US2317723A - Air blower - Google Patents
Air blower Download PDFInfo
- Publication number
- US2317723A US2317723A US315665A US31566540A US2317723A US 2317723 A US2317723 A US 2317723A US 315665 A US315665 A US 315665A US 31566540 A US31566540 A US 31566540A US 2317723 A US2317723 A US 2317723A
- Authority
- US
- United States
- Prior art keywords
- blower
- engine
- turbo
- air
- valve
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
- F02D2700/02—Controlling by changing the air or fuel supply
- F02D2700/0217—Controlling by changing the air or fuel supply for mixture compressing engines using liquid fuel
- F02D2700/0225—Control of air or mixture supply
- F02D2700/0246—Control of air or mixture supply for engines with compressor
- F02D2700/0258—Control of air or mixture supply for engines with compressor by other means
Definitions
- Another object of this invention is to provide an improved turbo-blower having an adjustable short circuit between its suction and delivery sides.
- An additional object of this invention lies in the provision of a;turbo-blower for delivering charging air to an internal combustion engine, such blower having a larger capacity than needed by said engine and being provided with a continuous but variable by-pass between its suction and delivery sides, the amount of by-pass depending upon the relative capacities of the turbo-blower and the engine.
- This invention accordingly consists in the features of construction, combination of parts, and in the unique relation of the members and in the relative proportioning and disposition thereof, all as more completely outlined herein.
- Fig. 1 illustrates a side view of an internal combustion engine in combination with a turboblcwer designed in accordance with the relation ships of this invention
- Fig. 2 is a partial longitudinal cross-sectional view, drawn to an enlarged scale, of the turboblower illustrated in Fig. l.
- an internal combustion cngine which in this case may be a Diesel engine, is indicated by the reference, numeral I, and through suitable gears 2 and 3 is drivably conncctcd with the turbo-blower wheel 4.
- the latter upon being driven by the engine I, sucks in air through a suitable centrally located inlet opening and discharges it preferably through guiding vanes such as illustrated at 5 in Fig. 2. into the hollow spiral housing 6. from whence it is guided back to the engine I through the conduit 1.
- the turbo-blower is designed to have a capacity greater than is necessary for supplying the air to the internal combustion engine I, the turbo-blower is accordingly also provided with an outlet 8 on its discharge side, which r e sults in a short-circuit or by-pass between the suction and delivery, and indicated in Fig. 1 by the reference character N.
- an open-' Cal ing 9 is provided in the casing 6 immediately adjacent the outlet from the turbine wheel 4, and intermediate the periphery of the turbine Wheel and the air-guide vanes 5.
- a conical seat ID is formed at the outside of the opening 9, with which a conically shaped valve H is adapted to cooperate for controlling the size of the'outlet.
- the position of the valve l I is preferably adjusted as desired by means of a threaded valve rod l2 which can be screwed in and out of the attached housing l3.
- A-nut M will hold the valve i l in place in the desired position.
- turbo-blower which is obviously adaptable to internal combustion engines of varied requirements. If the turbo-blower has a much greater capacity than necessary for the engine, the valve 1 I will be open to a comparably large extent. If,- however, the turbo-blower has a capacity only slightly in excess of that needed by the engine, the valve II will be almost closed. It has long been known that the capacity of a centrifugal blower must closely approximate the requirements of the engine supercharge, for otherwise deleterious and unsafe conditions in the air-charging system, such as hammering will arise. By means of the present invention, however, a single turbo-blower can be used with internal combustion engines of a wide capacity range. For example, a turboblower which has been designed for an engine having a compression space of 1.5 liters can, b; proper adjustment of the short circuit, be made usable for an engine of only '1 liter compression space.
- While the invention has been described in connection with an internal combustion engine of .the Diesel type, it is also equally applicable to engines using a carbureter. If the carbureter is to be positioned on the p ressure side of the blower, this can be done in the usual manner. If the carbureter is to be positioned on the suction side of the blower, the mouth upon the suction side of the short circuit will be displaced along the entrance to the turbine wheel in such a manner as to exclude losses in fuel.
- control means for varying the amount of short circuit between the suction and delivery sides of the blower has been disclosed, it will also be clear to those skilled in this art that the other type of throttling means such as butterfly valves, slide valves and the like are contemplated.
- a turbo-blower comprising, in combination, a turbine wheel, a casing surrounding said wheel having a centrally located inlet opening, a substantially tangential discharge opening, and a 3.
- a turbo-blower comprising, in combination,-
- a casing having a centrally located inlet opening, a substantially tangential discharge openingand a by-pass opening, a turbine wheel centrally mounted for rotation within said casing, and airguide vanes for leading the air from said turbine wheel to said discharge opening, said by-pass opening being positioned in said casing intermediate the periphery of said turbine wheel and said air-guide vanes, and means for throttling said by-pass opening.
Description
April 7, 1943. w. BECHT AIR BLOWER Filed Jan. 26, 1940 In ventor Attorneys Patented Apr. 27, 1 943 UNITED STATES PATENT oFFlca 2,317,723 AIR BLOWER Walter Becht, Stuttgart-Bad Cannstatt, Ger many; vested in the Alien Property Custodian Application January 26, 1940, Serial No. 315,665 In Germany February 4, 1939 Claims.
bustion engines of a large range in size.
Another object of this invention is to provide an improved turbo-blower having an adjustable short circuit between its suction and delivery sides.
An additional object of this invention lies in the provision of a;turbo-blower for delivering charging air to an internal combustion engine, such blower having a larger capacity than needed by said engine and being provided with a continuous but variable by-pass between its suction and delivery sides, the amount of by-pass depending upon the relative capacities of the turbo-blower and the engine.
Other objedts will be in part obvious from the annexed drawing, and in part indicated in con' nection therewith by the following analysis of this invention.
This invention accordingly consists in the features of construction, combination of parts, and in the unique relation of the members and in the relative proportioning and disposition thereof, all as more completely outlined herein.
To enable others skilled in the art so fully to comprehend the underlying features thereof that they may embody the same by the numerous modifications in structure and relations contemplated by this invention, a drawing depicting a preferred form has been annexed as a part of this disclosure, and in such drawing:
Fig. 1 illustrates a side view of an internal combustion engine in combination with a turboblcwer designed in accordance with the relation ships of this invention; and
Fig. 2 is a partial longitudinal cross-sectional view, drawn to an enlarged scale, of the turboblower illustrated in Fig. l.
As shown in Fig. 1, an internal combustion cngine, which in this case may be a Diesel engine, is indicated by the reference, numeral I, and through suitable gears 2 and 3 is drivably conncctcd with the turbo-blower wheel 4. The latter, upon being driven by the engine I, sucks in air through a suitable centrally located inlet opening and discharges it preferably through guiding vanes such as illustrated at 5 in Fig. 2. into the hollow spiral housing 6. from whence it is guided back to the engine I through the conduit 1. Since, in accordance with the teachings of this invention, the turbo-blower is designed to have a capacity greater than is necessary for supplying the air to the internal combustion engine I, the turbo-blower is accordingly also provided with an outlet 8 on its discharge side, which r e sults in a short-circuit or by-pass between the suction and delivery, and indicated in Fig. 1 by the reference character N.
- vided an arrangement which is more fully illustrated in Fig. 2. As can be there seen, an open-' Cal ing 9 is provided in the casing 6 immediately adjacent the outlet from the turbine wheel 4, and intermediate the periphery of the turbine Wheel and the air-guide vanes 5. At the outside of the opening 9, is formed a conical seat ID with which a conically shaped valve H is adapted to cooperate for controlling the size of the'outlet. The position of the valve l I is preferably adjusted as desired by means of a threaded valve rod l2 which can be screwed in and out of the attached housing l3. A-nut M will hold the valve i l in place in the desired position.
From the above-described arrangement, it will be seen that I have provided a turbo-blower which is obviously adaptable to internal combustion engines of varied requirements. If the turbo-blower has a much greater capacity than necessary for the engine, the valve 1 I will be open to a comparably large extent. If,- however, the turbo-blower has a capacity only slightly in excess of that needed by the engine, the valve II will be almost closed. It has long been known that the capacity of a centrifugal blower must closely approximate the requirements of the engine supercharge, for otherwise deleterious and unsafe conditions in the air-charging system, such as hammering will arise. By means of the present invention, however, a single turbo-blower can be used with internal combustion engines of a wide capacity range. For example, a turboblower which has been designed for an engine having a compression space of 1.5 liters can, b; proper adjustment of the short circuit, be made usable for an engine of only '1 liter compression space.
It is also to be noted, that the use of a relatively large turbo-compressor does not result in any loss in over-all eiilciency of the resulting blower-engine combination. While the larger blower will use more engine power, the provision of a superfluous amount of air shifts the operation of the blower into a region of higher emciency, so that theover-all efllciency of the combination remains substantially the same. A proper designing of the outlet of the blower also makes up for any loss in efficiency.
While the invention has been described in connection with an internal combustion engine of .the Diesel type, it is also equally applicable to engines using a carbureter. If the carbureter is to be positioned on the p ressure side of the blower, this can be done in the usual manner. If the carbureter is to be positioned on the suction side of the blower, the mouth upon the suction side of the short circuit will be displaced along the entrance to the turbine wheel in such a manner as to exclude losses in fuel.
It will also be obvious to those skilled in this art that the principles of the present invention may be applied in the case of a two-stage centrifugal blowers, and, furthermore, that the supplied air may be used for scavenging purposes as well as charging purposes.
While a particular type of control means for varying the amount of short circuit between the suction and delivery sides of the blower has been disclosed, it will also be clear to those skilled in this art that the other type of throttling means such as butterfly valves, slide valves and the like are contemplated.
Having now-thus described the invention, in a specific embodiment thereof, as well as the function and mode of operation of the same, what I claim as new and desire to secure Letters Patent of the United Statesis:
1. A turbo-blower comprising, in combination, a turbine wheel, a casing surrounding said wheel having a centrally located inlet opening, a substantially tangential discharge opening, and a 3. A turbo-blower comprising, in combination,-
a casing having a centrally located inlet opening, a substantially tangential discharge openingand a by-pass opening, a turbine wheel centrally mounted for rotation within said casing, and airguide vanes for leading the air from said turbine wheel to said discharge opening, said by-pass opening being positioned in said casing intermediate the periphery of said turbine wheel and said air-guide vanes, and means for throttling said by-pass opening.
4. Thecombination according to claim 3, in
which the outside of said by-pass openingis provided with a conical seating face, and said last means includes a conically faced valve adapted to cooperate with said face to control said by-pass. g
5. The combination according to claim 3, in which the outside of said by-pass opening is provided with a conical seating face, and said last means includes a conically faced valve adapted to cooperate with said face to control said bypass, a threaded extension on said valve, and means for holding said extension in the desired position of said valve..
WALTER. BECHT.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2317723X | 1939-02-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2317723A true US2317723A (en) | 1943-04-27 |
Family
ID=7994605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US315665A Expired - Lifetime US2317723A (en) | 1939-02-04 | 1940-01-26 | Air blower |
Country Status (1)
Country | Link |
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US (1) | US2317723A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2470565A (en) * | 1945-10-09 | 1949-05-17 | Ingersoll Rand Co | Surge preventing device for centrifugal compressors |
US2524597A (en) * | 1947-10-08 | 1950-10-03 | Packard Motor Car Co | Crankcase ventilation |
US2613028A (en) * | 1946-01-08 | 1952-10-07 | Rolls Royce | Air compressor for use on aircraft |
US2645409A (en) * | 1948-05-17 | 1953-07-14 | Boeing Co | Air induction system heating in supercharged engine |
US2853227A (en) * | 1948-05-29 | 1958-09-23 | Melville W Beardsley | Supersonic compressor |
US3356034A (en) * | 1965-12-28 | 1967-12-05 | Ford Motor Co | Fluid pump flow bypass control |
-
1940
- 1940-01-26 US US315665A patent/US2317723A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2470565A (en) * | 1945-10-09 | 1949-05-17 | Ingersoll Rand Co | Surge preventing device for centrifugal compressors |
US2613028A (en) * | 1946-01-08 | 1952-10-07 | Rolls Royce | Air compressor for use on aircraft |
US2524597A (en) * | 1947-10-08 | 1950-10-03 | Packard Motor Car Co | Crankcase ventilation |
US2645409A (en) * | 1948-05-17 | 1953-07-14 | Boeing Co | Air induction system heating in supercharged engine |
US2853227A (en) * | 1948-05-29 | 1958-09-23 | Melville W Beardsley | Supersonic compressor |
US3356034A (en) * | 1965-12-28 | 1967-12-05 | Ford Motor Co | Fluid pump flow bypass control |
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