GB918674A - Improvements relating to the construction of gas turbine engines - Google Patents
Improvements relating to the construction of gas turbine enginesInfo
- Publication number
- GB918674A GB918674A GB1357660A GB1357660A GB918674A GB 918674 A GB918674 A GB 918674A GB 1357660 A GB1357660 A GB 1357660A GB 1357660 A GB1357660 A GB 1357660A GB 918674 A GB918674 A GB 918674A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vanes
- rotor
- disc
- construction
- april
- 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
Links
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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
918,674. Making turbines. GARRINGTONS Ltd. April 19, 1961 [April 19, 1960], No. 13576/60. Addition to 848,562. Class 83 (2). [Also in Group XXVI] The invention as set forth in Claim 1 of the parent Specification is modified in that the blind holes 12 are drilled from the smaller diameter end of the rotor and the slots 15 are formed so that they extend in the axial direction up to the transverse plane passing through the ends of the blind holes so as to leave a complete disc 14 at the larger diameter end of the rotor, the disc forming an abutment for the edges of the vanes 16 at this end. The smaller end of the rotor is provided with a detachable cap member 19 which provides a locating abutment for the vanes at this end. The edges of the vanes which are disposed adjacent the disc 14 are formed with projections 18 which upon assembly extend through holes 23 in the disc, the ends of the projections being subsequently riveted over to retain the vanes in position. The cap member 19 is secured to the rotor by means of a bolt 22.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1357660A GB918674A (en) | 1960-04-19 | 1960-04-19 | Improvements relating to the construction of gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1357660A GB918674A (en) | 1960-04-19 | 1960-04-19 | Improvements relating to the construction of gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB918674A true GB918674A (en) | 1963-02-13 |
Family
ID=10025472
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1357660A Expired GB918674A (en) | 1960-04-19 | 1960-04-19 | Improvements relating to the construction of gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB918674A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2361528A1 (en) * | 1976-08-11 | 1978-03-10 | Mowill Jan | RADIAL INLET GAS TURBINE ROTOR WHEEL |
US4419052A (en) * | 1980-02-07 | 1983-12-06 | Rockwell International Corporation | Turbine meter rotor |
GB2251028A (en) * | 1990-12-21 | 1992-06-24 | Black & Decker Inc | Cooling electric motor with a radial-flow fan |
-
1960
- 1960-04-19 GB GB1357660A patent/GB918674A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2361528A1 (en) * | 1976-08-11 | 1978-03-10 | Mowill Jan | RADIAL INLET GAS TURBINE ROTOR WHEEL |
US4188169A (en) * | 1976-08-11 | 1980-02-12 | Jan Mowill | Impeller element or radial inflow gas turbine wheel |
US4419052A (en) * | 1980-02-07 | 1983-12-06 | Rockwell International Corporation | Turbine meter rotor |
GB2251028A (en) * | 1990-12-21 | 1992-06-24 | Black & Decker Inc | Cooling electric motor with a radial-flow fan |
GB2251028B (en) * | 1990-12-21 | 1994-08-24 | Black & Decker Inc | Electric motor with a cooling fan |
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