US2665055A - Adjustable blade fan - Google Patents
Adjustable blade fan Download PDFInfo
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- US2665055A US2665055A US784043A US78404347A US2665055A US 2665055 A US2665055 A US 2665055A US 784043 A US784043 A US 784043A US 78404347 A US78404347 A US 78404347A US 2665055 A US2665055 A US 2665055A
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- rotor
- ring
- fan
- blades
- arms
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- 230000000694 effects Effects 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 241001289435 Astragalus brachycalyx Species 0.000 description 1
- 235000002917 Fraxinus ornus Nutrition 0.000 description 1
- 102000012152 Securin Human genes 0.000 description 1
- 108010061477 Securin Proteins 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000003867 tiredness Effects 0.000 description 1
- 208000016255 tiredness Diseases 0.000 description 1
Images
Classifications
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
- F04D29/36—Blade mountings adjustable
-
- 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
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
- F04D29/526—Details of the casing section radially opposing blade tips
Definitions
- My invention relates generally to fans for moving air or fiuids under pressure through ducts, and more particularly to simple mechanism for adjusting the pitch of the fan blades within predetermined limits to vary the volume and pressure of the fluid flow.
- Fans of the character herein involved are used as ventilating fans for mines, buildings, and ships, and it is often desirable to vary the volume and pressure of the fluid flow to meet altered conditions. It is also desirable that the pitch adjusting mechanism shall be such as to permit the simultaneous adjustment of the pitch angle of all of the blades of a fan, that it be possible to effect such adjustment by the change in position ofa single element, that it be possible to release for adjustment and tighten after adjustment the part which requires such adjustment, with a minimum of difficulty, and that nothing more than wrench and lever means shall be required for the making of the necessary adjustments and the'fixing-of the parts in the modified positions thereof.
- Fig. 1 is a longitudinal vertical section through a mine fan in which the invention is incorporated.
- Fig. 2 is an enlarged end elevational view of the fan rotor of Fig. 1, with casing parts omitted, the view being, subject to the understanding mentioned, taken approximately on the plane of the line 2-2 of Fig, 1.
- Fig. 3 is a section on the plane of the line 3-3 of Fig. 2, on an enlarged scale.
- Fig. 4 is an enlarged fragmentary view of a portion of the structure shown in Fig. 2, showingindexing and adjusting means.
- Fig. 5 is an enlarged section on the line 55 of Fig. 3, showing a detail of the adjusting mechanism.
- Fig. 6 is an enlarged fragmentary view showing releasable locking means.
- a mine fan generally designated 1.
- This mine fan structure includes a frusto-conical intake section 2 adapted to be connected by suitable conduit means 3 with a mine shaft or the like and with its other. end connected by a flared intake 4 with a propeller ring 5 to whose other side a vane ring assembly 8 is connected, this last including an outer fairing I and an inner fairing 8 connected together by vanes 9.
- an exhaust stack 16 of gradually increasing cross section.
- a streamlined nose portion 1 l providing a housingfor.
- a fan supporting and driving shaft 12 rotatably supported in-bearings 13 carried by a streamlined bearing pedestal [4 lies within the frusto-conical intake 2 and the forward portion of thefiared intake 4, which parts, together with the ring 5, make up a casing assembly generally designated I5.
- the shaft i2 is shown as carrying a large multiple V-belt. drive pulley I6 which is driven by V-belts l1 whose opposite runs pass through streamlined fairings, notshown because they are on the near side of the section on which Fig. 1 is taken.
- a streamlined tail section [8, whichlies rearwardly of the inner fairing 8 and is connected to the latter has an access door I9 which may be opened by releasing the holding bolts '20.”
- Within the propeller ring is a clearance ring 2
- a split cast rotor 22 carrying a series of fan blades 23.
- This rotor includes a hub portion 24 keyed as at 25 to a tapered portion 26 of the shaft 12 and held in position by a suitable washer 2'! and a nut 28 threadedly engaged with the end of the shaft 12.
- the rotor 3 includes cooperating annular plates 3
- and 32 cooperate to form bearings 40 in which shanks 4
- shown as cast integrally with the fan blades 23
- the blades may be rotated except as they are held, as hereinafter more fully described, on axes in the bearings 40.
- and 32 each have an arcuate series of openings ,41 through them, and the arms 44 project through the openings in one plate or. the other depending upon the manner of assembly, it being understood that if the arms are to be projected through the openings in the plate 32, this plate will be machined and tapped in the manner shortly to be described with respect to the plate 3
- they are shown as extending, through the openings 41 in the plate 3
- Each arm has a rounded head 48 for reception in and cooperation with the side walls 49 of notches 50 in a ring which will shortly be more fully described,
- is provided about its periphery, as wmbe noted; with a seriesof' notches 50 which are uniformly spaced, each of these notches having its side walls 49 mutually parallel and receiv- 11 's between saidsidewalls snugly one of the ballshaped extremities 48 of the arms 44', so that movements of the ring 5
- is mounted upon an annular flange 52 which is grooved as at*53"so as to provide a recess in which the inner edge of the ring may be rotatably received.
- the ring may be fixed in position relative to the flange 52 by means of bolts 54, washers '55; and lock washers 56, the bolts upon tightening thereof pressing the washers against the outer surface of the ring 5
- the fit of the ring is looseenough to permit it to have a rotary sli'ding motion in the'g'roove when the bolts 54 are slightlyuns'crewed
- has a 'hole or opening 58 formed through itand on the same are with this hole but in the rotor plate 3
- the mode of use of the blade adjusting mechanism will be readily understood.
- the bolts 54 are unscrewed in the plate 3
- a rod or other suitable lever device is then inserted through the hole 58 in the ring 5
- the rod as a lever, fulcruming in a hole 59 and engaging an abutment surface provided by the wall of the hole 58, and moving the outer end of said lever in a plane generally tangential to a cylinder struck from the axis of the rotor shaft and of a radius equal to the radial distance to the center or the holes 59, the ring 5
- the bolts 54 may be tightened and cause the washers to clamp the ring 5
- the wall of a hole 53 or of a bushing provides a fulcrum and the wall of the hole or opening 58 arl abutment; and that the lever engages oppositely racin surfaces inthese holes whicharespaced: axially of tha fan with respect to each other.
- Pitch adjusting mechanism for a propeller type fan having a rotor including a hub and a rim and a plurality of blades rotatably supported by said rotor for pitch angle adjustment and projecting radially from the rim thereof, said pitch adjusting mechanism including an adjusting member rotatably mounted on the rotor, means so operatively connecting the blades to said adjusting member that the adjustment of said member relative to said rotor varies the pitch of all of the blades, means for clamping said adjusting member to said rotor and supporting the same for rotation on an axis in the same line with the rotor axis, and means including a fulcrum on said rotor and an opening in said adjusting member for permitting a lever to have an end inserted through said opening into operative relation with said fulcrum and to be swun to elfect an adjustment of said adjusting member to change the pitch angle of the fan blades with respect to said hub, said fulcrum and said opening being disposed at like radial distance
- a rotor having radially extending bearings in its periphery for the reception of the pivot portions of fan blades, fan blades having pivot portions received in said bearings, arms secured to said pivot portions, a ring coaxial with said rotor and having pairs of mutually opposite walls each pair receiving closely between them one of said arms, means for securing said ring to said rotor to effect holding of said arms against swinging relative to said rotor, and means for adjusting said ring relative to said rotor including, on one of them, a fulcrum, and, in the other of them an opening through which a lever may have an end passed into engagement with said fulcrum, said opening and fulcrum disposed nearer the axis of the rotor than the pivot portions of said fan blades.
- a fan including a rotor and a vane ring having an inner fairing adjacent to said rotor and of a radius similar to the radius of the periphery of said rotor, said rotor having radially extending bearings in its periphery for the reception of the pivot portions of fan blades, fan blades having pivot portions received in said bearings, arms secured to said pivot portions, a ring coaxial with said rotor and having pairs of mutually opposite walls one pair cooperating with and closely receiving each of said arms, means for adjustably securing said ring to said rotor whereby the fixing of said ring relative to said rotor prevents swinging of said arms, and means inside said inner fairing for adjusting said ring relative to said rotor including, on one of them, a fulcrum for a ring adjusting lever and, on the other of them, and spaced axially of said fan from said fulcrum, abutment means also engageable by such a lever while the latter engages said fulc
- a rotor comprising a hub and end plates mounted on the hub to rotate therewith, said end plates having rim portions cooperating in providing bearings for the pivot elements of fan blades, fan blades having pivot elements rotatably mounted in said bearings, means for holding said pivot elements against longitudinal movement in said bearings, one of said end plates having openings therein, arms secured to said pivot elements and projecting through said openings, a ring coaxial with said last mentioned plate and rotatably supported by the latter and having portions providing oppositely facing surfaces closely receiving said arms between them, means for releasably clamping said ring in nonrotatable relation to said last mentioned end plate, and surfaces facing in opposite directions circumferentially of said rotor, and one on said last mentioned end plate and another on said ring and both located radially inwardly of the pivot elements of said fan blades, and spaced from each other axially of said fan, and concurrently engageable by a lever for effecting their relative rotation.
- a rotor comprisin a hub and end plates mounted on the hub to rotate therewith, said end plates having rim portions cooperating in providing bearings for the pivot elements of fan blades, fan blades having pivot elements rotatably mounted in said bearings, means for holding said pivot elements against longitudinal movement in said bearings, one of said end plates having openings therein, arms secured to said pivot elements and projecting through said openings, a ring coaxial with said last mentioned plate and rotatably supported by the latter and having notches closely receiving said arms, means for releasably clamping said ring in non-rotatable relation to said last mentioned end Plate, and means on said plate and ring, on each closer to its axis than the distance between said arms and the axis of said rotor, and spaced from each other axially of said rotor and engageable simultaneously by a lever for effecting their relative rotation about the rotor axis,
- said other end plate having openings therein opposite the first mentioned openings and said arms having means for releasably securing them to said pivot elements accessible through said last mentioned openings.
- a fan fan blades having pivot elements, a ot comp a b a d s a d e at mounted on the hub to rotate therewith, said end plates having rim portions, and said fan blades having pivot elements rotatably supported by said rim portions and held thereby against radial movement in either direction relativeto said rotor, one of said end plates having openings therein, arms secured to said pivot .elements andprojectmg through saidopenings, a ring coaxial with said last mentioned plate and rotatable on the axis of said rotor and having poi-'tions closely engaging the opposite sides of said arms and cooperating with said arms in sw inging of the latter and in holding them fixed, and means for fixing said ring in differentrelatively rotated positions with respect to Said rotor,
- said other plate having openings therein opposite the first mentioned openings and said arms having means for releasably clamping them to the pivot elements accessible through the openings in said other plate.
- Pitch adjusting mechanism for a propeller type fan having a rotor including a hub and a rim and a plurality of blades projecting radially from the thereof, including an annular adjusting member rotatably mounted on the rotor, means including arms fixed relative to saidblades andrecesses insaid member in which said arms are closely received for operatively connecting the blades to said adjusting member so that the rotation of said memberrelative to said rotor varies the pitch of all of the blades, means for clamping .saidadjusting member to said rotor in different relatively rotated positions, and means including fulcra on said rotor, and an opening in said adjusting member extending parallel to the axis of adjustment thereof and through whioh a lever can be inserted, a direction generally longitudinal of the axis of said rotor, into operative relation with said fulcra for eifecting ,an adjustment of said adjusting member, when the latter is released for rotation, to change the an l l fifi p
- a rotor having radially extending bearings in its periphery for th reception of the pivot portions of fan blades, fan blades having pivot portions received in said bearings and fixed against radial movement in'either direction relative to the latter,'arms secured to said pivot portions for selectively swinging the latter or holding them against turning on their aiies, a ring coaxial with said rotor'and having pairs of mutually opposite walls one pair cooperating with and closely receiving eacli'of said arms, means “for adjustably'securin'g' said ringto' said rotor, and means for adjusting said ring rela' tive to'said rotor including, on one of'them'; a fulcrum with'vv'hicli a lever is en'gageable "and can be caused to cooperate in effecting ring adjustment and, on the other of'them, abutment means engageable byflsuch' a lever, said fan including also a vane ring
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Description
Jan. 5, 1954 T. o. ADAMS, JR
ADJUSTABLE BLADE FAN 3 Sheets-Sheet 1 Filed Nov. 4, 1947 1320677107: .T/zomaa 0. tflciamcfr.
L; ,4- WM Jan. 5, 1954 T, DAMS, J 2,665,055
ADJUSTABLE BLADE FAN Filed Nov. 4, 1947 3 Sheets-Sheet 2 y J m; 4' WM Jan. 5, 1954 T. o. ADAMS, JR
ADJUSTABLE BLADE FAN 3 Sheets-Sheet 5 Filed'Nov. 4, 1947 Z52 vent 0r: f/zomayafldamsjcfr.
Patented Jan. 5, 1954 ADJUSTABLE BLADE FAN Thomas 0. Adams, Jr., New Philadelphia, Ohio,
assignor to Joy Manufacturing Company, a corporation of Pennsylvania Application November 4, 1947, Serial No. 784,043
9 Claims.
My invention relates generally to fans for moving air or fiuids under pressure through ducts, and more particularly to simple mechanism for adjusting the pitch of the fan blades within predetermined limits to vary the volume and pressure of the fluid flow.
, Fans of the character herein involved are used as ventilating fans for mines, buildings, and ships, and it is often desirable to vary the volume and pressure of the fluid flow to meet altered conditions. It is also desirable that the pitch adjusting mechanism shall be such as to permit the simultaneous adjustment of the pitch angle of all of the blades of a fan, that it be possible to effect such adjustment by the change in position ofa single element, that it be possible to release for adjustment and tighten after adjustment the part which requires such adjustment, with a minimum of difficulty, and that nothing more than wrench and lever means shall be required for the making of the necessary adjustments and the'fixing-of the parts in the modified positions thereof.
i It is an object of the present invention to provide improved and simple mechanism for adjusting the blade pitch of propeller'type fans and for maintaining the blades of such fans in the various positions to which they may be adjusted. It is another object of the present invention to provide improved adjusting and holding means forv the blades. of adjustable blade fans permitting the simultaneous and like adjustmentof all of the blades, the effecting of such adjustments, and the holding of the blades after such adjustments have been effected, with the use of but a single primary adjusting member, and the making'of such adjustments and the holding of the parts in adjusted positions by means of relatively light weight, so that excessive centrifugal forces will not be developed, and-with the formation of the adjusting-mechanism so that no unbalanced centrifugal force aficting the operation offthe fan rotorwill be produced. Other objects and advantages of the invention will hereinafter more fully'appear. V
f-gWhile the invention may be incorporated in other types of fans, I have shown the same embodi'ed'in a mine ventilating fan'in the accompanying drawings, in which for purposes'of illustration one form which the invention may assume in practice has been shown, and in these drawings Fig. 1 is a longitudinal vertical section through a mine fan in which the invention is incorporated.
. Fig. 2 is an enlarged end elevational view of the fan rotor of Fig. 1, with casing parts omitted, the view being, subject to the understanding mentioned, taken approximately on the plane of the line 2-2 of Fig, 1.
Fig. 3 is a section on the plane of the line 3-3 of Fig. 2, on an enlarged scale.
Fig. 4 is an enlarged fragmentary view of a portion of the structure shown in Fig. 2, showingindexing and adjusting means.
Fig. 5 is an enlarged section on the line 55 of Fig. 3, showing a detail of the adjusting mechanism.
Fig. 6 is an enlarged fragmentary view showing releasable locking means.
Referring to the drawings, and first to Fig. 1, it will be noted that there is shown in this figure a mine fan generally designated 1. This mine fan structure includes a frusto-conical intake section 2 adapted to be connected by suitable conduit means 3 with a mine shaft or the like and with its other. end connected by a flared intake 4 with a propeller ring 5 to whose other side a vane ring assembly 8 is connected, this last including an outer fairing I and an inner fairing 8 connected together by vanes 9. To the rear of the vane ring assembly there is arranged an exhaust stack 16 of gradually increasing cross section.
A streamlined nose portion 1 l providing a housingfor. a fan supporting and driving shaft 12 rotatably supported in-bearings 13 carried by a streamlined bearing pedestal [4 lies within the frusto-conical intake 2 and the forward portion of thefiared intake 4, which parts, together with the ring 5, make up a casing assembly generally designated I5. The shaft i2 is shown as carrying a large multiple V-belt. drive pulley I6 which is driven by V-belts l1 whose opposite runs pass through streamlined fairings, notshown because they are on the near side of the section on which Fig. 1 is taken. A streamlined tail section [8, whichlies rearwardly of the inner fairing 8 and is connected to the latter has an access door I9 which may be opened by releasing the holding bolts '20." Within the propeller ring is a clearance ring 2|, in close proximity to which the tips of the fan blades, later mentioned, move.
' Upon the shaft l2 there is supported for rotation with such shaft a split cast rotor 22 carrying a series of fan blades 23. This rotor includes a hub portion 24 keyed as at 25 to a tapered portion 26 of the shaft 12 and held in position by a suitable washer 2'! and a nut 28 threadedly engaged with the end of the shaft 12. The rotor 3 includes cooperating annular plates 3| and 32 having portions 33 engaging the opposite end surfaces of an enlarged flange 34 of the hub 24, the plate portions 33 being secured to the hub by bolts 35 threadedly engaging a ring 36, said bolts extending through both plates and through the collar portion 34 of the hub 24. The plates 3| and 32 cooperate to form bearings 40 in which shanks 4|, shown as cast integrally with the fan blades 23, are rotatably received. When there are no centrifugal forces acting on the fan blades, the blades may be rotated except as they are held, as hereinafter more fully described, on axes in the bearings 40. At theinner end of each shank 4| there is an enlarged collar portion Ma from which there extends radially inwardly a boss or pilot 42, and upon each of these bosses there is mounted a clamp 43 which has integral with it an arm 44, and these arms may be secured at any desired angle with respect to the fan blades 23 with which they are associated by means of bolts 46. The plates 3| and 32 each have an arcuate series of openings ,41 through them, and the arms 44 project through the openings in one plate or. the other depending upon the manner of assembly, it being understood that if the arms are to be projected through the openings in the plate 32, this plate will be machined and tapped in the manner shortly to be described with respect to the plate 3|.. Herein they are shown as extending, through the openings 41 in the plate 3|, the plate which is nearer to the streamlined tail of the fan casing. Each arm has a rounded head 48 for reception in and cooperation with the side walls 49 of notches 50 in a ring which will shortly be more fully described,
The ring 5| is provided about its periphery, as wmbe noted; with a seriesof' notches 50 which are uniformly spaced, each of these notches having its side walls 49 mutually parallel and receiv- 11 's between saidsidewalls snugly one of the ballshaped extremities 48 of the arms 44', so that movements of the ring 5| may effect adjustment of the fan blades. The ring 5| is mounted upon an annular flange 52 which is grooved as at*53"so as to provide a recess in which the inner edge of the ring may be rotatably received. The ring may be fixed in position relative to the flange 52 by means of bolts 54, washers '55; and lock washers 56, the bolts upon tightening thereof pressing the washers against the outer surface of the ring 5| and thus clamping the edge of this ring between the wall of the. groove 53 and the washers, The fit of the ring is looseenough to permit it to have a rotary sli'ding motion in the'g'roove when the bolts 54 are slightlyuns'crewed The ring 5| has a 'hole or opening 58 formed through itand on the same are with this hole but in the rotor plate 3| there are a number of smaller holes or openings '53,. these latter holes being provided with steel bushings 60 as liners. Radially inwardly of the hole '53 there are; marks SI representing different angle adjustments of the blades. These come directly above an index line 52 on the flange 52. This combination of lines; may be used for locating the steel ring 5| in any one. of a number of selected positions- The 'fan blades will be in their median position of angular adjustment when the central line markedM is opposite the line 62 on the flange, in their fposi tion of maximum air displacement when the line marked H is opposite the line 52 on the flange, and in their position of minimum air displace- 4 ment when the line L comes opposite the mark on the flange 52.
The mode of use of the blade adjusting mechanism will be readily understood. The bolts 54 are unscrewed in the plate 3|, thereby permitting the ring 5| to be rotated. A rod or other suitable lever deviceis then inserted through the hole 58 in the ring 5| and has its end extended into one of the holes 59 in the rotor plate 3|. By using the rod as a lever, fulcruming in a hole 59 and engaging an abutment surface provided by the wall of the hole 58, and moving the outer end of said lever in a plane generally tangential to a cylinder struck from the axis of the rotor shaft and of a radius equal to the radial distance to the center or the holes 59, the ring 5| may be actuated circumferentially and cause the various arms 44 to turn the shanks of the several fan blades angularly in proportion to the arcuate adjustment of the ring 5|. When the desired angle is attained, the bolts 54 may be tightened and cause the washers to clamp the ring 5|- firmly with respect to the rotor, and thus the angle of the blades may be maintained until it isagain desired to adjust it. In effecting adjust-- ment it will be noted that the wall of a hole 53 (or of a bushing provides a fulcrum and the wall of the hole or opening 58 arl abutment; and that the lever engages oppositely racin surfaces inthese holes whicharespaced: axially of tha fan with respect to each other. The surfaces eh g-aged by the lever during adjustingface oppositely circumferentially of the rotor; 7
Should a new range, either higher or lower than the initial setting be desired, it may be ob'-- tained by locating the ring 5| in one of its ex"- treme positions. The several bolts 46 would then be loosened by inserting an Allen wrench through the openings 41' in the plate 32-. The blades could then be rotated to any desired angle and the clamps again tightened. By following this procedure with each of the blades of the rotor, a new range of adjustment can be secured.
From the foregoing description, it will be apparent that I have provided a very simple and effective arrangement for lvarying the, angular adjustment of all: of the blades of a fan manna holding the blades in a desired common angular relation to thefhub of the fan. Adjusting aim: gle element will change the adjustment, of all "(if theblades and this element may be fixed, re.- leased a d; re-nxeasmw by tightening-a relatively' small number of holding elements; which clamp it againsta surface relative to which it "is moved during adjustment. Not only changes within the norm l limits may be provided; but: also entirelynew sets of limits maybe established mew s an' im l m nn r r p ef t the a ust e h P s ta erfprrn tl 're job walk through the exhaust stack on the fan until he has reached the tail access door |'9, and upon removal of the bolts 2U'this door drops down about hinges not shown and access "to the inner fairing 8 becomes pastime Having entered this fairing, pre x/tiredness remove. a single boltB and allow the upper half Cof a split bulkhead to swing down about ahinz'e D, and this brings, into easy access the bolts 54.. The effecting of the adjustment a'nd'the'c'dms plete reolosing of the fan ready for operationtakes not over five minutes in actual practice. One of the greatest advantages or the i-nvehtion inheres inthe operators ability 'to adjust the pitch of all of the blades simultaneously, arid-fir the extreme simplicity and cheapness of the structure for thisp'urpose While I have in this application specifically described one form which my invention may assume in practice, it will be understood that this form of the same is shown for purposes of illustration and that the invention may be modified and embodied in various other forms without departing from its spirit or the scope of the appended claims.
What I claim as new and desire to secure by Letters Patent is:
1. Pitch adjusting mechanism for a propeller type fan having a rotor including a hub and a rim and a plurality of blades rotatably supported by said rotor for pitch angle adjustment and projecting radially from the rim thereof, said pitch adjusting mechanism including an adjusting member rotatably mounted on the rotor, means so operatively connecting the blades to said adjusting member that the adjustment of said member relative to said rotor varies the pitch of all of the blades, means for clamping said adjusting member to said rotor and supporting the same for rotation on an axis in the same line with the rotor axis, and means including a fulcrum on said rotor and an opening in said adjusting member for permitting a lever to have an end inserted through said opening into operative relation with said fulcrum and to be swun to elfect an adjustment of said adjusting member to change the pitch angle of the fan blades with respect to said hub, said fulcrum and said opening being disposed at like radial distances from the rotor axis and closer to the latter than is said rim.
2. In a fan, a rotor having radially extending bearings in its periphery for the reception of the pivot portions of fan blades, fan blades having pivot portions received in said bearings, arms secured to said pivot portions, a ring coaxial with said rotor and having pairs of mutually opposite walls each pair receiving closely between them one of said arms, means for securing said ring to said rotor to effect holding of said arms against swinging relative to said rotor, and means for adjusting said ring relative to said rotor including, on one of them, a fulcrum, and, in the other of them an opening through which a lever may have an end passed into engagement with said fulcrum, said opening and fulcrum disposed nearer the axis of the rotor than the pivot portions of said fan blades.
3. In a fan, including a rotor and a vane ring having an inner fairing adjacent to said rotor and of a radius similar to the radius of the periphery of said rotor, said rotor having radially extending bearings in its periphery for the reception of the pivot portions of fan blades, fan blades having pivot portions received in said bearings, arms secured to said pivot portions, a ring coaxial with said rotor and having pairs of mutually opposite walls one pair cooperating with and closely receiving each of said arms, means for adjustably securing said ring to said rotor whereby the fixing of said ring relative to said rotor prevents swinging of said arms, and means inside said inner fairing for adjusting said ring relative to said rotor including, on one of them, a fulcrum for a ring adjusting lever and, on the other of them, and spaced axially of said fan from said fulcrum, abutment means also engageable by such a lever while the latter engages said fulcrum,
4. In a fan, a rotor comprising a hub and end plates mounted on the hub to rotate therewith, said end plates having rim portions cooperating in providing bearings for the pivot elements of fan blades, fan blades having pivot elements rotatably mounted in said bearings, means for holding said pivot elements against longitudinal movement in said bearings, one of said end plates having openings therein, arms secured to said pivot elements and projecting through said openings, a ring coaxial with said last mentioned plate and rotatably supported by the latter and having portions providing oppositely facing surfaces closely receiving said arms between them, means for releasably clamping said ring in nonrotatable relation to said last mentioned end plate, and surfaces facing in opposite directions circumferentially of said rotor, and one on said last mentioned end plate and another on said ring and both located radially inwardly of the pivot elements of said fan blades, and spaced from each other axially of said fan, and concurrently engageable by a lever for effecting their relative rotation.
5. In a fan, a rotor comprisin a hub and end plates mounted on the hub to rotate therewith, said end plates having rim portions cooperating in providing bearings for the pivot elements of fan blades, fan blades having pivot elements rotatably mounted in said bearings, means for holding said pivot elements against longitudinal movement in said bearings, one of said end plates having openings therein, arms secured to said pivot elements and projecting through said openings, a ring coaxial with said last mentioned plate and rotatably supported by the latter and having notches closely receiving said arms, means for releasably clamping said ring in non-rotatable relation to said last mentioned end Plate, and means on said plate and ring, on each closer to its axis than the distance between said arms and the axis of said rotor, and spaced from each other axially of said rotor and engageable simultaneously by a lever for effecting their relative rotation about the rotor axis,
said other end plate having openings therein opposite the first mentioned openings and said arms having means for releasably securing them to said pivot elements accessible through said last mentioned openings.
6. In a fan, including a rotor and a vane ring having an inner fairing adjacent to said rotor and of a radius similar to the radius of the pe= riphery of said rotor, said vane ring having an open end through which access to its interior may be had and said rotor comprising a hub and end plates mounted on the hub to rotate therewith, fan blades having pivot elements rotatably supported adjacent the outer periph= cries of said plates for turning on their own axes, means for holding said pivot elements against radial movement with respect to said rotor, one of said end plates having openings therethrough, arms secured to said pivot elements and projecting through said openings, a ring member coaxial with said last mentioned plate and rotatably supported by said rotor and having wall portions closely receiving said arms, means for .releasably clamping said member in nonrotatable relation to said rotor, and ring member adjusting means accessible from within said inner fairing and including in spaced relation to each other axially of said fan a fulcrum on said last mentioned plate and an abutment on said ring member simultaneously engageable by a lever to effect their relative rotation.
7. In a fan, fan blades having pivot elements, a ot comp a b a d s a d e at mounted on the hub to rotate therewith, said end plates having rim portions, and said fan blades having pivot elements rotatably supported by said rim portions and held thereby against radial movement in either direction relativeto said rotor, one of said end plates having openings therein, arms secured to said pivot .elements andprojectmg through saidopenings, a ring coaxial with said last mentioned plate and rotatable on the axis of said rotor and having poi-'tions closely engaging the opposite sides of said arms and cooperating with said arms in sw inging of the latter and in holding them fixed, and means for fixing said ring in differentrelatively rotated positions with respect to Said rotor,
said other plate having openings therein opposite the first mentioned openings and said arms having means for releasably clamping them to the pivot elements accessible through the openings in said other plate.
8. Pitch adjusting mechanism for a propeller type fan having a rotor including a hub and a rim and a plurality of blades projecting radially from the thereof, including an annular adjusting member rotatably mounted on the rotor, means including arms fixed relative to saidblades andrecesses insaid member in which said arms are closely received for operatively connecting the blades to said adjusting member so that the rotation of said memberrelative to said rotor varies the pitch of all of the blades, means for clamping .saidadjusting member to said rotor in different relatively rotated positions, and means including fulcra on said rotor, and an opening in said adjusting member extending parallel to the axis of adjustment thereof and through whioh a lever can be inserted, a direction generally longitudinal of the axis of said rotor, into operative relation with said fulcra for eifecting ,an adjustment of said adjusting member, when the latter is released for rotation, to change the an l l fifi p of h b fi 3 11 999 to the hub.
9. In a fan, a rotor having radially extending bearings in its periphery for th reception of the pivot portions of fan blades, fan blades having pivot portions received in said bearings and fixed against radial movement in'either direction relative to the latter,'arms secured to said pivot portions for selectively swinging the latter or holding them against turning on their aiies, a ring coaxial with said rotor'and having pairs of mutually opposite walls one pair cooperating with and closely receiving eacli'of said arms, means "for adjustably'securin'g' said ringto' said rotor, and means for adjusting said ring rela' tive to'said rotor including, on one of'them'; a fulcrum with'vv'hicli a lever is en'gageable "and can be caused to cooperate in effecting ring adjustment and, on the other of'them, abutment means engageable byflsuch' a lever, said fan including also a vane ring providing a fairing close to the periphery of said rotor and having in communication with its interior an accessdoor and so disposed that said'means for adjusting said ring relative to said rotor is accessible from within it. I THOMAS O. ADAMS, JR.
References Cited in the file of this patent UNITED STATES Number Name Date 1,225,053 Pitts May .8, 1917 1,456,699 Kramer May 29, 1923 1,935,314 Finch etal Nov. 14, 19.33 2,232,670 Barrett Feb. 18,1941 2,341,974 Browne Feb. 14, 1944 2,3 ,3 3 binger Jun 6, 194, 2,382,535 Bauer Aug. 14, 1945 2,495,434 Troller Jan. 24, 1950 2,607,430 Dean Aug. 19, 1 952 FOREIGN PATENTS ,Number Country Date 337,552 Italy L- Mar. 7,' 1936 567,978 Great-Britain; Mar. '12, 1945 697,416 Germany Oct. '14, 1940
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US784043A US2665055A (en) | 1947-11-04 | 1947-11-04 | Adjustable blade fan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US784043A US2665055A (en) | 1947-11-04 | 1947-11-04 | Adjustable blade fan |
Publications (1)
Publication Number | Publication Date |
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US2665055A true US2665055A (en) | 1954-01-05 |
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Family Applications (1)
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US784043A Expired - Lifetime US2665055A (en) | 1947-11-04 | 1947-11-04 | Adjustable blade fan |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1038231B (en) * | 1955-06-22 | 1958-09-04 | Nuesse & Graefer K G Maschf | Fan with adjustable blades |
US2869535A (en) * | 1954-05-12 | 1959-01-20 | Fairchild Engine & Airplane | Aircraft heating system |
US3687569A (en) * | 1971-03-19 | 1972-08-29 | Gen Electric | Rotor with variable angle blades |
US4171183A (en) * | 1976-09-24 | 1979-10-16 | United Technologies Corporation | Multi-bladed, high speed prop-fan |
FR2446935A1 (en) * | 1979-01-19 | 1980-08-14 | Szelloezoe Muevek | Fan blade pitch adjusting mechanism - consists of movable ring inside shroud, connected by adjustable rods to blade spindles |
CN105626308A (en) * | 2014-11-21 | 2016-06-01 | 通用电气公司 | Variable pitch fan for gas turbine engine and method of assembling the same |
US9869190B2 (en) | 2014-05-30 | 2018-01-16 | General Electric Company | Variable-pitch rotor with remote counterweights |
US10100653B2 (en) | 2015-10-08 | 2018-10-16 | General Electric Company | Variable pitch fan blade retention system |
US11674435B2 (en) | 2021-06-29 | 2023-06-13 | General Electric Company | Levered counterweight feathering system |
US11795964B2 (en) | 2021-07-16 | 2023-10-24 | General Electric Company | Levered counterweight feathering system |
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US2869535A (en) * | 1954-05-12 | 1959-01-20 | Fairchild Engine & Airplane | Aircraft heating system |
DE1038231B (en) * | 1955-06-22 | 1958-09-04 | Nuesse & Graefer K G Maschf | Fan with adjustable blades |
US3687569A (en) * | 1971-03-19 | 1972-08-29 | Gen Electric | Rotor with variable angle blades |
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US9869190B2 (en) | 2014-05-30 | 2018-01-16 | General Electric Company | Variable-pitch rotor with remote counterweights |
CN105626308A (en) * | 2014-11-21 | 2016-06-01 | 通用电气公司 | Variable pitch fan for gas turbine engine and method of assembling the same |
US10072510B2 (en) * | 2014-11-21 | 2018-09-11 | General Electric Company | Variable pitch fan for gas turbine engine and method of assembling the same |
CN105626308B (en) * | 2014-11-21 | 2020-07-31 | 通用电气公司 | Variable pitch fan for gas turbine engine and method of assembling same |
US10100653B2 (en) | 2015-10-08 | 2018-10-16 | General Electric Company | Variable pitch fan blade retention system |
US11674435B2 (en) | 2021-06-29 | 2023-06-13 | General Electric Company | Levered counterweight feathering system |
US12180886B2 (en) | 2021-06-29 | 2024-12-31 | General Electric Company | Levered counterweight feathering system |
US11795964B2 (en) | 2021-07-16 | 2023-10-24 | General Electric Company | Levered counterweight feathering system |
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