US1335002A - Blade - Google Patents

Blade Download PDF

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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
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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
Application number
US187246A
Inventor
Johnson Josiah Francis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric and Manufacturing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric and Manufacturing Co filed Critical Westinghouse Electric and Manufacturing Co
Priority to US187246A priority Critical patent/US1335002A/en
Application granted granted Critical
Publication of US1335002A publication Critical patent/US1335002A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • Y10T29/49339Hollow 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.
US187246A 1917-08-20 1917-08-20 Blade Expired - Lifetime US1335002A (en)

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US187246A US1335002A (en) 1917-08-20 1917-08-20 Blade

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Cited By (11)

* Cited by examiner, † Cited by third party
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

Cited By (15)

* Cited by examiner, † Cited by third party
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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