US1141938A - Air-regulating device for centrifugal compressors. - Google Patents
Air-regulating device for centrifugal compressors. Download PDFInfo
- Publication number
- US1141938A US1141938A US74261413A US1913742614A US1141938A US 1141938 A US1141938 A US 1141938A US 74261413 A US74261413 A US 74261413A US 1913742614 A US1913742614 A US 1913742614A US 1141938 A US1141938 A US 1141938A
- Authority
- US
- United States
- Prior art keywords
- impeller
- air
- vanes
- discharge
- regulating device
- 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
- 239000012530 fluid Substances 0.000 description 10
- 230000001105 regulatory effect Effects 0.000 description 7
- 230000015556 catabolic process Effects 0.000 description 4
- 238000005192 partition Methods 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 241000370685 Arge Species 0.000 description 1
- 208000036366 Sensation of pressure Diseases 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- QEVHRUUCFGRFIF-MDEJGZGSSA-N reserpine Chemical compound O([C@H]1[C@@H]([C@H]([C@H]2C[C@@H]3C4=C(C5=CC=C(OC)C=C5N4)CCN3C[C@H]2C1)C(=O)OC)OC)C(=O)C1=CC(OC)=C(OC)C(OC)=C1 QEVHRUUCFGRFIF-MDEJGZGSSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 235000014101 wine Nutrition 0.000 description 1
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
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/105—Centrifugal pumps for compressing or evacuating with double suction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
-
- 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
- F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/462—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/52—Outlet
Definitions
- Patented .l une 8, 1915 Patented .l une 8, 1915.
- PatentedJune 8, 1915
- This invention relates to centrifugal machines for compressing air, and its object is to retard or prevent the breakdown which is liable to occur when a critical point is reached in the ratio between the speed of the machine and the volume of air delivered. If this critical point is passed, surging of the air column and violent pulsations in pres sure are liable to be set up, which endanger the machine and interfere with its usefulness.
- Each speed has its own breakdown point, and so long as the volume'of air delivered remains on the safe side of the curve thus established, no trouble will be ,experienced. But when the machine is running at a constant number of revolutions per minute, the lessening of the volume delivered means also that the velocity of the air column is lessened.
- the casing 1 has an intake 2 and an out- If the velocity can be let 3.
- Mounted on the shaft 4 are two impellers 5 and 6, each ot which is double, that is to say, it has driving blades on each side of a central web 7.
- the air entering through the intake is admitted to the housing 8 of each impeller through ports 9 adjacent to the hub.
- On one side of each impeller these ports are controlled by a rotary valve 10, having ports 11 to register with the ports 9, and intermediate solid portions 12 to close said ports 9 when the valve is turned.
- each impeller is-divided into two compartments by a partition 13, lying in the same plane as the web of the impeller and making a close running fit with its peri hery.
- a set of main discharge vanes 14 of theusual shape and arrangement.
- I provide in each channel an auxiliary vane 15 mounted on a shaft 16 which extends through the housing of the impeller and is provided on one or both 4 ends with a lever arm 17.
- each lever carries a segment gear 18 mes ing with a spur gear 19 formed integral with one of the valves 10.
- a rod 20 pivoted to one of the levers enables the valves and all the auxiliary vanes to be adjusted at the same time;
- the rod 20 can be actuated by hand, or automatically by a speed governor (not shown),
- the object of this is to balance the end thrust when the valves are partially or wholly closed, due to the router quantity of fluid entering one side 0 the impeller than the other.
- valves 10 and the auxiliary vanes 15 in the same machine; but it is evident that one or the other device may beomitted; or, if desired, the. valve" 10 may be used on one side of an im-.
- a casing having an inlet opening and an outlet opening, ar shaft, a p nrality of double inlet impellers mounted on said shaft,1and a valve associated with each impeller to control the admission of fluid to one side thereof, said valves being arranged on opposite sides of adjacent im pellers whereby the end thrust is balanced;
- a 3 The combination with a centrifugal air compressor having a double inlet impeller,
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Description
C. P. CRISSEY.
AIR REGULATING DEVICE FOR CENTRIFUGAL COMPRESSORS.
APPLICATION FILED JAN. I7. 1913.
Patented .l une 8, 1915.
2 SHEETS-SHEET I.
Inventor, F2 Crisseg,
Witnesses Clarence C. P. CRISSEY. AIR REGULATING ounce FOR CENTRIFUGAL COMPRESSORS.
APPLICATION FILED JAN-17,1913.
2 SHEETSSHEET 2.
Inventor;
aa lzzr.
illa Witnesses CLARENCE P. OBISSEY, OF EAST ORANGE, NEW JERSEY, ESSIGNOR TO GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
AIR-REGULATING DEVICE FOR CENTBI'FUGAL COMPBESSORS I Specification of Letters Patent.
Patented June 8, 1915.
Application filed January 17, 19 18. v Serial No. 742,614.
To all whom it may concern:
Be it known that I, CLARENCE P. Cmssnr, a citizen of the United States, residin at East Orange, in the county of Essex, tate of New Jersey, have invented certain new and useful Improvements in Air-Regulating Devices for Centrifugal Compressors, of which the following is a specification.
This invention relates to centrifugal machines for compressing air, and its object is to retard or prevent the breakdown which is liable to occur when a critical point is reached in the ratio between the speed of the machine and the volume of air delivered. If this critical point is passed, surging of the air column and violent pulsations in pres sure are liable to be set up, which endanger the machine and interfere with its usefulness. Each speed has its own breakdown point, and so long as the volume'of air delivered remains on the safe side of the curve thus established, no trouble will be ,experienced. But when the machine is running at a constant number of revolutions per minute, the lessening of the volume delivered means also that the velocity of the air column is lessened. maintained in spite of the lessened volume, the danger of a breakdown is greatly reduced. My invention, therefore, concerns a particular construction of the compressor by which the velocity diagram can be kept approximately correct even at light loads and thus a correct functioning of the fluid will be secured. I accomplish this by making the impeller, or each impeller, if more than one is used, capable of taking ail-"from both sides; controlling by a suitable valve the air admitted to one side; dividing the discharge chamber by a partition in line with the impeller, so that each halfof the impeller will deliver its air to its own setof discharge vanes, and providing, if desired, auxiliary vanes to regulate the delivery of the fluid. The special construction of these parts and the particular functions of each Wlll appear from. the following detailed description, reference being had to the accompanying drawings, in which- 7 Figure 1 is an end elevation of a centrifugal air compressor partly broken away to show some of the mechanism embodying my invention, and Fig. 2 is a longitudinal section of the same machine.
The casing 1 has an intake 2 and an out- If the velocity can be let 3. Mounted on the shaft 4 are two impellers 5 and 6, each ot which is double, that is to say, it has driving blades on each side of a central web 7. The air entering through the intake is admitted to the housing 8 of each impeller through ports 9 adjacent to the hub. On one side of each impeller, these ports are controlled by a rotary valve 10, having ports 11 to register with the ports 9, and intermediate solid portions 12 to close said ports 9 when the valve is turned. By suitably adjusting the position of this valve, the amount of air admitted to that-side of the impeller can be accurately regulated,
The discharge chamber surrounding each impeller is-divided into two compartments by a partition 13, lying in the same plane as the web of the impeller and making a close running fit with its peri hery. In each of the compartments thus ormed is a set of main discharge vanes 14 of theusual shape and arrangement. In crder to cdntrol the effective area of the discharge channels between the vanes, I provide in each channel an auxiliary vane 15 mounted on a shaft 16 which extends through the housing of the impeller and is provided on one or both 4 ends with a lever arm 17. Inasmuch as it is desirable to adjust all these auxiliary vanes simultaneously and to the same degree, each lever carries a segment gear 18 mes ing with a spur gear 19 formed integral with one of the valves 10. A rod 20 pivoted to one of the levers enables the valves and all the auxiliary vanes to be adjusted at the same time;
the vanes being gradually closed when the I ports 9 are gradually closed, and vice versa. The rod 20 can be actuated by hand, or automatically by a speed governor (not shown),
as may be desired.
It will be observed that the two valves 10. are on opposite sides of the two impellers.
.The object of this is to balance the end thrust when the valves are partially or wholly closed, due to the router quantity of fluid entering one side 0 the impeller than the other.
In the operation of this compressor, as the quantity at which breakdown occurs is approached, both sides of the impellers being open to the fluid, the governor or other means will cause the valves 10 to close. The velocity of the fluid passin into the active side of the impellers will, t erefore, be such as to form a velocity diagram which is more nearly correct and thus rea-kdown will not take place until the quantity is again greatly reduced. This latter quantity can be made so small a ercenta e of the rated capacity of the machme' that reakdown is eliminated to all intents. and purposes, because outside of the range of operating conditions. When the valves 10 are closed, there is a tendency for the fluid discharged from the active side of the impeller "to flow into the discharge compartment of the other side. This is prevented, or at least greatly limited,-by the small clearance between the partition and the periphery of the impeller web.
I deem it better to use both the valves 10 and the auxiliary vanes 15 in the same machine; but it is evident that one or the other device may beomitted; or, if desired, the. valve" 10 may be used on one side of an im-.
vanes on the other ciple of operation of my invention, together with the apparatus which now consider to represent the-best embodiment thereof;.but
" I desire to have it understood that the apparatus shown is only illustrative, and that the invention can be carried out by other means.
- What I claim as new, and desire to secure Y by Letters Patent of the United States, is
1. In a --centrifugal air compressor, the combination iof. ,a casing having an inlet opening and an outlet opening, ar shaft, a p nrality of double inlet impellers mounted on said shaft,1and a valve associated with each impeller to control the admission of fluid to one side thereof, said valves being arranged on opposite sides of adjacent im pellers whereby the end thrust is balanced;
2. The combination with a centrifugal air compressor having a double inlet impeller,
of a discharge chamber provided with a partition-in line with the web of said impeller, discharge vanes in each compartment of said chamber, and means located between thefldischarge vanes and operable to change the contour of the channels there- 66 between for controlling the effective area of I i suchdischarge channels. A 3. The combination with a centrifugal air compressor having a double inlet impeller,
of a discharge chamber provided with a' partition in :line with the web of said im-' peller, maindischarge vanesin each compartment of said chamber, and auxiliary. vanesv for controlling the effective area of the discharge channels between the'main vanes. I
4. The combination with a centrifugal air compressor having a double inlet im eller I and walls forming stationary disc arge channels at the periphery thereof, of means for regulating the admission of fluid to one side of s id impeller, and means for regulating the effective area/of the discharge channels,
5. The combination with. a centrifugal air compressor having a double inlet impeller of meansfor regulating the admission 0 fluid to one sideof said impeller, means for regulating the effective area of the discharge channels, and means for eflect i ng said regulations simultaneously. v
6. In a centrifugal air compressor, the" combination of an impeller, stationary discharge vanes surrounding it and definingpassages for directing the fluid discharged from the periphery of the impeller, and auxiliary discharge vanes carried by the first named vanes, and adapted to be adjusted to vary the' efiective area of said passages.
7. In a eentrifu al air. compressor, that!) combination of an impeller, stationary discharge vanes surrounding it and defining passages for directing the find discharged from the periphery of the impeller, auxiliary, discharge vanes carried by the first named wines, and means for simultaneously adjusting them to vary the eflective area of said passages. v In witness whereof, I have hereunto set my hand 13th'dav of Januarly, 1913. im Y CLAB NCE P. CR SSEY.
'Witnesses':
R. T.-Fnoer, H. V. ALLEN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US74261413A US1141938A (en) | 1913-01-17 | 1913-01-17 | Air-regulating device for centrifugal compressors. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US74261413A US1141938A (en) | 1913-01-17 | 1913-01-17 | Air-regulating device for centrifugal compressors. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1141938A true US1141938A (en) | 1915-06-08 |
Family
ID=3210034
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US74261413A Expired - Lifetime US1141938A (en) | 1913-01-17 | 1913-01-17 | Air-regulating device for centrifugal compressors. |
Country Status (1)
Country | Link |
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US (1) | US1141938A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2648195A (en) * | 1945-12-28 | 1953-08-11 | Rolls Royce | Centrifugal compressor for supercharging internal-combustion engines |
DE1094915B (en) * | 1959-02-25 | 1960-12-15 | Bbc Brown Boveri & Cie | Control device for turbo machines |
US3009319A (en) * | 1955-06-29 | 1961-11-21 | Gregory D Filipenco | Turbojet engine |
-
1913
- 1913-01-17 US US74261413A patent/US1141938A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2648195A (en) * | 1945-12-28 | 1953-08-11 | Rolls Royce | Centrifugal compressor for supercharging internal-combustion engines |
US3009319A (en) * | 1955-06-29 | 1961-11-21 | Gregory D Filipenco | Turbojet engine |
DE1094915B (en) * | 1959-02-25 | 1960-12-15 | Bbc Brown Boveri & Cie | Control device for turbo machines |
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