[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

US1050119A - Turbine-blade. - Google Patents

Turbine-blade. Download PDF

Info

Publication number
US1050119A
US1050119A US60717611A US1911607176A US1050119A US 1050119 A US1050119 A US 1050119A US 60717611 A US60717611 A US 60717611A US 1911607176 A US1911607176 A US 1911607176A US 1050119 A US1050119 A US 1050119A
Authority
US
United States
Prior art keywords
blades
blade
base strip
openings
turbine
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
US60717611A
Inventor
Warren B Flanders
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.)
COLONIAL TRUST CO
Original Assignee
COLONIAL TRUST 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 COLONIAL TRUST CO filed Critical COLONIAL TRUST CO
Priority to US60717611A priority Critical patent/US1050119A/en
Application granted granted Critical
Publication of US1050119A publication Critical patent/US1050119A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32Locking, e.g. by final locking blades or keys
    • 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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines

Definitions

  • WITNESSES INVENTOR' J ⁇ ⁇ NW 3%. 5mm Qw/WQ UNITED STATliS PATENT OFFICE.
  • This invention relates to means for securing blades or vanes to a blade holding element.
  • Figure 1 is a fragmental perspective view vof a base strip to which a plurality of blades are attached;
  • Fig. 2 is a plan View of the base strip, the blades being shown in section;
  • Fig. 3 is a section on the line 33 of Fig. 2;
  • Fig. 4 is a detail perspective View. of one of the inserts or fastening devices for securing the blades and base strip together.
  • a preferred embodimentrof myinvention is illustrated in the drawings as comprising a base strip 5 having a straight side 6 and an incline side 'T; the incline side being adapted to fit in an undercut portion in a groove ir the element which is adapted to receive it.
  • the strip 5 is illustrated as being provided with a plurality of approximately comma-shaped openings 8, whichextend laterally through the strip 5 and which are adapted to receive the ends of blades 9.
  • the contours of the blades are concavo-convex, that is, the convex face 10 of each blade 9 will be of approximately the same shape as the edge 11 of the opening 8 which receives it.
  • each blade 9 is less than the width of the opening 8 so that the space between the concave portion 12 of each blade and the edge 13 of the opening 8 may be filled by an insert or filler piece 14.
  • the filler piece or insert 1a is best shown in Fig. t as being approximately comma-shaped in cross section.
  • the blades and inserts may be introduced into the openings 8 of the base strip and the inserts swaged or calked into the sockets or openings 8 so as to upset them; that is, change the cross sectional area of the insert and thereby securely fasten the roots of the blades 9 in the base strip.
  • Units comprising a base strip, blades and inserts or packing pieces may be made of any desiredlengths ready to be inserted into the turbine element to receive them.
  • the preferred form of base strip will be that shown in Fig. 1 so that the base strips may be put in grooves and fastened in by wedges in a manner commonly employed at this time; however, it is obvious that the particular form of base strip shown is not essential to my invention.
  • a base strip having a plurality of openings, a blade for each opening and havin its convex side bearing against one edge 0 the opening, a space being formed between the convex side of the blade and the opensubscribed my name this 3rd day of Febing, and a packing piece insertible in said ruary, 1911, space to fasten the blade in its opening, the

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

W. B. FLANDERS.
TURBINE BLADE.
APPLICATION FILED r1113. 7, 1911.
1,050,1 19. Patented Jan. 14, 1913.
WITNESSES: INVENTOR' J} \NW 3%. 5mm Qw/WQ UNITED STATliS PATENT OFFICE.
WARREN B. FLANDERS, 0F PITTSBURGH, PENNSYLVANIA, ASSIGNOR, BYEMESNE AS SIGNMIENTS, TO THE COLONIAL TRUST COMPANY, TRUSTEE, OF PITTSBURGH, PENN- SYLVANIA, A CORPORATION OF PENNSYLVANIA.
TURBINE-BLADE.
Specification of Letters Patent.
Patented Jan. 14, 1913.
To all whom it may concern Be it known that I, \VARREN B. FLANonRs, a citizen of the United States, and a resident of Pittsburgh, in the county of Allegheny and State of Pennsylvania, have made a new and useful Invention in Turbine- Blades, of which the following is a specification.
This invention relates to means for securing blades or vanes to a blade holding element.
As an example of the application of the invention I have illustrated blades for Parsons type turbine secured to a base strip by suitable fastening devices.
In the drawings: Figure 1 is a fragmental perspective view vof a base strip to which a plurality of blades are attached; Fig. 2 is a plan View of the base strip, the blades being shown in section; Fig. 3 is a section on the line 33 of Fig. 2; and Fig. 4 is a detail perspective View. of one of the inserts or fastening devices for securing the blades and base strip together.
A preferred embodimentrof myinvention is illustrated in the drawings as comprising a base strip 5 having a straight side 6 and an incline side 'T; the incline side being adapted to fit in an undercut portion in a groove ir the element which is adapted to receive it. The strip 5 is illustrated as being provided with a plurality of approximately comma-shaped openings 8, whichextend laterally through the strip 5 and which are adapted to receive the ends of blades 9. The contours of the blades are concavo-convex, that is, the convex face 10 of each blade 9 will be of approximately the same shape as the edge 11 of the opening 8 which receives it. The thickness of each blade 9 is less than the width of the opening 8 so that the space between the concave portion 12 of each blade and the edge 13 of the opening 8 may be filled by an insert or filler piece 14. The filler piece or insert 1a is best shown in Fig. t as being approximately comma-shaped in cross section. The blades and inserts may be introduced into the openings 8 of the base strip and the inserts swaged or calked into the sockets or openings 8 so as to upset them; that is, change the cross sectional area of the insert and thereby securely fasten the roots of the blades 9 in the base strip.
Units comprising a base strip, blades and inserts or packing pieces may be made of any desiredlengths ready to be inserted into the turbine element to receive them. The preferred form of base strip will be that shown in Fig. 1 so that the base strips may be put in grooves and fastened in by wedges in a manner commonly employed at this time; however, it is obvious that the particular form of base strip shown is not essential to my invention.
Having thus described my invention What I claim and desire to secure by Letters Patent is:
1. The combination of a base strip having approximately comma-shaped openings, blades in the openings and inserts filling the spaces between the faces of the blades and edges of the openings.
The combination with a base strip having a plurality of openings therein, blades fitting in the openings and packing ieces for securing the root-s of the blades 1n the openings in the strip, the packing pieces being of approximately the same cross-sectional area as the spaces which are to receive them.
3. The combination with a base strip having comma shaped openings, blades in the openings and having their convexed faces conforming to one side of an opening in the strip, and a packing piece interposed in the opening between a concave face of the blade and one edge of the opening.
4.. A base strip having a plurality of openings, a blade for each opening and havin its convex side bearing against one edge 0 the opening, a space being formed between the convex side of the blade and the opensubscribed my name this 3rd day of Febing, and a packing piece insertible in said ruary, 1911, space to fasten the blade in its opening, the
packing pieces being of approximately the V WARREN FLANDERS' 5 same cross-sectional area as the spaces-which Witnesses:
are to receive them. C. W. MQGHEE,
In testimony whereof, I have hereunto B. M. FERO.
US60717611A 1911-02-07 1911-02-07 Turbine-blade. Expired - Lifetime US1050119A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US60717611A US1050119A (en) 1911-02-07 1911-02-07 Turbine-blade.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US60717611A US1050119A (en) 1911-02-07 1911-02-07 Turbine-blade.

Publications (1)

Publication Number Publication Date
US1050119A true US1050119A (en) 1913-01-14

Family

ID=3118386

Family Applications (1)

Application Number Title Priority Date Filing Date
US60717611A Expired - Lifetime US1050119A (en) 1911-02-07 1911-02-07 Turbine-blade.

Country Status (1)

Country Link
US (1) US1050119A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4893990A (en) * 1987-10-07 1990-01-16 Matsushita Electric Industrial Co., Ltd. Mixed flow impeller
US9682756B1 (en) 2016-10-17 2017-06-20 General Electric Company System for composite marine propellers
US20170204728A1 (en) * 2014-06-26 2017-07-20 Mitsubishi Heavy Industries, Ltd. Turbine rotor blade row, turbine stage, and axial-flow turbine
US20180030835A1 (en) * 2015-02-10 2018-02-01 Mitsubishi Hitachi Power Systems, Ltd. Turbine and gas turbine
US10125619B2 (en) 2015-11-19 2018-11-13 General Electric Company Rotor assembly for use in a turbofan engine and method of assembling
US10486785B2 (en) 2016-10-17 2019-11-26 General Electric Company Propeller assembly and method of assembling
US10633067B2 (en) 2016-10-17 2020-04-28 General Electric Company Method and system for improving flow characteristics in marine propellers
US10689073B2 (en) 2016-10-17 2020-06-23 General Electric Company Apparatus and system for marine propeller blade dovetail stress reduction
US10703452B2 (en) 2016-10-17 2020-07-07 General Electric Company Apparatus and system for propeller blade aft retention
US11052982B2 (en) 2016-10-17 2021-07-06 General Electric Company Apparatus for dovetail chord relief for marine propeller

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4893990A (en) * 1987-10-07 1990-01-16 Matsushita Electric Industrial Co., Ltd. Mixed flow impeller
US20170204728A1 (en) * 2014-06-26 2017-07-20 Mitsubishi Heavy Industries, Ltd. Turbine rotor blade row, turbine stage, and axial-flow turbine
US11220909B2 (en) * 2014-06-26 2022-01-11 Mitsubishi Heavy Industries, Ltd. Turbine rotor blade row, turbine stage, and axial-flow turbine
US20180030835A1 (en) * 2015-02-10 2018-02-01 Mitsubishi Hitachi Power Systems, Ltd. Turbine and gas turbine
US10655471B2 (en) * 2015-02-10 2020-05-19 Mitsubishi Hitachi Power Systems, Ltd. Turbine and gas turbine
US10125619B2 (en) 2015-11-19 2018-11-13 General Electric Company Rotor assembly for use in a turbofan engine and method of assembling
US9682756B1 (en) 2016-10-17 2017-06-20 General Electric Company System for composite marine propellers
US10486785B2 (en) 2016-10-17 2019-11-26 General Electric Company Propeller assembly and method of assembling
US10633067B2 (en) 2016-10-17 2020-04-28 General Electric Company Method and system for improving flow characteristics in marine propellers
US10689073B2 (en) 2016-10-17 2020-06-23 General Electric Company Apparatus and system for marine propeller blade dovetail stress reduction
US10703452B2 (en) 2016-10-17 2020-07-07 General Electric Company Apparatus and system for propeller blade aft retention
US11052982B2 (en) 2016-10-17 2021-07-06 General Electric Company Apparatus for dovetail chord relief for marine propeller

Similar Documents

Publication Publication Date Title
US1544318A (en) Turbine-blade lashing
US1050119A (en) Turbine-blade.
US1719415A (en) Turbine-blade attachment
US1165005A (en) Blade construction for elastic-fluid turbines.
US1717203A (en) Bladed-turbine structure
US1247400A (en) Blading for elastic-fluid turbines.
US1010750A (en) Turbine-balde shroud.
US1050187A (en) Blade-mounting.
US1072457A (en) Blade-mounting.
US1073623A (en) Steam-turbine blade.
US1149658A (en) Turbine-blading.
US998862A (en) Securing means for turbine-blades.
US1590328A (en) Fastening means for turbine blading
US913273A (en) Blade for turbines.
US1705585A (en) Turbine-blade fastening
US1187445A (en) Steam-turbine.
US1187451A (en) Steam-turbine.
US1245810A (en) Tying means for turbine-blades.
US1468694A (en) Flexible and insulating, supporting, and reenforcing rings for crown blades of turbins
US1010630A (en) Blade-holding means for turbines.
US2315610A (en) Turbine blade shroud fastening
US791744A (en) Elastic-fluid turbine.
US791735A (en) Elastic-fluid turbine.
US1109998A (en) Turbine-rotor.
US953526A (en) Elastic-fluid turbine.