US1178452A - Turbine-blading. - Google Patents
Turbine-blading. Download PDFInfo
- Publication number
- US1178452A US1178452A US79277513A US1913792775A US1178452A US 1178452 A US1178452 A US 1178452A US 79277513 A US79277513 A US 79277513A US 1913792775 A US1913792775 A US 1913792775A US 1178452 A US1178452 A US 1178452A
- Authority
- US
- United States
- Prior art keywords
- rim
- roots
- plates
- grooves
- blade
- 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
Links
- 238000012856 packing Methods 0.000 description 7
- 239000011324 bead Substances 0.000 description 5
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 2
- 244000182067 Fraxinus ornus Species 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004326 stimulated echo acquisition mode for imaging Methods 0.000 description 1
Images
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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
-
- 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
- F01D5/3069—Fixing blades to rotors; Blade roots ; Blade spacers between two discs or rings
Definitions
- Figs. 3 and 4 are detail views show-' ing the blade roots and packing pieces.
- a denotes the rim of the rotor which may be a continuous ring or may be of segments butted end to end.
- This rim is transversely slotted in its outer periphery as at b to receive the roots 0 of the blades (Z, and usually packing pieces 6, it being understood that the roots have fiat front and irregular rear faces, the packing pieces fitting in back of the roots and filling the slots I).
- circumferential grooves f are cut in the rim, roots and packing pieces at both sides.
- Side plates g, 9, having beads h, h, which fit in the grooves f, f, are next applied and clamped to the rim in any convenient manner as by the headed pins 2'.
- the rim is provided with circumferential side shoulders 70, vis, to which the side plates 9, g, are fitted to withstand the centrifugal force occasioned by the rotation of the rotor.
- the outer ends of the blades may be shrouded in any desired manner as 1s usual in structures of this sort.
- the securing means herelnabove described constitute an extremely strong and secure fastening which may be economically manufactured, and one in which the parts are well supported against the heavy strains to which they are subjected.
- FIG. 2 1s a side.
- an annular rim having transverse slots in its outer edge, laterally extending shoulders at thesides of the rim below the slots, circumferential grooves in the sides of the, slotted portion of the rim, blades with their roots located in the slots and with their edges grooved, in alinement with the grooves in the rim, side plates fitted to saidrim and provided with shoulders adapted to engage theshoulders on the rim, and beads'adaptedto fit in the grooves and interengaging parts on said plates and roots.
- a rim having its outer edge transversely slotted, blades with roots fitting in said slots, side plates located against the sides of the rim, means for holding them inposition, interengaging parts on said plates and rim, packing pieces located in the slots back of the'blade roots,
- a shaft a rim provided with lateral shouldersat its base and transversely slotted in its periphery, blades With roots fitting said and notches in the rim and blade roots, and slots, circumferential grooves in the sides means located just inside of said rim for 10 of the slotted portion of the rim, notches in clamping said plates onto said rim.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
W. J. A. LONDON.
' TURBINE BLADING. APPLICATION. FILEDOCT. 1. 1913.
1,178,452., Patented Apr. 4, 1916.
INVENTOR.
WITN
William J A. London:
m. ZMQM A T] 'ORNE Y i iii WILLIAM J. A. LONDON, or HARTFORD, coNNEoTIoUT, assrelvort; To THE TERRY STEAM TURBINE COMPANY, or HARTF R CONNECTICUT A CORPORATION or v CONNECTICUT. v 1, TURBINE-BL DING. p y
,jspecification of Letters Patent. l Patented A 4 1916 To all whom it may concern:
Be it known that I, IVILLIAM J. A. LoN-v DON, a subject of the King of England, and resident of Hartford, county of Hartford, and State of Connecticut, have invented certain new and useful Improvements in view thereof with one of theside plates removed. Figs. 3 and 4 are detail views show-' ing the blade roots and packing pieces.
Referring to the drawings a denotes the rim of the rotor which may be a continuous ring or may be of segments butted end to end. This rim is transversely slotted in its outer periphery as at b to receive the roots 0 of the blades (Z, and usually packing pieces 6, it being understood that the roots have fiat front and irregular rear faces, the packing pieces fitting in back of the roots and filling the slots I).
Then all of the blades and packing pieces have been assembled on the rim, circumferential grooves f are cut in the rim, roots and packing pieces at both sides. Side plates g, 9, having beads h, h, which fit in the grooves f, f, are next applied and clamped to the rim in any convenient manner as by the headed pins 2'. The rim is provided with circumferential side shoulders 70, vis, to which the side plates 9, g, are fitted to withstand the centrifugal force occasioned by the rotation of the rotor.
At the center of the side plates a suitable hub-may be provided by which the rotor 'may be mounted on a shaft. The outer ends of the blades may be shrouded in any desired manner as 1s usual in structures of this sort.
The securing means herelnabove described constitute an extremely strong and secure fastening which may be economically manufactured, and one in which the parts are well supported against the heavy strains to which they are subjected.
I intend to secure herein any changes or modifications in the structure which'come within the scope of the appended claims.
sectional view of part of a rotor showing the blade-fastening means. Fig. 2 1s a side.
I claim as my invention 1. In a blade-fastening device of thecharacter described, a rim transversely slotted,
in its periphery, blades with roots located 1n sa1d slots, alined grooves in the sides of said rim and the edges of said roots, plates secured to the sides of said rim, and beads thereon adapted to fit said grooves 2. In a blade-fastening device of the character described, an annular rim having transverse slots in its outer edge, laterally extending shoulders at thesides of the rim below the slots, circumferential grooves in the sides of the, slotted portion of the rim, blades with their roots located in the slots and with their edges grooved, in alinement with the grooves in the rim, side plates fitted to saidrim and provided with shoulders adapted to engage theshoulders on the rim, and beads'adaptedto fit in the grooves and interengaging parts on said plates and roots. p
4. In a blade-fastening device of the character described, a rim having its outer edge transversely slotted, blades with roots fitting in said slots, side plates located against the sides of the rim, means for holding them inposition, interengaging parts on said plates and rim, packing pieces located in the slots back of the'blade roots,
and interlocking parts onsaid plates and I said blade roots and packing pieces.
' 5.'In a device of the character described, a shaft, a rim provided with lateral shoulders at its base'and transversely slotted in its periphery, blades with roots fitting said slots, circumferential grooves in thesides of the slotted portion of the rim, notches in the blade roots alined with said grooves,
plates secured to said'shaft and supporting said rimbetween them; shoulders on the plates engaging the shoulders on the rim, and beads on the plates fitting in the grooves and notchesin the rim and blade roots.
6. In a device of the character described, a shaft, a rim provided with lateral shouldersat its base and transversely slotted in its periphery, blades With roots fitting said and notches in the rim and blade roots, and slots, circumferential grooves in the sides means located just inside of said rim for 10 of the slotted portion of the rim, notches in clamping said plates onto said rim.
the blade roots alined With said grooves, T plates secured to said shaft and supporting WILLIAM LOND01\' said rim between them, shouldersv on the Witnesses:
plates engaging the shoulders on the rim, H. E. HART,
beads on the plates fitting in the grooves A. E. OBRIEN.
Copies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents,
' Washington, D. G.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US79277513A US1178452A (en) | 1913-10-01 | 1913-10-01 | Turbine-blading. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US79277513A US1178452A (en) | 1913-10-01 | 1913-10-01 | Turbine-blading. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1178452A true US1178452A (en) | 1916-04-04 |
Family
ID=3246441
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US79277513A Expired - Lifetime US1178452A (en) | 1913-10-01 | 1913-10-01 | Turbine-blading. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1178452A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2559013A (en) * | 1946-01-25 | 1951-07-03 | United Specialties Co | Method of making turbine wheels |
| US2601969A (en) * | 1946-01-25 | 1952-07-01 | United Specialties Co | Turbine wheel |
| US2701120A (en) * | 1945-10-22 | 1955-02-01 | Edward A Stalker | Turbine blade construction with provision for cooling |
| US2916257A (en) * | 1953-12-30 | 1959-12-08 | Gen Electric | Damping turbine buckets |
| US2981517A (en) * | 1958-08-18 | 1961-04-25 | Georges Raymond Emile | Bladed wheels, more particularly for gas turbines |
| US3055633A (en) * | 1957-04-19 | 1962-09-25 | Pouit Robert | Hot gas turbines |
| DE102016219818A1 (en) * | 2016-10-12 | 2018-04-12 | Rolls-Royce Deutschland Ltd & Co Kg | Blade assembly with ring segment or disc segment-shaped blade carrier and radially inner stiffening structure |
| US10794188B2 (en) | 2016-10-12 | 2020-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor blade assembly comprising a ring-shaped or disc-shaped blade carrier and a radially inner reinforcement structure |
-
1913
- 1913-10-01 US US79277513A patent/US1178452A/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2701120A (en) * | 1945-10-22 | 1955-02-01 | Edward A Stalker | Turbine blade construction with provision for cooling |
| US2559013A (en) * | 1946-01-25 | 1951-07-03 | United Specialties Co | Method of making turbine wheels |
| US2601969A (en) * | 1946-01-25 | 1952-07-01 | United Specialties Co | Turbine wheel |
| US2916257A (en) * | 1953-12-30 | 1959-12-08 | Gen Electric | Damping turbine buckets |
| US3055633A (en) * | 1957-04-19 | 1962-09-25 | Pouit Robert | Hot gas turbines |
| US2981517A (en) * | 1958-08-18 | 1961-04-25 | Georges Raymond Emile | Bladed wheels, more particularly for gas turbines |
| DE102016219818A1 (en) * | 2016-10-12 | 2018-04-12 | Rolls-Royce Deutschland Ltd & Co Kg | Blade assembly with ring segment or disc segment-shaped blade carrier and radially inner stiffening structure |
| US10794199B2 (en) | 2016-10-12 | 2020-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor blade assembly comprising a ring segment shaped or disc segment shaped blade carrier and a radially inner reinforcement structure |
| US10794188B2 (en) | 2016-10-12 | 2020-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor blade assembly comprising a ring-shaped or disc-shaped blade carrier and a radially inner reinforcement structure |
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