US1335002A - Blade - Google Patents
Blade Download PDFInfo
- Publication number
- US1335002A US1335002A US187246A US18724617A US1335002A US 1335002 A US1335002 A US 1335002A US 187246 A US187246 A US 187246A US 18724617 A US18724617 A US 18724617A US 1335002 A US1335002 A US 1335002A
- Authority
- US
- United States
- Prior art keywords
- blade
- tip
- wearing
- rub
- blades
- 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
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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
Definitions
- This invention relates to blades and has for an object to produce a blade which provided with a wearing tip which will read ily yield to abrasion, and will therefore prerent damage to the blade in case of a blade rub.
- a l further object is to produce a. blade having a tip of full cross sectional area but of greatly reduced abrasion resisting characteristics.
- the amount of leakage through the clearance space at the end of the blade is materially reduced, below that encountered where the blade is reduced in section at the end to provide a wiarii'igz edge, due to the fact that the leakage space is bounded by surfaces having appreciable area.
- Figure 1 is diagrammatic elevation of a blade embodying my invention.
- Fig. '2 is a plan view of a blade shown in Fig. 1.
- Fig. 3 is a diagrammatic view of a. blade illustrating a modification of my invention.
- Fig. dis a plan view of the blade shown in llig. 3.
- Fig. 5 is a diagrammatic view of a blade illustrating a further modification of my invention.
- Figs. 1 and 2 l have shown the outer or free end of a blade 5.
- the blade In order that the outer or free end 6 may have the freely wearing characteristics required to elin'iinate any danger of damage due to blade rub, l: have shown the blade as provided with a. depression 7, which is so formed as to leave only a narrow wall. 8 of the material of which the blade is formed. This depression is preferably filled with a material which may be easily worn away. T he thin walls 8 surrounding the wearing material are thin enough to wear away as readily as the wearing material, in case of blade rub, and consequently the danger of any damage to the turbine resulting from a blade rub is completely eliminated.
- a blade 10 which, as shown, is provided with a dove-tailed slot 11 out in its tip.
- a. soft metal blade tip 12 is inserted in the slot 11 and is formed with outer flanges 13 and 14:, so as to cover the entire end of the blade 10, as shown in Fig. 41 Consequently, in case of blade rub, only the soft tip 12 comes in contact with. the adjacent element and is, of course, quickly worn away without any damage to the rest of the blade or to the turbine.
- I have shown a blade 15 having a dovetailed slot 16 cut in its outer end, in which an inlay 17 of soft or friable ntiaterial may be placed.
- the tips 18 and 19 of the blade body 15 extend clear out to the end of the blade, but as they are of relatively small cross section they will be quickly worn away in case of blade rub along with the soft or friable material 17.
- the blade is of full cross section clear out to its tip. consequently no portion of the working; surface is lost in securing the easy wearing characteristics required.
- the wire drawing at the ends of the blades is increased with the result that the small clearance is effective in reducing leaking at the ends of the blades.
- a turbine blade terminating in a recessed tip portion having a Working surface similar to that of the body of the blade, and a Wearing tip having a relatively low abrasion resisting characteristic mounted in the recess flush with the tip and held against lateral displacement by the portions of the blade overlapping the tip.
- a turbine blade having a substantially uniform cross-section throughout its Working surface, terminating in a recessed tip portion having a Working surface similar to that ol the body of the blade, and a wearing tip having a relatively low abrasion resisting clmracteristic mounted in the recess flush with the tip and held against lateral displacement by the portions of the blade overlapping the Wearing tip.
- a turbine blade terminating in a tip portion having a Working surface similar to that of the body of the blade and provided with an undercut recess and a wearing tip having a relatively low abrasion resisting characteristic mounted in the recess and held against lateral displacement by the portion of the blade overlapping the tip.
Description
J. F. JOHNSON.
BLADE.
APPLICATION FILED AUG-20, I917- Patented Mar. 30, 1920.
IfiVENYDR. I BY ATIIORNEYS.
lll ll llillll STATES llflAfTllllfillll Olllll l(illiv JUSIAH FRANCIS JGHNSUN, OF EDGE'W'UUD, PENNSYLVANIA, AbEiITrNUIt TO HOUSE ELECTRIC & Mlll'ii- COMPANY, A. GGRPORATIWN O35 PENNESYLVAIEHA.
v 13mins.
tat-races.
To all whom may concern:
Be it known that l, Josran than are J 0111(- son, a. citizen of the lJlllllQCl States, and a resident of Edgewood, in the county of Allegheny and Eltate of Pennsylvania, have made a new and useful lnvention in Blades, of which the following is a specification.
This invention relates to blades and has for an object to produce a blade which provided with a wearing tip which will read ily yield to abrasion, and will therefore prerent damage to the blade in case of a blade rub.
a l further object is to produce a. blade having a tip of full cross sectional area but of greatly reduced abrasion resisting characteristics.
These and other objects are attained by means of the blades embodying; the features herein described and illustrated in the drawings accompanying and forming a part hereof.
ln some types of turbines it is common practice to provide small clearances between the free ends of the blades and the adjacent blade atrrying elen'ient. lily invention contemplates the production of a blade which is especially adapted to be employed under conditions where small clearances between the end of the blade and an adjacent element are essential. l accomplish this by proriding the blade with a tip which effectually eliminates any danger of damage to the turbine due to blade rub due to the fact that the tip will readily wear away or yield when subject to a rub. An additional feature of the invention is that a blade so equipped presents an unimpaired working face from the mounting elen'ient to the free end of the blade. In addition to this, the amount of leakage through the clearance space at the end of the blade is materially reduced, below that encountered where the blade is reduced in section at the end to provide a wiarii'igz edge, due to the fact that the leakage space is bounded by surfaces having appreciable area.
In drawings: Figure 1 is diagrammatic elevation of a blade embodying my invention.
Fig. '2 is a plan view of a blade shown in Fig. 1.
Fig. 3 is a diagrammatic view of a. blade illustrating a modification of my invention.
Specification. of Letters Patent. Pgitgnted H1 PM}, 192
Application filed. August 20, 1917.
Fig. dis a plan view of the blade shown in llig. 3.
Fig. 5 is a diagrammatic view of a blade illustrating a further modification of my invention.
In Figs. 1 and 2 l have shown the outer or free end of a blade 5. In order that the outer or free end 6 may have the freely wearing characteristics required to elin'iinate any danger of damage due to blade rub, l: have shown the blade as provided with a. depression 7, which is so formed as to leave only a narrow wall. 8 of the material of which the blade is formed. This depression is preferably filled with a material which may be easily worn away. T he thin walls 8 surrounding the wearing material are thin enough to wear away as readily as the wearing material, in case of blade rub, and consequently the danger of any damage to the turbine resulting from a blade rub is completely eliminated.
In Fig. 3, l have illustrated the outer end of a blade 10 which, as shown, is provided with a dove-tailed slot 11 out in its tip. a. soft metal blade tip 12 is inserted in the slot 11 and is formed with outer flanges 13 and 14:, so as to cover the entire end of the blade 10, as shown in Fig. 41 Consequently, in case of blade rub, only the soft tip 12 comes in contact with. the adjacent element and is, of course, quickly worn away without any damage to the rest of the blade or to the turbine. In Fig. 5, I have shown a blade 15 having a dovetailed slot 16 cut in its outer end, in which an inlay 17 of soft or friable ntiaterial may be placed. On each side of the slot 16, the tips 18 and 19 of the blade body 15 extend clear out to the end of the blade, but as they are of relatively small cross section they will be quickly worn away in case of blade rub along with the soft or friable material 17.
In all the embodiments of my invention shown, the blade is of full cross section clear out to its tip. consequently no portion of the working; surface is lost in securing the easy wearing characteristics required. In addition to this, the wire drawing at the ends of the blades is increased with the result that the small clearance is effective in reducing leaking at the ends of the blades.
While I have illustrated and described several embodiments of my invention, it will by the appended claims.
lVhat I claim is:
1. A turbine blade terminating in a recessed tip portion having a Working surface similar to that of the body of the blade, and a Wearing tip having a relatively low abrasion resisting characteristic mounted in the recess flush with the tip and held against lateral displacement by the portions of the blade overlapping the tip.
2. A turbine blade having a substantially uniform cross-section throughout its Working surface, terminating in a recessed tip portion having a Working surface similar to that ol the body of the blade, and a wearing tip having a relatively low abrasion resisting clmracteristic mounted in the recess flush with the tip and held against lateral displacement by the portions of the blade overlapping the Wearing tip.
3. A turbine blade terminating in a tip portion having a Working surface similar to that of the body of the blade and provided with an undercut recess and a wearing tip having a relatively low abrasion resisting characteristic mounted in the recess and held against lateral displacement by the portion of the blade overlapping the tip.
In testimony whereof I have hereunto subscribed my name this 17th: day of August, 1917.
JOSIAH FRANCIS JOHNSON.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US187246A US1335002A (en) | 1917-08-20 | 1917-08-20 | Blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US187246A US1335002A (en) | 1917-08-20 | 1917-08-20 | Blade |
Publications (1)
Publication Number | Publication Date |
---|---|
US1335002A true US1335002A (en) | 1920-03-30 |
Family
ID=22688188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US187246A Expired - Lifetime US1335002A (en) | 1917-08-20 | 1917-08-20 | Blade |
Country Status (1)
Country | Link |
---|---|
US (1) | US1335002A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2507079A (en) * | 1946-06-19 | 1950-05-09 | Charles H Zimmerman | Abrading mechanism |
US3294315A (en) * | 1964-09-28 | 1966-12-27 | Buffalo Forge Co | Fan construction |
US4728262A (en) * | 1986-01-22 | 1988-03-01 | Textron Inc. | Erosion resistant propellers |
EP0273852A2 (en) * | 1986-12-29 | 1988-07-06 | United Technologies Corporation | Turbine blade having a fused metal-ceramic abrasive tip |
EP1072759A1 (en) * | 1999-07-29 | 2001-01-31 | General Electric Company | Tip insulated airfoil |
US20080145207A1 (en) * | 2006-12-14 | 2008-06-19 | General Electric | Systems for preventing wear on turbine blade tip shrouds |
US20110014060A1 (en) * | 2009-07-17 | 2011-01-20 | Rolls-Royce Corporation | Substrate Features for Mitigating Stress |
JP2014508883A (en) * | 2011-02-22 | 2014-04-10 | シーメンス アクティエンゲゼルシャフト | Method for manufacturing a protective layer for a rotor blade |
US20170044927A1 (en) * | 2014-04-30 | 2017-02-16 | Borgwarner Inc. | Lock-up prevention vane for variable geometry turbocharger |
US9713912B2 (en) | 2010-01-11 | 2017-07-25 | Rolls-Royce Corporation | Features for mitigating thermal or mechanical stress on an environmental barrier coating |
US10040094B2 (en) | 2013-03-15 | 2018-08-07 | Rolls-Royce Corporation | Coating interface |
-
1917
- 1917-08-20 US US187246A patent/US1335002A/en not_active Expired - Lifetime
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2507079A (en) * | 1946-06-19 | 1950-05-09 | Charles H Zimmerman | Abrading mechanism |
US3294315A (en) * | 1964-09-28 | 1966-12-27 | Buffalo Forge Co | Fan construction |
US4728262A (en) * | 1986-01-22 | 1988-03-01 | Textron Inc. | Erosion resistant propellers |
EP0273852A2 (en) * | 1986-12-29 | 1988-07-06 | United Technologies Corporation | Turbine blade having a fused metal-ceramic abrasive tip |
EP0273852A3 (en) * | 1986-12-29 | 1989-11-29 | United Technologies Corporation | Turbine blade having a fused metal-ceramic abrasive tip |
EP1072759A1 (en) * | 1999-07-29 | 2001-01-31 | General Electric Company | Tip insulated airfoil |
US20080145207A1 (en) * | 2006-12-14 | 2008-06-19 | General Electric | Systems for preventing wear on turbine blade tip shrouds |
US7771171B2 (en) * | 2006-12-14 | 2010-08-10 | General Electric Company | Systems for preventing wear on turbine blade tip shrouds |
US20110014060A1 (en) * | 2009-07-17 | 2011-01-20 | Rolls-Royce Corporation | Substrate Features for Mitigating Stress |
US9194243B2 (en) * | 2009-07-17 | 2015-11-24 | Rolls-Royce Corporation | Substrate features for mitigating stress |
US9713912B2 (en) | 2010-01-11 | 2017-07-25 | Rolls-Royce Corporation | Features for mitigating thermal or mechanical stress on an environmental barrier coating |
JP2014508883A (en) * | 2011-02-22 | 2014-04-10 | シーメンス アクティエンゲゼルシャフト | Method for manufacturing a protective layer for a rotor blade |
US10040094B2 (en) | 2013-03-15 | 2018-08-07 | Rolls-Royce Corporation | Coating interface |
US20170044927A1 (en) * | 2014-04-30 | 2017-02-16 | Borgwarner Inc. | Lock-up prevention vane for variable geometry turbocharger |
DE112015002061B4 (en) | 2014-04-30 | 2021-07-22 | Borgwarner Inc. | ANTI-LOCKING VAN FOR A TURBOCHARGER WITH ADJUSTABLE GEOMETRY |
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