US855809A - Turbine-driven blower. - Google Patents

Turbine-driven blower. Download PDF

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Publication number
US855809A
US855809A US211940A US1904211940A US855809A US 855809 A US855809 A US 855809A US 211940 A US211940 A US 211940A US 1904211940 A US1904211940 A US 1904211940A US 855809 A US855809 A US 855809A
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United States
Prior art keywords
blower
turbine
inlet
impeller
housing
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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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US211940A
Inventor
Auguste Camille Edmond Rateau
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RATEAU TURBINE Co
Original Assignee
RATEAU TURBINE Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US13645502A external-priority patent/US827750A/en
Application filed by RATEAU TURBINE Co filed Critical RATEAU TURBINE Co
Priority to US211940A priority Critical patent/US855809A/en
Application granted granted Critical
Publication of US855809A publication Critical patent/US855809A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/006Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps double suction pumps

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

PATENTED JUNE 4, 1907.
No. 855,809. Y
A. G. E. RATEAU. TURBINE DRIVEN BLOWER.
APPLICATION IILED JUHB 10I 1904.
2 BREEZE-SHEET 1.
PATEN'IED mum, 1907" A. 0. B.- RATEAU.
TURBINE DRIVEN BLOWER.
APPLICATION rum) JUNE 10. 1904.
-2 SHEETS-SHEET 2.
UNITED sTATEs PATENT OFFICE.
AUGUSTE CAMILLE EDMOND RATEAU, OF PARIS, FRANCE, ASSIGNOR TO RATEAU TURBINE COMPANY, OF CHICAGO, ILLINOIS, A CORPORA- 'IION or WEST VIRGINIA.
TURBINE-DRIVEN BLOWER.
Specification of LettersPatent.
Patented June 4, 1907.
Original application filed December 24, 1902, Serial No. 1i36 ,455. Divided and this application filed June 10, 1904. Serial No. 2112940.
[ all whrmt it nut concern:
Be it known that I, AUGUSTE CAMILLE EDMOND RATEAU, a citizen of the Republic of France, residing at Paris, France, have invented a certain new and useful Improvement in 'lurbine-Driven Blowers, of which the following is a specification.
The present application is a division of my prior application, Serial No. 136,455, filed IO December 24, 1902, and relates to centrifugal fans or blowers.
The object of theinvention is to provide an improved organization of"blowing apparatus and driving mechanism therefor which as a whole will be simple, compact, strong,
and capable of operating efliciently at very high speed, to produce a current of air-of high velocity and pressure.
Generally speaking, the invention contemplates the employment of a turbine engine upon the shaft of which the impeller wheels of two or more centrifugal blowers are directly mounted, preferably one on each side of said turbine, with housings for said im peller wheels forming central inlets and peripheral delivery chambers of gradually increasing cross section, and a pipe of gradually increasing diameter connecting the discharge outlet of one blower with the inlet passage of 0 the other blower.
' I will describe my invention by reference to the accompanying drawings, wherein,
Figure l is a side elevation, partially in section, of myimproved turbinedriven blower; Fig. 2 is a plan view thereof; Fig. 3
is a vertical sectional view of one of the blowers showing the impeller wheel in full elevation.
The same figures of reference designate the same parts wherever shown.
The turbine engine 4, having the steam inlet 1 and the steam discharge pipe 6, has its 'shaft 14 mounted in bearings 15 and 16 on either side of said turbine; and on the ends 4 5 of said shaft are mounted the impeller wheels I? of the blowers. Said bearings are located approximately midway between the turbine and the respective impeller wheels. Both blowers are constructed alike, their internal o arrangement being indicated in Figs. 1 and 3.
The impeller wheel 17 is'surrounded by a housing 40 which is formed to provide an air inlet 18 opening centrally around the impeller wheel, and a peripheral d elivery-chamber 19, having a gradually-increased cross-sectional area in the direction of rotation of the wheel, terminating in an outlet 21. Said outlet is of smaller diameter than the inlet, the velocity of the air being greater at the discharge opening. Similarly the blower at the opposite end of the shaft is provided. with a housing which forms an inlet 28 and a peripheral i delivery chamber 29 having an outlet orifice 39 smaller than said inlet 38.
The impeller wheel is preferably con structed as shown in Figs. 1 and 3' of a single piece of metal formed with straight radial blades 30-and a central web or dislgeach blade being preferably provided with a strengthening rib on its back, which rib is formed by a radial extension of the central web. These impellers are driven at very high speed by the turbine and must be strong and rigid.
One of the advantages of the present in vention is that since two or more blowers are provided to absorb the power of the turbine, they can each be made comparatively small, so as to be adapted for the high speed at which a turbine necessarily runs.
The inlet and outlet orifices of the blowers preferably open upwardly, as shown, and in accordance with my invention the discharge outlet 21 of one blower is connected by a diagonal pipe 20 with the inlet 28 of the'other blower, said pipe gradually increasing in diameter in the direction of passage of the air, that is, toward the said inlet 28.
The operation is as follows: Air enters the inlet 18 and is carried radially outward'by the centrifugal action of the impeller 17, and delivered through the chamber 19 to the discharge outlet 21 of the first blower. From thence it passes through the pipe 20 of gradually increasing diameter to t 1e inlet 28 of the second blower, being finally delivered through the outlet 39 at a very highvelocity and pressure. The total air pressure at the inlet 28 of the second blower is considerably increased beyond the total pressure atthe discharge outlet of the first blower, due to the increasing diameter of the connecting pipe 20, and in accordance with the Well known laws of pressure in fluids. In the passages 19, and 29, eachof which gradually increases n cross section, the velocity of the air decreases, and the energy thereof is manifested in an increase ofi pressure. Thus the pressurecreated by the first impeller wheel increases gradually in the delivery chamber 19, and the pipe 20, and the air is com pressed again by the second impeller wheel, thus securing a higher final pressure than would have been obtained if the impeller wheels: were connected 111 series by a passage of unistrong, and compactly organized, so that very great power maybe developed in. a com; paratively small machine.
Having thus described my invention, I claim as new and desire to secureliy Letters Patent, thefollo'win 1. The combination a with a shaft and means for driving the same, of a fluid impeller having anrimpeller wheel mounted upon said shaft, a peripheral delivery chamber having an air inlet on each side of the impeller wheel, and a housing for said fluid impeller surrounding said air inlets, said housing having a single air inlet.
2. The combination with a shaft and means for driving the same, of centrifugal blowers having their impeller wheels mounted upon said shaft, a peripheral delivery chamber of gradually increasing cross-section for each impeller wheel, said delivery chambers having an inlets on each side of the impeller wheels, a housing for each impeller wheel said housing having an air inlet, and a pipe connecting the discharge outlet of one blower with the inlet to the housing of a succeeding blower.
.3. The combination with a centrifugal blower'provided with an impeller wheel and" a delivery chamber therefor having an air inlet on each side of said wheel,of a housing for said blower, said housing having an air inlet, a second centrifugal blower, and a pipe connecting the discharge outlet of said second blower with the inlet to the housing of the other.
4. The combination with a steam turbine and its shaft, of blowers having their impeller' wheels mounted directly on said shaft, a peripheral delivery chamber of gradually increasing crosssection for each impeller wheel, said chambers having air inlets on each side of said wheels a housing'foreach blower having a single an inlet communicating with the air inlets t0 the corresponding impeller wheel, the delivery outlet of each blower being smaller than the nlet to the Housing, and a pipe of gradually-increasing
US211940A 1902-12-24 1904-06-10 Turbine-driven blower. Expired - Lifetime US855809A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US211940A US855809A (en) 1902-12-24 1904-06-10 Turbine-driven blower.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13645502A US827750A (en) 1902-12-24 1902-12-24 Blowing machinery.
US211940A US855809A (en) 1902-12-24 1904-06-10 Turbine-driven blower.

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US855809A true US855809A (en) 1907-06-04

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2632596A (en) * 1950-05-19 1953-03-24 Christopher A Schellens Turbine driven pump
US3303994A (en) * 1964-03-16 1967-02-14 Mitsubishi Heavy Ind Ltd Exhaust gas turbine supercharger
US3817653A (en) * 1972-02-10 1974-06-18 Hydro Jet Pumps Inc Centrifugal pump apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2632596A (en) * 1950-05-19 1953-03-24 Christopher A Schellens Turbine driven pump
US3303994A (en) * 1964-03-16 1967-02-14 Mitsubishi Heavy Ind Ltd Exhaust gas turbine supercharger
US3817653A (en) * 1972-02-10 1974-06-18 Hydro Jet Pumps Inc Centrifugal pump apparatus

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