GB628263A - Improvements in or relating to axial flow compressors - Google Patents
Improvements in or relating to axial flow compressorsInfo
- Publication number
- GB628263A GB628263A GB25559/46A GB2555946A GB628263A GB 628263 A GB628263 A GB 628263A GB 25559/46 A GB25559/46 A GB 25559/46A GB 2555946 A GB2555946 A GB 2555946A GB 628263 A GB628263 A GB 628263A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- fluid
- rows
- groups
- flow
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
- F04D29/544—Blade shapes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
628,263. Axial-flow compressors. BREGUET, L. Aug. 27, 1946, No. 25559. Convention date, June 1, 1943. [Class 110(i)] An axial-flow compressor comprises a stator and a rotor co-axially mounted with respect to each other and each is provided with circumferential rows of blades the rows being arranged in groups, each group consisting of a plurality of rows, groups of fixed and moving blades occurring alternately along the length of the compres. sor. The profile of each group of moving blades 3, 4, 5 is substantially a mirror image of the profile of the adjacent groups of fixed blades 3<1>, 4<1>, 5<1>, and the blades are curved and set to provide restricted inlets for the fluid, so that the passage allowed to the fluid between two successive blades in the same row offers, in a plane at right angles to the middle line of the passage, a section which increases in the direction of flow of the fluid. An intermediate blade 8 may also be included between the blades 4.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR628263X | 1943-06-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB628263A true GB628263A (en) | 1949-08-25 |
Family
ID=8989534
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25559/46A Expired GB628263A (en) | 1943-06-01 | 1946-08-27 | Improvements in or relating to axial flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB628263A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1031132B (en) * | 1955-07-18 | 1958-05-29 | Eta Corp G M B H | Centrifugal machine, especially centrifugal pump for dripping media |
US2841325A (en) * | 1954-05-04 | 1958-07-01 | Snecma | Axial compressors |
DE977016C (en) * | 1951-04-01 | 1964-11-05 | Eta Corp G M B H | Centrifugally acting centrifugal pump impeller with blades bounded by impeller walls or by stationary walls and a throat-like narrowing in the blade channel |
US3173604A (en) * | 1962-02-15 | 1965-03-16 | Gen Dynamics Corp | Mixed flow turbo machine |
WO1982003430A1 (en) * | 1981-03-27 | 1982-10-14 | Vartiala Heikki | Propeller |
FR2650338A1 (en) * | 1989-07-27 | 1991-02-01 | Mtu Muenchen Gmbh | ROTOR, ESPECIALLY FOR COMPRESSORS OR TURBINES OF GAS TURBINE DRIVE UNITS |
EP2092163A1 (en) * | 2006-11-14 | 2009-08-26 | Volvo Aero Corporation | Vane assembly configured for turning a flow ina a gas turbine engine, a stator component comprising the vane assembly, a gas turbine and an aircraft jet engine |
CH704212A1 (en) * | 2010-12-15 | 2012-06-15 | Alstom Technology Ltd | Axial Compressor. |
EP2474744A1 (en) * | 2011-01-11 | 2012-07-11 | Siemens Aktiengesellschaft | Annular flow channel for an axial compressor |
EP2256299A3 (en) * | 2009-04-24 | 2014-04-09 | Pratt & Whitney Canada Corp. | Deflector for a gas turbine strut and vane assembly |
DE102014203603A1 (en) * | 2014-02-27 | 2015-08-27 | Rolls-Royce Deutschland Ltd & Co Kg | Blade row group |
RU2586426C2 (en) * | 2013-05-03 | 2016-06-10 | Текспейс Аеро С.А. | Stator of axial turbo machine with ailerons in blade roots |
EP3425164A1 (en) * | 2017-07-06 | 2019-01-09 | United Technologies Corporation | Tandem rotor disk apparatuses and corresponding gas turbine engine |
-
1946
- 1946-08-27 GB GB25559/46A patent/GB628263A/en not_active Expired
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE977016C (en) * | 1951-04-01 | 1964-11-05 | Eta Corp G M B H | Centrifugally acting centrifugal pump impeller with blades bounded by impeller walls or by stationary walls and a throat-like narrowing in the blade channel |
US2841325A (en) * | 1954-05-04 | 1958-07-01 | Snecma | Axial compressors |
DE1031132B (en) * | 1955-07-18 | 1958-05-29 | Eta Corp G M B H | Centrifugal machine, especially centrifugal pump for dripping media |
US3173604A (en) * | 1962-02-15 | 1965-03-16 | Gen Dynamics Corp | Mixed flow turbo machine |
WO1982003430A1 (en) * | 1981-03-27 | 1982-10-14 | Vartiala Heikki | Propeller |
FR2650338A1 (en) * | 1989-07-27 | 1991-02-01 | Mtu Muenchen Gmbh | ROTOR, ESPECIALLY FOR COMPRESSORS OR TURBINES OF GAS TURBINE DRIVE UNITS |
EP2092163A4 (en) * | 2006-11-14 | 2013-04-17 | Volvo Aero Corp | Vane assembly configured for turning a flow ina a gas turbine engine, a stator component comprising the vane assembly, a gas turbine and an aircraft jet engine |
EP2092163A1 (en) * | 2006-11-14 | 2009-08-26 | Volvo Aero Corporation | Vane assembly configured for turning a flow ina a gas turbine engine, a stator component comprising the vane assembly, a gas turbine and an aircraft jet engine |
EP2256299A3 (en) * | 2009-04-24 | 2014-04-09 | Pratt & Whitney Canada Corp. | Deflector for a gas turbine strut and vane assembly |
CN103354875A (en) * | 2010-12-15 | 2013-10-16 | 阿尔斯通技术有限公司 | Axial compressor |
CN103354875B (en) * | 2010-12-15 | 2016-08-24 | 通用电器技术有限公司 | Axial compressor |
US9810226B2 (en) | 2010-12-15 | 2017-11-07 | Ansaldo Energia Ip Uk Limited | Axial compressor |
WO2012080053A1 (en) * | 2010-12-15 | 2012-06-21 | Alstom Technology Ltd | Axial compressor |
CH704212A1 (en) * | 2010-12-15 | 2012-06-15 | Alstom Technology Ltd | Axial Compressor. |
AU2011344469B2 (en) * | 2010-12-15 | 2015-06-25 | Ansaldo Energia Ip Uk Limited | Axial compressor |
RU2564386C2 (en) * | 2010-12-15 | 2015-09-27 | Альстом Текнолоджи Лтд | Axial compressor |
WO2012095220A1 (en) * | 2011-01-11 | 2012-07-19 | Siemens Aktiengesellschaft | Annular flow duct for an axial flow compressor |
EP2474744A1 (en) * | 2011-01-11 | 2012-07-11 | Siemens Aktiengesellschaft | Annular flow channel for an axial compressor |
RU2586426C2 (en) * | 2013-05-03 | 2016-06-10 | Текспейс Аеро С.А. | Stator of axial turbo machine with ailerons in blade roots |
DE102014203603A1 (en) * | 2014-02-27 | 2015-08-27 | Rolls-Royce Deutschland Ltd & Co Kg | Blade row group |
US10030521B2 (en) | 2014-02-27 | 2018-07-24 | Rolls-Royce Deutschland Ltd & Co Kg | Group of blade rows |
EP3425164A1 (en) * | 2017-07-06 | 2019-01-09 | United Technologies Corporation | Tandem rotor disk apparatuses and corresponding gas turbine engine |
US11136991B2 (en) | 2017-07-06 | 2021-10-05 | Raytheon Technologies Corporation | Tandem blade rotor disk |
EP3957824A1 (en) * | 2017-07-06 | 2022-02-23 | Raytheon Technologies Corporation | Tandem rotor disk apparatuses and corresponding gas turbine engine |
US11549518B2 (en) | 2017-07-06 | 2023-01-10 | Raytheon Technologies Corporation | Tandem blade rotor disk |
US12049904B2 (en) | 2017-07-06 | 2024-07-30 | Rtx Corporation | Tandem blade rotor disk |
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