US849992A - Turbine-blade. - Google Patents
Turbine-blade. Download PDFInfo
- Publication number
- US849992A US849992A US32287606A US1906322876A US849992A US 849992 A US849992 A US 849992A US 32287606 A US32287606 A US 32287606A US 1906322876 A US1906322876 A US 1906322876A US 849992 A US849992 A US 849992A
- Authority
- US
- United States
- Prior art keywords
- wheel
- rim
- turbine
- foot
- 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
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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
- F01D5/3023—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
Definitions
- This invention relates to an improved turbine-blade and means for securing the same; and its object is to provide simple and eective means for securing hollow blades of the crescent shaped cross-section type to the turbine-wheel.
- Figure 1 is a side elevation of a f1 agment of a wheel-rim with some blades in position.
- Fig. Zis a plan of Fig. 1.
- Fig. 3 is a cross-section on the hne 3 3 of Fig. 1.
- Fig. 4 is a cross-section of a modification'.
- the crescent-shaped hollow blade a is preferably formed in one piece with its four-cornered foot b by pressing from a pipe or by bendin of sheet metal to give the coniiguration s own, in which the foot forms a fourcornered box-like shell with the upwardlyextending crescent-shaped blade.
- the rim c of the wheel is rovided at intervals with transverse slots dividing the rim of the wheel into a plurality of four-cornered sec tions of a size adapted to iit snugly within the hollow foot b.
- a circular groove e is provided, and theblade-foot b is placed over its section and the metal of the same is pressed into the groove e when the blade is in position, the latter being thus securely fastened to the rim.
- Fig. 4 a modified form of attachment is shown according to which the-wheel is provided with a circumferential groove f, the foot b of the blade being made of a size to fit withinsaid roove.
- a bolt g extendm t ough the wheel-rim and the blade, ho ds the two snugly against relative g displacement.
- -of-blades having a hollow foot of angular cross-section arranged to embrace a portion of the wheel-rim, and means for securing the foot to the rim.
- blades each having a hollow foot arranged-to receive a section of the rim the material of said foot being forced into the said grooves at the sides.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
,992. PATENTED APR. 9 J. B.. PRIKART & 0. JAEGER.
TURBINE BLADE. APPLIGATION FILED JUNE'zz, 190e.
hlhllllllIIHllHh Ill;
UNITED STATES PATENT OEE-ICE.
TURBINE-BLADE.
Specification of Letter Patentl I Patented. April 9, 1907.
y Application filed June 22,1906. Serial No. 322,876.-
To a/ZZ whom it may concern.-
Be it known that we, J OHANN RUDOLF FRIKART, engineer, a citizen of Switzerland, and GsKAR JAEGER, engineer, a citizen of Germany, residing at Munich, Bavaria, Germany, have invented certain new and useful Improvements in Turbine-Blades and we do hereby declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
This invention relates to an improved turbine-blade and means for securing the same; and its object is to provide simple and eective means for securing hollow blades of the crescent shaped cross-section type to the turbine-wheel.
The details of the invention, as hereinafter more fully described and as particularly set out in the accompanying claims, will be readily understood by reference to the accompanying drawings, in which is illustrated a preferred embodiment of the invention with modiications.
In the drawings, Figure 1 is a side elevation of a f1 agment of a wheel-rim with some blades in position. Fig. Zis a plan of Fig. 1. Fig. 3 is a cross-section on the hne 3 3 of Fig. 1. Fig. 4 is a cross-section of a modification'.
The crescent-shaped hollow blade a is preferably formed in one piece with its four-cornered foot b by pressing from a pipe or by bendin of sheet metal to give the coniiguration s own, in which the foot forms a fourcornered box-like shell with the upwardlyextending crescent-shaped blade. The rim c of the wheel is rovided at intervals with transverse slots dividing the rim of the wheel into a plurality of four-cornered sec tions of a size adapted to iit snugly within the hollow foot b. Around the two sides of the wheel-rim a circular groove eis provided, and theblade-foot b is placed over its section and the metal of the same is pressed into the groove e when the blade is in position, the latter being thus securely fastened to the rim.
In Fig. 4 a modified form of attachment is shown according to which the-wheel is provided with a circumferential groove f, the foot b of the blade being made of a size to fit withinsaid roove. In this` case .a bolt g, extendm t ough the wheel-rim and the blade, ho ds the two snugly against relative g displacement.
It will be obvious that this invention is applicable as well to radial or axial turbines and that slight modifications of the detailsv would adapt the same for a wide range of use without departing from the spirit and scope of the invention. Y
Having thus described the invention, what we claim as new, and desire tosecure by Letters Patent, is-
'1. The combination with a turbine-wheel, of blades having a tubular foot, and means for securing the foot to the rim of the wheel.`
2. The combination with a turbine-wheel, of-blades having a tubular foot arranged to embrace a portion of the wheel-rim, and
means for securing the foot to the rim of the wheel. l
3. The combination, with a turbine-Wheel,
of blades having a tubular foot arranged in telescopic relation to a portion of the Wheelrlm.
4. The combination, with a turbine-wheel,A
of blades havin V a hollow foot of angular cross-section, an means for securing the foot to the rim of the wheel.
5. The combination, with a turbine-wheel,
-of-blades having a hollow foot of angular cross-section arranged to embrace a portion of the wheel-rim, and means for securing the foot to the rim. v v
6. The combination with a turbine-wheel provided on the side of its rim with a circular groove, of blades having -a hollow foot arranged to embrace a portion of the wheel-rim and provided with an inwardly-extending crease to enga e the groove.
7. The com ination with a turbine-wheel having its rim divided into sections, of blades each having a hollow foot arranged to receive a section of the rim. n
8. The combination with a turbine-wheel having its rim divided into sections and provided on its sides with circular grooves, of
blades each having a hollow foot arranged-to receive a section of the rim the material of said foot being forced into the said grooves at the sides.
IOC
9.- The combination with a turbine-wheel having its rim divided into sections and provided on each side Witha circular groove, of crescent-shaped hollow blades each having a 5 four-cornered hollow foot arranged to receive a section of the rim, the material of the said foot being forced into the said grooves at the, f
sides.
JOHANN RUDOLF FRIKART.
BESSE/S.
OSKAR JAEGER. Witnesses z ULYssEs. J. BY WATER,
GEORG KRNER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US32287606A US849992A (en) | 1906-06-22 | 1906-06-22 | Turbine-blade. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US32287606A US849992A (en) | 1906-06-22 | 1906-06-22 | Turbine-blade. |
Publications (1)
Publication Number | Publication Date |
---|---|
US849992A true US849992A (en) | 1907-04-09 |
Family
ID=2918453
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US32287606A Expired - Lifetime US849992A (en) | 1906-06-22 | 1906-06-22 | Turbine-blade. |
Country Status (1)
Country | Link |
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US (1) | US849992A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2435427A (en) * | 1946-09-16 | 1948-02-03 | United Specialties Co | Turbine wheel |
US2484274A (en) * | 1946-09-16 | 1949-10-11 | United Specialties Co | Turbine wheel |
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 |
US2658718A (en) * | 1944-12-22 | 1953-11-10 | Power Jets Res & Dev Ltd | Manufacture and attachment of turbine and like blading |
US2976014A (en) * | 1952-01-19 | 1961-03-21 | Bbc Brown Boveri & Cie | Blading for use in axial flow machines |
US3742706A (en) * | 1971-12-20 | 1973-07-03 | Gen Electric | Dual flow cooled turbine arrangement for gas turbine engines |
-
1906
- 1906-06-22 US US32287606A patent/US849992A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2658718A (en) * | 1944-12-22 | 1953-11-10 | Power Jets Res & Dev Ltd | Manufacture and attachment of turbine and like blading |
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 |
US2435427A (en) * | 1946-09-16 | 1948-02-03 | United Specialties Co | Turbine wheel |
US2484274A (en) * | 1946-09-16 | 1949-10-11 | United Specialties Co | Turbine wheel |
US2976014A (en) * | 1952-01-19 | 1961-03-21 | Bbc Brown Boveri & Cie | Blading for use in axial flow machines |
US3742706A (en) * | 1971-12-20 | 1973-07-03 | Gen Electric | Dual flow cooled turbine arrangement for gas turbine engines |
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