US1289278A - Blade-mounting. - Google Patents
Blade-mounting. Download PDFInfo
- Publication number
- US1289278A US1289278A US15897717A US15897717A US1289278A US 1289278 A US1289278 A US 1289278A US 15897717 A US15897717 A US 15897717A US 15897717 A US15897717 A US 15897717A US 1289278 A US1289278 A US 1289278A
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- US
- United States
- Prior art keywords
- blade
- joint
- rivets
- tongues
- mounting
- 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.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
Definitions
- This invention relates to blade mountings and has for an object to produce a new and 1 improved blade mounting which is espe: cially adapted to be employed in attaching 5 greater efliciency I than any other rivetedblades to moving blade carrying elements.
- a further object is to produce a blade mounting which includes a riveted joint of blade mounting now in use and known to me.
- a further object is to produce a riveted blade mounting in which some of the rivets are subjected to more than double shear.
- a further object is to produce a blade mounting of high efli'ciency, which is simple.
- Fig. 2 is a modification of the blade mounting shown in Fig. 1.
- Fig. 3 is a sectional view of another embodiment of my invention.
- Fig. 4 is a diagrammatic sectional view of a blade mounting which illustrates one of the obj ects of my invention.
- Turbine blades have frequently been mounted by inserting their shanks in a v groove' in the blade carrying element and by then securing each blade shank in place with one or more locking members such as rivets.
- the ordmary construction consists I in a single groove in the blade carrying element and a single tongue on the blade shank so that the rivets are in double shear.
- I increase the efficiency and strength of the blade mounting by increasing the number of times some of the locking members or rivets are in shear. Although the number and size of the members or rivets are limited as before, the-strength of the joint is greatly increased by improving the efficiency of the joint. In carrying out my invention, I preferably provide .a
- Fig. 1 I have illustrated a portion of a blade carrying element 5 and a portion of a blade 6, which is mounted on the blade carrying element 5-.
- the shank of theblade 6 is shown as provided with three tongues 17, 8 and 9, which fit into grooves in the blade carrying element 5 and coiiperate with two tongues 10 and 11., formed, on the blade carrying element 5.
- llhe central tongue 8 of the blade shank is shown longer than the two side tongues 7 and 9, so that an inner locking member or rivet 12 passes through only the central tongue 8 and is therefore only in double shear.
- An outer locking member or rivet 13 passes through the tongues 7, 10, 11 and 9 and'is thereforein quadruple shear.
- a blade 19 mounted on a blade carrying member 20 in such a way thatin' order for the blade 19 to pull away from the blade carrying member it would be necessary to shear ofi' ten rivet sections.
- the blade 19 is provided with three tongues 21, 22 and 23, which coiiperate with ,two tongues 24 and 25, provided on the blade carrying member 20.
- a blade. shank forming an interleaving joint with a blade carrying element, and a plurality of rivets passed transversely through the interleavrivets being in more than double shear.
- a blade forming an interleaving joint with a blade carrying element, said joint consisting in part in a single tongue and groove joint and in part in a multiple'tongue and groove joint, and rivets passed through both the single and the multiple tongue and groove joints.
- a blade mounting comprising a blade forming a multiple tongue and groove joint with a blade carrying element, and rivets in difi'erent degrees of multiple shear for se- U connection pass through dilferent numbers of tongues, and rivets passing transversely through the connection.
- a blade mounting comprising a blade shank forming a multiple tongue and groove oint with a blade carrying element, the lengths of the tongues being such that rivets passed through the joint at varying distances from. the edge of the blade carrying element pass through a different number of tongues.
- a blade mounting comprising a bladeforming a multiple tongue and 'groove joint with a blade carrying element, and rivets in more than double shear for securing the blade in place.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Insertion Pins And Rivets (AREA)
Description
H. F. SCHMIDT.
BLADE MOUNTING.
APPLICATION FILED MAR. 31. 19:7.
.1,%89,278, Patented Dec. 31,1918.
J N VEN TOR.
15M wmm ATTORNEYS.
' HENRY F. 'SCHMIDT, OF PITTSBURGH, PENNSYLVANIA, AS SLIGN OR TO WESTINGHOUSE ELECTRIC & MANUFACTURING COMPANY, A CORPORATION OF PENNSXLVANIA.
BLADE-MOUNTING.
To all whom it may concern:
Be it known'that I, HENRY F. So, a
citizen of the United States, and a resident of Pittsburgh, in the county of Allegheny 5 and State of Pennsylvania, have made a new and useful Invention in Blade-Mounting, of
which the following is a specification.
This invention relates to blade mountings and has for an object to produce a new and 1 improved blade mounting which is espe: cially adapted to be employed in attaching 5 greater efliciency I than any other rivetedblades to moving blade carrying elements.
A further object is to produce a blade mounting which includes a riveted joint of blade mounting now in use and known to me. A further object is to produce a riveted blade mounting in which some of the rivets are subjected to more than double shear.
A further object is to produce a blade mounting of high efli'ciency, which is simple.
Fig. 2 is a modification of the blade mounting shown in Fig. 1.
Fig. 3 is a sectional view of another embodiment of my invention.
Fig. 4 is a diagrammatic sectional view of a blade mounting which illustrates one of the obj ects of my invention.
Turbine blades have frequently been mounted by inserting their shanks in a v groove' in the blade carrying element and by then securing each blade shank in place with one or more locking members such as rivets. The ordmary construction consists I in a single groove in the blade carrying element and a single tongue on the blade shank so that the rivets are in double shear. The
result would be the same if the blade shank straddled a single tongue on the blade carrylng element. size of the rivet or rivets is limited by the pitchof the blades and consequently by the In either construction, the
Specification of Letters Patent. I Patented Dec. 31, 1918. Application filed March 31, 1917. Serial N0. 158,977-
amount of material which may be left in the shank. The number of rivets of a vrea- 'sonable size is limited for the same reason. As the number and size of the rivets are limited, the strength and eflic'iency of the joint are also limited in the single tongue and groove construction.
In my invention I increase the efficiency and strength of the blade mounting by increasing the number of times some of the locking members or rivets are in shear. Although the number and size of the members or rivets are limited as before, the-strength of the joint is greatly increased by improving the efficiency of the joint. In carrying out my invention, I preferably provide .a
multiple tongue and groove joint between the blade shank and the blade carrying element, which is so formed as to throw all or a part of the locking members or rivets in more than double shear and. to thereby increase the efficiency and hence the strength of the joint. Obviously this may be done without increasing the weight of the joint, and at substantially'the same cost as the cost of the old construction, by increasing the number of tongues in the joint and by decreasing their thickness. It is evident that the efiiciency'of the joint is further increased by the greatly increased amount of surface, due to the multiple tongue construction, held in frictional engagement by the rivets. I
In Fig. 1, I have illustrated a portion of a blade carrying element 5 and a portion of a blade 6, which is mounted on the blade carrying element 5-. The shank of theblade 6 is shown as provided with three tongues 17, 8 and 9, which fit into grooves in the blade carrying element 5 and coiiperate with two tongues 10 and 11., formed, on the blade carrying element 5. llhe central tongue 8 of the blade shank is shown longer than the two side tongues 7 and 9, so that an inner locking member or rivet 12 passes through only the central tongue 8 and is therefore only in double shear. An outer locking member or rivet 13 passes through the tongues 7, 10, 11 and 9 and'is thereforein quadruple shear.
the blade carrying element 5, it would be necessary for it to shear off six rivet sections. If the multiple tongue construction were not provided, the total number of rivet In order for the blade to tear away from sections to be sheared oil would be only four, consequently the strength of the olnt has been increased by a shear area equal to twlce the section of one of the rivets. This is acsimilar to that shown in Fig. 1, but having a difierent distribution of the metal in the tongues of the joint. As before, ablade 14 is provided with three tongues 15, 16 and 17, which fit in grooves in a blade carrying member 18. In order to distribute the stresses to the best advantage, I have shown the tongue 16 as having two difi'erent thicknesses. As before, this joint has the shearing strength of six rivet cross sections.
In Fig. 3, I have shown a blade 19 mounted on a blade carrying member 20 in such a way thatin' order for the blade 19 to pull away from the blade carrying member it would be necessary to shear ofi' ten rivet sections. The blade 19 is provided with three tongues 21, 22 and 23, which coiiperate with ,two tongues 24 and 25, provided on the blade carrying member 20. The tongues 21, 24,
'23 and 25' are stepped so as to more uniformly distribute the stress throughout the joint. As shown, two rivets 26 and 27 are passed through the tongues 21, 24, 22, 25
- and 23 and one rivet is passed through the central tongue 22, which is longer than the other tongues carried by the blade 19. It
is evident that the" joint could be further strengthened 'by adding more tongues or more rivets if desired.
In 4, Ihave illustrated a theoretical construction in whichrthe amount of metal in the blade carrying element 82 is decreased as the amountin the blade shank 33 is increased, and vice versa. I have indicated three rivets A, B,. and C as being passed through the joint. The relatively small amount of metal immediately below the rivet O in the blade carrying element 32 I must support only the pull of the one rivet 66 construction illustrated in Figs. 1, 2, and 3 C. 'Below B the material'must sustain the pull of both B and C and is therefore thicker. Below A it must stand the cumulative pull of all three rivets A, B, andC and therefore has substantially three times as much net Conversely the mathis rivet and therefore the cross-sectional areaof the shank is small at this point. At C the shank sustains the cumulative pull of all three rivets and has substantially three times as much cross-section al area. The
ing joint, some of said 1,2se,27e
IVhile I have described and illustrated several embodimenm of my invention, it Wlll be apparent to those skilled in the art that various changes, modifications, additions and omissions may be made in the apparatus illustrated without departing from the spirit and scopeof the invention as set forth by the appended claims.
What I claim is:
1. In a blade mounting, a blade. shank forming an interleaving joint with a blade carrying element, and a plurality of rivets passed transversely through the interleavrivets being in more than double shear.
2. In a blade mounting, a blade forming an interleaving joint with a blade carrying element, said joint consisting in part in a single tongue and groove joint and in part in a multiple'tongue and groove joint, and rivets passed through both the single and the multiple tongue and groove joints.
3. A blade mounting comprising a blade forming a multiple tongue and groove joint with a blade carrying element, and rivets in difi'erent degrees of multiple shear for se- U connection pass through dilferent numbers of tongues, and rivets passing transversely through the connection.
5. A blade mounting comprising a blade shank forming a multiple tongue and groove oint with a blade carrying element, the lengths of the tongues being such that rivets passed through the joint at varying distances from. the edge of the blade carrying element pass through a different number of tongues.
6. A blade mounting comprising a bladeforming a multiple tongue and 'groove joint with a blade carrying element, and rivets in more than double shear for securing the blade in place. I
7. In a blade mounting, a joint'between a blade and a blade carrying element in which the cross-sectional area of the metal in each member of the joint increases from a .relatively small amount at the extremities of the members to substantially fifty per cent; of the total cross-sectional .anea in each subscribed niy narne this 30th day of-March, member near the center of the Joint, and 1917.
finally to substantially the full width of the joint, in eaeh member at the point therein HENRY S 5 adjacent to the extremity-0f the other mem- Witnesses:
ber. G. W. McGmm,
In testimony whereof, I have hereunto M. B. GORDON.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB114826D GB114826A (en) | 1917-03-31 | ||
US15897717A US1289278A (en) | 1917-03-31 | 1917-03-31 | Blade-mounting. |
FR489485A FR489485A (en) | 1917-03-31 | 1918-03-27 | Assembly of steam turbine blades |
US241433A US1345642A (en) | 1917-03-31 | 1918-06-22 | Blade-mounting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15897717A US1289278A (en) | 1917-03-31 | 1917-03-31 | Blade-mounting. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1289278A true US1289278A (en) | 1918-12-31 |
Family
ID=3356843
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US15897717A Expired - Lifetime US1289278A (en) | 1917-03-31 | 1917-03-31 | Blade-mounting. |
Country Status (1)
Country | Link |
---|---|
US (1) | US1289278A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2613058A (en) * | 1945-11-30 | 1952-10-07 | Atkinson Joseph | Cooled bladed rotor |
US2790620A (en) * | 1952-07-09 | 1957-04-30 | Gen Electric | Multiple finger dovetail attachment for turbine bucket |
US4135849A (en) * | 1977-01-21 | 1979-01-23 | Westinghouse Electric Corp. | Pinned root turbine blade providing maximum friction damping |
US5062769A (en) * | 1989-11-22 | 1991-11-05 | Ortolano Ralph J | Connector for turbine element |
US20140127026A1 (en) * | 2012-11-05 | 2014-05-08 | General Electric Company | Locking blade for a rotor |
US11306601B2 (en) * | 2018-10-18 | 2022-04-19 | Raytheon Technologies Corporation | Pinned airfoil for gas turbine engines |
-
1917
- 1917-03-31 US US15897717A patent/US1289278A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2613058A (en) * | 1945-11-30 | 1952-10-07 | Atkinson Joseph | Cooled bladed rotor |
US2790620A (en) * | 1952-07-09 | 1957-04-30 | Gen Electric | Multiple finger dovetail attachment for turbine bucket |
US4135849A (en) * | 1977-01-21 | 1979-01-23 | Westinghouse Electric Corp. | Pinned root turbine blade providing maximum friction damping |
US5062769A (en) * | 1989-11-22 | 1991-11-05 | Ortolano Ralph J | Connector for turbine element |
US20140127026A1 (en) * | 2012-11-05 | 2014-05-08 | General Electric Company | Locking blade for a rotor |
US9255483B2 (en) * | 2012-11-05 | 2016-02-09 | General Electric Company | Locking blade for a rotor |
US11306601B2 (en) * | 2018-10-18 | 2022-04-19 | Raytheon Technologies Corporation | Pinned airfoil for gas turbine engines |
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