post 62 mounted to the crank arm 30 (e.g., threaded or pressed into the crank arm 30), and the opposite end of the biaser 60 presses against a tab 64 of the housing 22 positioned in the cavity 50 (the portion of the tab 64 that the biaser 60 contacts is not actually shown but is indicated in FIG. 4 and would be understood by one of ordinary skill in the art).
  • The motion transmitter 32 and the crank arm 30 are positioned in slidable contact with one another. The motion transmitter 32 and the crank arm 30 cooperate to provide a spherical interface 66 therebetween. The spherical interface 66 inhibits axial play of the crank arm 30 and the axle 56 along the crank rotation axis 36, and accommodates rotation of the motion transmitter 32 about the fan rotation axis 15.
  • The crank arm 30 comprises a groove 68, and the motion transmitter 32 comprises an end portion 60 received in the groove 68. Illustratively, the end portion 70 is spherical, and the groove 68 is a spherical groove receiving the spherical end portion 70. The groove 68 extends lengthwise along a periphery 72 of the crank arm 30, and lies in an imaginary plane 74 perpendicular to the crank rotation axis 36 (the plane 74 (the plane 74 coincides with the section plane of FIG. 6 and is indicated in FIG. 6 as a dashed box for sake of illustration). The groove 68 may be machined into the periphery 72.
  • The spherical interface 66 may be wear resistant. The motion transmitter 32 may be made, for example, of stainless steel so as to be anti-corrosive. The crank arm 30 and axle 56 may be made, for example, of hardened steel (e.g., heat-treated) so as to be wear-resistant and not wear prematurely.
  • As such, the motion transmitter 32 and the crank arm 30 slide against one another when the motion transmitter 32 and the piston 24 move along the fan rotation axis 15 in the first and second axial directions 26, 28. In this way, motion is converted between rotary motion of the crank arm 30 and linear motion of the motion transmitter 32 and the piston 24. As the motion transmitter 32 and the piston 24 move axially along the fan rotation axis 15, the blades 16 rotate proportionally to this axial and linear movement of the motion transmitter 32 and piston 24.
  • The axle 56 and the sensor 34 are connected to one another such that rotation of the crank arm 30 about the crank rotation axis 36 is detected by the sensor 34 via corresponding rotation of the axle 56 about the crank rotation axis 36. In an embodiment, the axle 56 and the sensor 34 may be keyed to one another such that rotation of the axle 56 causes rotation of a corresponding sleeve of the sensor 34. A key of the sleeve may be received by a keyway of the axle 56. In other embodiments, the axle 56 and the sleeve may have the key and the keyway, respectively. The axle 56 and the sensor 34 may be connected to one another in other ways (e.g., splined, or interference fit).
  • The sensor 34 detects the angular position of the crank arm 30 relative to the crank rotation axis 36, with the angular position being indicative of the pitch of the blades 16. The sensor 34 may be configured, for example, as a rotary potentiometer that outputs a position signal (e.g., analog), proportional to the pitch of the blades 16. The position signal is proportional to the angular position of the crank arm 30 and thus the blade pitch. As such, the position is indicative the angular position and the blade pitch. The position signal may be used in by a control system on board the vehicle 10 to control the blades 16 to a desired blade pitch to modulate airflow to a desired level. The control system (e.g., a controller thereof) may receive the position signal and determine the blade pitch based on the position signal. The control system may then control the blade pitch via the axial position of the piston 24 relative to the fan rotation axis 15.
  • While the above describes example embodiments of the present disclosure, these descriptions should not be viewed in a limiting sense. Rather, other variations and modifications may be made without departing from the scope and spirit of the present disclosure as defined in the appended claims.

Claims (15)

What is claimed is:
1. A variable pitch fan assembly, comprising:
a fan configured to rotate about a fan rotation axis and comprising blades with a pitch that is variable,
a piston connected to the fan and configured to move axially relative to the fan rotation axis to change the pitch of the blades,
a rotary crank arm yieldably biased toward the piston,
a motion transmitter positioned in communication with the piston and the crank arm to transmit motion axially therebetween relative to the fan rotation axis, and
a sensor positioned to detect an angular position of the crank arm, the angular position indicative of the pitch of the blades.
2. The variable pitch fan assembly of claim 1, comprising a bearing mounted to the motion transmitter, wherein the piston is connected to the motion transmitter via the bearing such that the piston is configured to rotate relative to the motion transmitter with the fan about the fan rotation axis.
3. The variable pitch fan assembly of claim 2, comprising a spacer, wherein the bearing comprises an outer race and an inner race, and the spacer is supported on the outer race and spaces the piston apart from the inner race.
4. The variable pitch fan assembly of claim 3, wherein the spacer contacts the bearing and the piston and comprises a ring surrounding the outer race and a lip extending radially from the ring relative to the fan rotation axis and axially between the bearing and the piston relative to the fan rotation axis so as to space the piston axially apart from the inner race relative to the fan rotation axis.
5. The variable pitch fan assembly of claim 2, comprising a housing and a bushing positioned in a bore of the housing, wherein the motion transmitter is positioned in the bushing for axial and rotational movement relative to the fan rotational axis.
6. The variable pitch fan assembly of claim 1, comprising a housing, wherein the fan is supported for rotation relative to the housing about the fan rotation axis, the housing comprises a cavity and a bore extending from the cavity, the crank arm is positioned in the cavity, and the motion transmitter is positioned in the bore for linear movement therein along the fan rotation axis.
7. The variable pitch fan assembly of claim 6, comprising a bushing positioned in the bore, and the motion transmitter is positioned in the bushing.
8. The variable pitch fan assembly of claim 1, wherein the motion transmitter and the crank arm are positioned in slidable contact with one another.
9. The variable pitch fan assembly of claim 1, wherein the crank arm comprises a groove, and the motion transmitter comprises an end portion received in the groove.
10. The variable pitch fan assembly of claim 1, wherein the motion transmitter and the crank arm cooperate to provide a spherical interface therebetween.
11. The variable pitch fan assembly of claim 10, wherein the motion transmitter comprises a spherical end portion, and the crank arm comprises a spherical groove receiving the spherical end portion.
12. The variable pitch fan assembly of claim 11, wherein the spherical groove extends lengthwise along a periphery of the crank arm.
13. The variable pitch fan assembly of claim 11, wherein the crank arm is configured to rotate about a crank rotation axis, and the spherical groove lies in an imaginary plane perpendicular to the crank rotation axis.
14. The variable pitch fan assembly of claim 1, wherein the motion transmitter is configured as a rod.
15. The variable pitch fan assembly of claim 1, wherein the motion transmitter is positioned to transmit motion linearly between the piston and the crank arm.
US16/042,250 2018-07-23 2018-07-23 Variable pitch fan assembly with blade pitch indication Abandoned US20200025208A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US16/042,250 US20200025208A1 (en) 2018-07-23 2018-07-23 Variable pitch fan assembly with blade pitch indication
BR102019009976A BR102019009976A2 (en) 2018-07-23 2019-05-16 set of variable pitch fans
CN201910530445.3A CN110748501A (en) 2018-07-23 2019-06-19 Variable pitch fan assembly with blade pitch indication

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16/042,250 US20200025208A1 (en) 2018-07-23 2018-07-23 Variable pitch fan assembly with blade pitch indication

Publications (1)

Publication Number Publication Date
US20200025208A1 true US20200025208A1 (en) 2020-01-23

Family

ID=69162870

Family Applications (1)

Application Number Title Priority Date Filing Date
US16/042,250 Abandoned US20200025208A1 (en) 2018-07-23 2018-07-23 Variable pitch fan assembly with blade pitch indication

Country Status (3)

Country Link
US (1) US20200025208A1 (en)
CN (1) CN110748501A (en)
BR (1) BR102019009976A2 (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1877115A (en) * 1929-09-26 1932-09-13 Zipay John Rapp Variable pitch propeller mechanism
US2225209A (en) * 1938-11-18 1940-12-17 Dewey David Brainard Motor cooling control
US2698772A (en) * 1950-04-27 1955-01-04 American Viscose Corp Twister mounting
US3758097A (en) * 1971-06-25 1973-09-11 P Newswanger Automatic vise jaw
US4356771A (en) * 1977-08-16 1982-11-02 Franz Plasser Bahnbaumaschinen-Industriegesellschaft M.B.H. Self-propelled track working machine
US5320186A (en) * 1991-06-03 1994-06-14 Ford New Holland, Inc. Draft control system with closed loop drop/raise rate control
US20160025102A1 (en) * 2013-03-13 2016-01-28 Cnh Industrial America Llc A variable pitch fan and a method for varying the blade pitch in a fan
US20190136867A1 (en) * 2017-10-09 2019-05-09 Mt-Propeller Entwicklung Gmbh Control Apparatus For A Hydraulic Variable-Pitch Propeller And Propeller Unit Comprising A Control Apparatus Of This Kind

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0517419B1 (en) * 1991-06-03 1995-09-13 New Holland U.K. Limited Draft control system with safety disconnect
DE10319550A1 (en) * 2002-05-01 2003-12-04 Murata Machinery Ltd Motor driven eccentric press
ITMI20080346A1 (en) * 2008-02-29 2009-09-01 Braking Sunstar S P A "BRAKING DEVICE"

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1877115A (en) * 1929-09-26 1932-09-13 Zipay John Rapp Variable pitch propeller mechanism
US2225209A (en) * 1938-11-18 1940-12-17 Dewey David Brainard Motor cooling control
US2698772A (en) * 1950-04-27 1955-01-04 American Viscose Corp Twister mounting
US3758097A (en) * 1971-06-25 1973-09-11 P Newswanger Automatic vise jaw
US4356771A (en) * 1977-08-16 1982-11-02 Franz Plasser Bahnbaumaschinen-Industriegesellschaft M.B.H. Self-propelled track working machine
US5320186A (en) * 1991-06-03 1994-06-14 Ford New Holland, Inc. Draft control system with closed loop drop/raise rate control
US20160025102A1 (en) * 2013-03-13 2016-01-28 Cnh Industrial America Llc A variable pitch fan and a method for varying the blade pitch in a fan
US20190136867A1 (en) * 2017-10-09 2019-05-09 Mt-Propeller Entwicklung Gmbh Control Apparatus For A Hydraulic Variable-Pitch Propeller And Propeller Unit Comprising A Control Apparatus Of This Kind

Also Published As

Publication number Publication date
BR102019009976A2 (en) 2020-02-04
CN110748501A (en) 2020-02-04

Similar Documents

Publication Publication Date Title
US7481620B2 (en) Wind power plant
WO2008075186B1 (en) Calibrated mechanical orthopedic driver with wear-compensated torque-limiting mechanism
US20120144939A1 (en) Double Bearing Assembly for Rotating Shaft
CN101208542B (en) Swash plate mechanism
US7757570B1 (en) Torque sensor with alignment system
US11407622B2 (en) Anti-rotation with cables
US20160160969A1 (en) Electrohydraulic actuator
US20100189386A1 (en) Angular-contact ball bearing in a tandem arrangement, and bearing arrangement having the angular-contact ball bearing
US8894497B2 (en) Sliding ball type constant velocity joint for vehicle
WO2002021004A3 (en) Bearing with adjustable setting
US5090295A (en) Radial piston engine
EP4039588A1 (en) Anti-torque rotor for a helicopter
US4579206A (en) Fluid coupling device and valve mechanism for use therein
US20200025208A1 (en) Variable pitch fan assembly with blade pitch indication
DE102005053408A1 (en) Actuating device for friction clutch, has mechanical transmission unit carrying sensor component and sliding in bifurcate guide which carries measuring sensor component, and protective cap covering latter component
EP1343688B1 (en) Offset crowned roller assembly for variable pitch propellers
US6997619B2 (en) Clutch release mechanism with a device for compensating for lack of precision in a friction clutch of a motor vehicle
US11002621B2 (en) Method and device for determining torque exerted on a shaft including transferring torque to a gearbox by the shaft and exerting axial force on the shaft dependent on the torque exerted by the shaft to the gearbox
US20160201697A1 (en) Variable wobbler for hydraulic unit
US6540055B2 (en) Driving arrangement with a free-wheel coupling
US7032470B2 (en) Yoke bearing providing improved support
EP3102824B1 (en) Low friction compact servo piston assembly
JP2005511986A (en) Screw actuator module
US2424530A (en) Throwout bearing
JP2003184873A (en) Bearing equipment for automatic transmission

Legal Events

Date Code Title Description
AS Assignment

Owner name: DEERE & COMPANY, ILLINOIS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:MILLER, SHAUN J.;REEL/FRAME:046435/0114

Effective date: 20180723

STPP Information on status: patent application and granting procedure in general

Free format text: NON FINAL ACTION MAILED

STPP Information on status: patent application and granting procedure in general

Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER

STPP Information on status: patent application and granting procedure in general

Free format text: FINAL REJECTION MAILED

STPP Information on status: patent application and granting procedure in general

Free format text: RESPONSE AFTER FINAL ACTION FORWARDED TO EXAMINER

STPP Information on status: patent application and granting procedure in general

Free format text: RESPONSE AFTER FINAL ACTION FORWARDED TO EXAMINER

STPP Information on status: patent application and granting procedure in general

Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER

STPP Information on status: patent application and granting procedure in general

Free format text: FINAL REJECTION MAILED

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION