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Publication numberUS1673564 A
Publication typeGrant
Publication dateJun 12, 1928
Filing dateApr 20, 1926
Priority dateApr 20, 1926
Publication numberUS 1673564 A, US 1673564A, US-A-1673564, US1673564 A, US1673564A
InventorsCharles E Hathorn, Sylvanus A Reed
Original AssigneeCurtiss Aeroplane & Motor Co
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Propeller-twisting press
US 1673564 A
Abstract  available in
Images(3)
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Claims  available in
Description  (OCR text may contain errors)

June 12, 1928. 1,673,564

C. E. HAZTHORN ET AL PROPELLER TWI S TING PRES S Filed r 20 5 Sheets-Sheet 1 lNws-N'roRs CHARLEfi E. HATHORN w YLVAHUS A. REED.

PROPELLER TWI S TI NG PRES 5 Filed April 20, 1926 3 Sheets-Sheet 5 INVENTORJ. CHARLE5E HATHORN By finvAmusARzzo.

AT NEY Patented June 12, 1928.

UNITED STATES 1,673,564 PATENT OFFICE.

CHARLES E. HATI-IORN, OF HEMPSTEAD, AND SYLVANUS A. REED, OF NEW YORK,

N. Y., ASSIGNORS TO CURTISS AEROPLANE & MOTOR COMPANY, INC., A CORPORA- 'I'ION OF NEVT YORK.

PROPELLER-TWISTING PRESS.

Application filed April 20, 1926.

Our invention relates to propellers and more particularly to the m ihod of and apparatus for twisting metal propellers of aircraft.

In the manufacture of metal propellers for aircraft the propeller blank is first milled to change its cross-section from rectangular to approximately aerofoil form. This having been accomplished the propeller blank is ready to be twisted. Heretofore in twisting the propeller blank a rotary twisting machine has been used. Such a machine, while especially designed for twisting and bending the propeller blank, is nevertheless objectionable in that, due to the peculiarity of the twist, a multiple number of separate and wholly independent machine operations are required to be performed. One blade of the propeller blank is first clamped between the jaws of the twisting machine about 12 incl cs out from the transverse center line of the blank and given an initial twist of approximately 40 degrees. The propeller blank is then unclaniped, withdrawn from the machine, and reset exactly as before except that the opposite or untwisted propeller blade is clamped in place. Thus set, with said jaws engaging said opposite blade at a corresponding point out from said center line, said opposite blade is given an initial or center twist exactly the same as its companion. This initial twist of each blade is in each instance constant, that is to say, if a twist of 40 degrees is given each blade at its 12-inch station out from said center line, each said blade throughout the remaining portion of its length will bear to the untwisted center portion of the blank a i0 degree angle. Unfortunately, however, if properly shaped or twisted, the blade angles of an aeronautical propeller vary. Generally speaking such variation ranges anywhere from approximately 40 degrees at the blade root to approximately 15 degrees at the tip. To obtain this gradually diminishing blade angle a second series of machine operations is required. These operations, of which there are many, the number depending upon the particular propeller design, are usually performed with the same machine as are the initial or center twist operations and are generally designated the reverse or countertwist operations. Each blade, as it is reversely or counter-twisted, is acted upon re- Serial No. 103,316.

peatedly and separately altho in each instance the repeated operations are the same. At intervals from the innermost station outwardly each blade is marked off at predetermined intermediate stations. These stations indicate the exact spot or point at which the blade should be held between the jaws of the machine during each successive reverse or counter-twist, and, as such stations are usually anywhere from six inches to twelve inches apart, and asthe propeller blank must be clamped at every or at least every other station, and a certain degree of reverse twist imparted to each blade after each successive clamping, obviously the operations incident to properly reversely twisting or countertwisting the propeller blank are numerous. Again unfortunately, the blade angles obtained by thus reversely twisting the propeller blank are only approximately correct and must afterwards be checked and corrected by other means necessitating additional work and the further handling of the propeller blank. Moreover, after twisting the blank and correcting the blade angles, it is further important that the axis of each blade be canted or bent forward slightly to relieve, during actual use of the propeller, certain bending stresses known at this time to exist. This latter bending operation is usually performed by hand.

An object of the present invention is to eliminate the many successive and tedious operations above outlined by providing, instead of rotary twisting machines, a propeller twisting press. Preferably such press comprises co-acting dies, adjustable for different designs of propellers, between which the propeller blank is laid; means for holding the propeller blank in place between said dies; and additional means for bringing said dies together. In bringing said dies together (thru hydraulic or other power means), the propeller blank, in one and the same operation, is initially twisted, reversely or counter-twisted, and bent longitudinally as aforesaid; the initial twist, the countertwist, and the longitudinal bend, in each instance, being so exact and so perfect as to wholly eliminate the heretofore subsequent check and correction accorded the angle of the propeller blades. By thus performing, in a single operation, the functions heretofore performed by numerous operations, the

manufacturing cost of metal aeronautical propellers is very appreciably reduced.

A further object of the invention is to so form the co-acting dies of the propeller press as to subjectthe blank to the action of the dies at inter 'als or stations so relatively spaced as to produce in the blank a substantially uniformly varying angle as d1st1n guished from the more or less successive pronounced angular variations produced heretofore.

A still further object of the invention 13 the provision of a novel term of holding means whereby the propeller blank is firmly held between the dies and against movement in any direction other than rotary or vertical. such rotary movement. at the ends of the blank, being essential to the completion of the initial as well as the counter-twist operations.

Other objects, advantages and characteri tics of the invention will be hereinafter pointed out.

In the drawings, wherein like reference characters denote like or corresponding parts,

Fig. 1 is a side elevation of the press;

Fig. 2 is a horizontal section on the line 22 of Fig. 1;

Fig. 3 is a side elevation of a portion of each die and its associated plate showing the relation of the propeller blank thereto as the dies approach one another in a twi t ing operation;

Fig. 4 is a plan view of the lower die showing the propeller blank ready to receive its various twists;

Fig. 5 is an end view of the die portion of the press showing the manner in which the blank ends are clamped or held in place;

Fig. 6 is a similar view showing the relation of the press parts upon the completion of the 'arious blank twists;

Fig. 7 is a section on the line 77 of Fig. 3;

Fig. 8 is a view similar to Fig. 7 with the dies brought together to complete the propeller twist;

Fig. 9 is a perspective view of one of the die pieces and die blocks;

Fig. 10 is a perspective view of a properly twisted propeller blank. the broken line indicating the configuration of the blank prior to receiving the twist, and

Fig. 11 is a view similar to Fig. 8 illustrating a modification.

In the embodiment of the invention selected for illustration. a hydraulic press of more or less conventional form is shown. Preferably such press comprises a ba e plate 20. a top plate 21, a ram (not shown) and such other ordinary hydraulic press parts as operating mechanism 22 and supporting frame. the latter consisting of uprights a cross-head 2t and a base portion 25 within which the ram is enclosed. This particular form of hydraulic press, however, is merely illustrative, and a ditl'erent l'orm ot press, other than hydraulic, it desired, may be used.

To each of the plates 20 and 21 of the press a die-carrier is l'astcncd. The diecarricr ill of the plate it! i mounted thereon and in cross-:rction is ol approximately channel l'orm. lt is laterally braced as at QT to said brace plate and at its opposite ends is provided with vertically extending guide arms The other of the die-carriers, designated as it). tastcned to and against; the underl'aee ot' the top plate 21. and like the die-carrier :30. it too i laterally braced. The bracing $30 for the die-carrier 29, however. is carried. not to its supporting plate, but directly to the cross-head 241 of the frame. This ditlcrence in the bracing arrangement for the two plates 20 and 21 is made possible by the fact that the plate 21 is fixed in its relation to the supporting jl'rame whereas the plate 20 vertically movable. Otherwise the die-carriers 26 and 25) are the same. The guide arm 2s. ot which there are four, two at each end of the die carrier :26. hear at all times directly against the vertical side walls of the fixed die-carrier Q9.

Within the l'acin channels of the two diccarriers 26 and 2!) the. co-acting press dies are fastened. 3oth said dies, the lower designated in its entirety as 31, and the upper similarly designated as 32. are substantially identical in size, form and construction. Each die comprises a plurality of die-holding blocks 33 and a similar number of diepicccs or sections 3-}. These die-pieces 31 are preterably of semi-disc form and except; tor a slight ditl'erence in the configuration of the active ub'-'tantially straight edge 35 of each. 111" also identical. The die-holding blocks 23 extend transversely of the diecarriers and are removably fastened within the channels thereof by bolts 36. The top face of each die-block 33 is hollowed out as at $37 to receive in the recess thus formed, one of said die-pieces 3-}. aid die-pieces fit snugly within said recesses and bear firmly throughout' their respective rounded edges directly against the similarly rounded bottom recess walls. Such bearing contact. plus the block side wall engagement, otlcrs suflicicnt; contact area between the die-pieces and the die-blocks to hold the former against. both lateral and vertical relative movement under all circumstances. Bolts 38 penetrating the die-block ends and fitting bolt holes 39 formed in the die-pieces. firmly hold said die-pieces against rotational movement when properly set. lly graduating the rounded edge of each die-piece in degrees as indicated atv 40, each said die-piece may be accurately separately adjusted as desired.

As previously explained, an aeronautical ltltl propeller, if properly shaped, is required to be twisted in a manner such that the blades thereof present to the right angle plane of its longitudinal axis a degree angle or thereabouts at the innermost blade stations which are usually twelve inches out from the transverse center line of the propeller blank; such blade angle gradually lessening from said twelve inch station outwardly to approximately a fifteen degree angle at the blade tip. To obtain this peculiar gradually diminishing blade angle from said twelve inch station outwardly, the active edges of the several die-pieces 84: at opposite sides of the transverse center line of each die present, when viewed from the die ends, (see Fig. 7) slightly different angles at each blade station, the angles increasing inwardly toward the die centers in a like manner and to the same extent from the oppositeouter ends of said dies. As the diminishing blade angle is preferably more pronounced in the vicinity of the points at which a maximum twist is desired, the diepieces, at the inner blade stations are placed closer together than they are at the outer blade ends.

In Fig. 10 of the drawings the propeller blank is illustrated in broken lines as it appears before being pressed or twisted and in full lines it is illustrated as it appears properly shaped. Such blank is designated as 41 and the center opening formed therein is designated as 42. This center opening a2 is formed in the blank at the inter-section of the longitudinal and transverse center lines thereof before said blank is twisted and shaped. lVith said opening 42 properly located the propeller blank is laid between the dies 31 and of the press. To center the blank relatively to said dies a spindle 43 is provided. Said spindle projects vertically upwardly from the exact center of the lower die 31 and is adapted to snugly engage in said center opening 4-2 of the propeller blank. By providing a comparatively snug fit between said spindle and said center opening the propeller blank is firmly held against rotational and lateral movement in the vicinity of its transverse center line, against longitudinal displacement under all circumstances, and in a manner such that, during the twisting operation, other than a corresponding twist at opposite sides of said center line cannot possibly occur.

As a further means for holding the propeller blank during a twisting operation, end clamps or devices are provided. These end clamps are mounted between vertical guide rails 44 (two for each clamp) fastened to the die-carrier 26 at its opposite ends. Each clamp comprises a fixed jaw a5. a movable jaw 46, clamp ends or head portions 4:7, and clamping bolts 48. The head portions 47 (see Figs. 5 and 6) of each clamp are preferably formed integrally with the fixed jaw 45 thereof and are adapted to bear on and fit between the guide rails at as indicated. Said head portions t? are also provided with arcuate end grooves 49 within which said guide rails al engage. In this manner said end clamps are held against transverse or endwise movement the movable freely both vertically and rotationally. A mark 50 on each clamp indicates the exact longitudinal center line of the co-acting dies of the press.

In operation, a propeller blank is laid longitudinally of and between the (Jo-acting dies 31 and 32 of the press with the spindle 43 extending vertically thru the center hole 42 of the propeller blank. The ends of the propeller are then clamped between the aws 4.5 and 46 of the end clamps with the markings 50 on said clamps in registry with the longitudinal center line of the propeller blank. Thus positioned and securely clamped between the press dies the blank 41 is ready to be twisted or shaped. As the dies 31 and 32 are brought together the innermost die pieces 3st at opposite sides of the transverse center line of the blank first bear thereon to positively twist it as said dies appreach each other. This first twist, due to the high angle of the die pieces at said inner most blade stations, constitutes what has heretofore been designated the initial or center twist and it, the initial or center twist, continues uninterruptedly until the desired blade angle at said innermost blade stations is obtained. The reverse or counter-twist operation, as intimated, is obtained while and during the initial twist operation. the commencing only after such initial twist operation is under way. The counter-twist operation, however, is completed at the same moment as said initial twist operation and due to the varying angles of the outer die pieces is *ariable throughout the respective blade lengths. To longitudinally bend or cant the propeller blank shim 51 of different thickness may be inserted beneath the outer die blocks as illustrated. No re-check or correction is required it and when the die-pieces are properly set. All bonds or twists are obtained by the one operation, i. e., the bringing of the dies 31 and 32 together.

In the modification of Fig. 11, instead of providing adjustable die-pieces, die pieces 52 of a given configuration are provided. Such die-pieces are fastened between the die-car rier of the press by bolts 53 and are preferably interchangcaible. For shaping or twisting propeller blanks of different design, where non-atljustable die-pieces ar used, a different set of such die-pieces must be provided for each design that is different.

lVhile we have described our invention in detail in its present preferred embodiment, it will be obvious to those skilled in the art after understanding our invention, that various changes and modifications may be made. therein without departing from the spirit. or scope thereof. '0 aim in the appended claims to cover all such modifications and changes.

\Vhatwe claim is:

1. A press for twisting propellers including dies between which the propeller is laid. rotatable clamps for holding said propeller in place between said dies, and means for bringing said dies together.

2. A press for twisting propellers including dies between which the propeller is laid, guidestmounted at the die ends. clamps carried by and rotatable within said guides for holding the propeller in place between said dies, and means for bringing said dies together.

A press {or twisting propellers including dies between which the propeller is laid, freely rotatable clamps mounted at the die ends to hold said propeller in place between said dies, means for holding each said clamp against morementtransversely of said dies, and means for bringing said dies together.

4. A press for twisting propellers including dies between which the propeller is laid, each die comprising a plurality of separately adjustable die-pieces, means for holding each die-piece in its adjusted position, a center spindle for holding the propeller in place between said dies, relatively movable end clamps likewise engageable with said propeller to hold it. in place between said dies, and means for bringing said dies together with the propeller held therebetween.

The method of twisting metal aeronautical propellers which consists in progressively bringing to bear on the opposite faces of the propeller blank at dilterent star tions throughout its length a plurality of individually termed die-pieces each haying an engaging surface set at an angle cal culated to produce in a. finished product that particular twist deemed correct for that particular station at which said die-piece bears.

(1. A press for twisting propellers comprising dies between which the propeller is laid, each die including a. plurality of transversely extending die pieces adapted to he indiridually adjusted to present toward the propellcr a working face. the angularit of which may be varied by such adjustment, means for holding said propeller in place between said dies and means for bringing said dies together.

7. A. press for twisting propellers comprising dies between which the propeller is laid, each die including a plurality of transversely extending die pieces individualtv rotatable about an axis extending longitudinally of said die to \"ary the angle of the working 'l'ace thereof. means for holding said propeller in place between said dies and means for bringing said dies together.

8. A press for twisting propellers comprising dies between which the propeller is laid. each die including a plurality of freely removable transversely extending die pieces adapted to separately engage, each within a recess -formed within said (lie, means for holding said propeller in place between said dies and means for bringing said dies together.

9. A press for twisting propellers comprising dies between which the propeller is. laid. clamps for said propeller rotatable during th twisting thereof. and means for bringing said dies together with the propeller held in place by said clamps.

Tn testimony whereof we hereunto aflix our signatures.

CHARLES E. I*I. \'II-TORN. SYLVANUS A. REED.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2433226 *Jun 5, 1945Dec 23, 1947Leblanc Rolland AForming or bending die assembly for presses
US2828777 *Oct 14, 1954Apr 1, 1958Western Electric CoWire forming fixture
US6089061 *May 12, 1999Jul 18, 2000Northrop Grumman CorporationModularized reconfigurable heated forming tool
US6185978 *Mar 4, 1997Feb 13, 2001Accra Teknik AbMethod for manufacturing of curved and quenched profiled elements and a die tool for carrying out the method
US6928850 *Apr 19, 2004Aug 16, 2005Texas Instruments IncorporatedMethod and tooling for z-axis offset of lead frames
US20040194529 *Apr 19, 2004Oct 7, 2004Pelletier William J.Method and tooling for z-axis offset of lead frames
US20060042347 *Dec 15, 2003Mar 2, 2006Bae Systems PlcAircraft component manufacturing tool and method
EP0328476A2 *Feb 9, 1989Aug 16, 1989United Technologies CorporationMethod for fabricating integrally bladed rotors
Classifications
U.S. Classification72/305, 72/311, 72/413
International ClassificationB21D53/78, B21D53/00
Cooperative ClassificationB21D53/78
European ClassificationB21D53/78