EP0280205B1 - Compresseur radial - Google Patents
Compresseur radial Download PDFInfo
- Publication number
- EP0280205B1 EP0280205B1 EP88102419A EP88102419A EP0280205B1 EP 0280205 B1 EP0280205 B1 EP 0280205B1 EP 88102419 A EP88102419 A EP 88102419A EP 88102419 A EP88102419 A EP 88102419A EP 0280205 B1 EP0280205 B1 EP 0280205B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- diffuser
- slots
- radial
- blades
- radial compressor
- 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
- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
- F04D29/444—Bladed diffusers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D21/00—Pump involving supersonic speed of pumped fluids
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
Definitions
- the invention relates to a radial compressor according to the preamble of claim 1.
- the object of the invention is to stabilize the compression surges occurring in certain operating areas on the flow inlet side of the radial guide vane ring and to reduce their effects on the characteristic diagram.
- the blades of the radial guide vane ring alternately have two different lengths and the slots are arranged at least approximately at right angles in front of the short blades and extend to the side next to the front edge of the blade of the nearest long blades. It is generally known that a radial guide vane ring inserted into the diffuser of a radial compressor has an effect on the surge limit of the radial compressor. It has proven advantageous to manufacture the blades of the radial guide vane ring alternately with two different lengths in the case of highly loaded radial compressors.
- a compression shock occurs at least on the leading edge of the short stator vanes.
- the lossy back and forth movement of the compression shock, caused by transient outflow from the impeller, is reduced or avoided by the configuration according to the invention.
- the slots arranged at least approximately at right angles to the blades (and accordingly also approximately at right angles to the flow) connect the diffuser to at least one storage space arranged behind the diffuser channel wall.
- the slots are advantageously incorporated into both opposite diffuser channel walls and correspondingly connected to annular storage spaces arranged on both sides of the diffuser channel walls.
- the two annular storage spaces are combined to form a coherent annular space.
- the two storage spaces are subdivided into individual segments which are partitioned off from one another, a segment being assigned to each slot.
- This special design of the storage rooms depends on the Design of the respective radial compressor.
- the inventive design and arrangement of the slots and the storage spaces behind them keep the radial compressor in a stable working area because the map width of the radial compressor increases due to the partial reduction of the compression surges.
- the impeller 1 of a radial compressor shown in part, is fastened on a shaft designated by the center line 2.
- the impeller 1 conveys the air flow 3 entering the radial compressor into a diffuser 4, which is composed of an unbladed diffuser 4a and a bladed diffuser 4b.
- a diffuser 4 which is composed of an unbladed diffuser 4a and a bladed diffuser 4b.
- the Diffuser channel walls 5, 6 are incorporated into slots 7a, 7b, which connect the diffuser channel 4 to storage spaces 8, 9 arranged on both sides of the diffuser channel wall 5, 6 and surrounding the diffuser channel 4 in a ring shape.
- Fig. 2 it can be seen that the blades 9, 10 of the radial guide vane ring 11 are alternately different lengths (short blade 9; long blade 10). Slits 7a are arranged almost at right angles to the leading edge of the blade in front of the short blades 9 and extend laterally next to the leading edge 10a of the blade.
- the map shown in FIG. 3 (solid lines) is that of a conventional radial compressor in the event of a faulty flow to the radial compressor and thus to the radial guide vane ring 11, i.e. without specially arranged slots 7a, 7b and without storage spaces 8a, 8b arranged behind it.
- a characteristic field expansion is achieved, the size of which is defined by the proportion b1 (dashed line delimitation of the characteristic field).
- a similar characteristic curve field is shown in FIG. 4, with an undisturbed inflow being assumed in this characteristic field.
- a characteristic extension by the dimension b2 can be achieved by applying the invention.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Claims (1)
- Compresseur radial avec un diffuseur (4, 4a,4b) intercalé après la roue mobile (1), des lumières (7a, 7b) étant usinées dans au moins une paroi du canal du diffuseur (5, 6), lumières qui relient le diffuseur (4, 4a, 4b) à au moins un espace de réserve (8a, 8b) placé derrière la paroi du canal de diffuseur (5, 6), le diffuseur (4) étant associé à une couronne d'aubes directrices radiales (11) et les lumières (7a, 7b) étant disposées du côté de l'entrée du flux de la couronne d'aubes directrices radiales, caractérisé en ce que les aubes (9, 10) de la couronne d'aubes directrices radiales (11) comportent alternativement deux longueurs différentes et les lumières (7a, 7b) sont placées au moins approximativement à angle droit devant les aubes courtes (9) et s'étendent latéralement près des arêtes avant (10a) d'une aube longue au moins contigu.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19873705307 DE3705307A1 (de) | 1987-02-19 | 1987-02-19 | Radialverdichter |
DE3705307 | 1987-02-19 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0280205A2 EP0280205A2 (fr) | 1988-08-31 |
EP0280205A3 EP0280205A3 (en) | 1989-08-02 |
EP0280205B1 true EP0280205B1 (fr) | 1991-05-08 |
Family
ID=6321337
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP88102419A Expired - Lifetime EP0280205B1 (fr) | 1987-02-19 | 1988-02-19 | Compresseur radial |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0280205B1 (fr) |
DE (2) | DE3705307A1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19814627C2 (de) * | 1998-04-01 | 2001-02-22 | Man Turbomasch Ag Ghh Borsig | Kühlluftentnahme aus dem Diffusorteil eines Kompressors einer Gasturbine |
DE19817705C2 (de) * | 1998-04-21 | 2001-02-15 | Man Turbomasch Ag Ghh Borsig | Kühlluftentnahme aus dem Diffusorteil eines Kompressors einer Gasturbine |
EP1710442A1 (fr) * | 2005-04-04 | 2006-10-11 | ABB Turbo Systems AG | Système de stabilisation de courant pour compresseur radial |
DE102008044505B4 (de) | 2008-09-08 | 2010-07-01 | Friedrich-Alexander-Universität Erlangen-Nürnberg | Radialverdichter |
CN102506029B (zh) * | 2011-12-29 | 2014-04-16 | 中联重科股份有限公司 | 一种离心风机叶轮及离心风机 |
US20130280060A1 (en) * | 2012-04-23 | 2013-10-24 | Shakeel Nasir | Compressor diffuser having vanes with variable cross-sections |
DE102016201256A1 (de) * | 2016-01-28 | 2017-08-03 | Siemens Aktiengesellschaft | Strömungsmaschine mit beschaufeltem Diffusor |
DE102017203230A1 (de) | 2017-02-28 | 2018-08-30 | Siemens Aktiengesellschaft | Diffusor |
JP2020510783A (ja) * | 2017-03-03 | 2020-04-09 | エリオット・カンパニー | キャビティ音響モードによる騒音及び構造の励振を最低限に抑える方法及び構成 |
IT202000001216A1 (it) * | 2020-01-22 | 2021-07-22 | Nuovo Pignone Tecnologie Srl | Un diffusore con passo delle pale di diffusore non costante e turbomacchina centrifuga comprendente detto diffusore |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE916604C (de) * | 1942-09-12 | 1954-08-12 | Daimler Benz Ag | Leitschaufelkranz fuer Fliehkraftgeblaese |
US4131389A (en) * | 1975-11-28 | 1978-12-26 | The Garrett Corporation | Centrifugal compressor with improved range |
US4368005A (en) * | 1977-05-09 | 1983-01-11 | Avco Corporation | Rotary compressors |
GB2013280B (en) * | 1978-01-25 | 1983-02-23 | Secr Defence | Diffusers for centrifugl compressors |
FR2487018A1 (fr) * | 1980-07-16 | 1982-01-22 | Onera (Off Nat Aerospatiale) | Perfectionnements aux compresseurs supersoniques |
-
1987
- 1987-02-19 DE DE19873705307 patent/DE3705307A1/de not_active Withdrawn
-
1988
- 1988-02-19 EP EP88102419A patent/EP0280205B1/fr not_active Expired - Lifetime
- 1988-02-19 DE DE8888102419T patent/DE3862650D1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0280205A2 (fr) | 1988-08-31 |
DE3705307A1 (de) | 1988-09-01 |
EP0280205A3 (en) | 1989-08-02 |
DE3862650D1 (de) | 1991-06-13 |
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