US3355095A - Combined casing and noise muffler for a vortex fan - Google Patents

Combined casing and noise muffler for a vortex fan Download PDF

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US3355095A
US3355095A US524132A US52413266A US3355095A US 3355095 A US3355095 A US 3355095A US 524132 A US524132 A US 524132A US 52413266 A US52413266 A US 52413266A US 3355095 A US3355095 A US 3355095A
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casing
ducts
noise
vortex fan
chambers
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US524132A
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Joel W Hollenberg
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Singer Co
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Singer Co
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Priority to US524132A priority Critical patent/US3355095A/en
Priority to DE6604795U priority patent/DE6604795U/en
Priority to GB22807/66A priority patent/GB1101966A/en
Priority to NL6608229A priority patent/NL6608229A/xx
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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
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/663Sound attenuation
    • F04D29/664Sound attenuation by means of sound absorbing material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D23/00Other rotary non-positive-displacement pumps
    • F04D23/008Regenerative pumps

Definitions

  • ABSTRACT OF THE DISCLOSURE vA vortex fan has a single unitary casing in which are provided an open side channel, a housing for a driving electric motor and enlarged cavities communicating respectivelywith inlet and outlet openings in the side channel.
  • Straight self-supporting ducts carried within the cavities and connected for fluid ow to the inlet and outlet openings form with the cavities acoustically resonant chambers.
  • the ducts have a series of distributed wall perforations providing acoustical coupling between the interior ofthe ducts and the respective separate chambers.
  • each chamber is filled with a preformed body of material having vfrequency-selective sound energy dissipative characteristics.
  • This invention relates to a vortex fan and more particularly to a casing for such a fan which combines in one structurey means providing a side channel, inlet and outlet, ducts, and a muffler for reducing the noise level with'- out'compromising the fan performance.
  • Vortexlpumps for handling liquids are well known in the art and have Ibeen used successfully for obtaining high cut-olf pressures' with relatively low peripheral speeds of the impeller.
  • 'Ihese pumps are characterized by having an open side channel which cooperates with a multi-bladed impeller to produce a' helical-toroidal path for iiuid flow through the pump,
  • a serious noise problem arises which is not present when'liquids are being used.
  • Previous attempts to correct the noise problem have resulted in severely degrading the performance as a fan tothe point where such performance is no longer attractive unless the noise can be tolerated.
  • the vortex fan has not found general favor as a practical means for obtaining high pressures in air or gas flow-systems.
  • an object of this invention to provide simple yand effective means for reducing the noise level of a vortex fan without adversely affecting the fan performance andnvvithout adding substantially to the size and weight of the fan or to the complexity of its assembly.
  • this invention provides a unitary casing containing an open side channel for the impeller, inlet and outlet ducts for said channel and tuned resonant chambers having dissi-pative characteristics and formed as part of the casing and surrounding and acoustically coupled to said ducts for reducing the noise in a frequency band related to the number of impeller blades and the angular velocity of the impeller.
  • FIG. 1 is an end elevational view of a vortex fan embodying the invention with parts of the casing cut away to show the impeller and also the muffler construction.
  • FIG. 2 is a longitudinal sectional view of the device of FIG. l taken substantially on the line 2-2 of FIG. 1.
  • FIG. 3 is a disassembled perspective view of the device of FIG. 1.
  • a vortex fan comprising essentially a rotary impeller 10, a stationary casing 11 and a cover 12.
  • the casing 11 is formed Iwith a semi-toroidal cavit 13 which forms the side channel for the fan.
  • a radial dividing wall 14 in the cavity 13 interrupts the peripheral continuity of the semi-toroidal channel and apertures 15 and 16 Iformed in the casing and located adjacent to and on opposite sides of the dividing wall 14 provide inlet and outlet openings for fluid iiow in the channel.
  • the rotary impeller 10 is also formed with a semitoroidal cavity 17 substantially identical with the cavity 13 in the casing 11 except that a series of radially extending peripherally-spaced blades 18 are contained in cavity 17 and form a series of cells facing vand opening into the casing cavity 13 when the parts are in assembled position as in FIG. 2.
  • the impeller 10 forms with the cavity 13 a helical-toroidal path for'uid ilow with the pitch of the helix being determined by the peripheral spacing of the blades 18.
  • An electric motor stator core 19 with winding 20 is pressed into a bore 21 formed in the casing 11.
  • Arotor core 22 - is secured to a shaft 23 journaled at one end in bearing 24 supported in the casing 11, and at the other end in bearing 25 supported in a removable end cover 26.
  • the impeller 10 is secured to shaft 23 for rotation therewith and has a close running fit with all adjacent surfaces of the casing 11 to minimize air leakage.
  • the cover 12 is itted to the casing 11 on a rabbeted shoulder 27 and the joint is sealed to form avsealed enclosure for the impeller
  • the structure involving the impeller blades 18 recurrently sweeping past the air stream entering and exiting through the apertures 15 and 16 produces a siren effect which generates a disagreeable whining noise in the audible frequency range.
  • the maximum noise level centers about a frequency related 'to thel number of blades and the angular velocity of the impeller and shows up on the noise spectrum as a-rather4 distinct peak.
  • the casing 11 is formed on the side opposite to the cavity 13 with two separate extended cylindrical chambers 28 and 29 which communicate with the respective apertures 15 and 16 as shown. These chambers are of larger internal diameter than the associated apertures and have their axial directions preferably parallel with the motor shaft axis. Duets 30 and 31 having internal diameters that match those of the apertures 15 and 16 are inserted axially within said chambers and in aligned connection with said apertures to form straight Huid-guiding inlet and outlet means. A ange 32 secured to the ducts 30 and 31 forms a cover for the chambers 28 and 29. Securement of the flange 32 to the ducts and to the chambers may be readily effected by the use of well-known epoxy cements. Although a single flange is shown in the illustrative embodiment, separate fianges for each duct may be used if desired and it is possible to form the flange integrally Vwithithe chamber wall.
  • annular spaces formed between the ducts 3f) and 31 and the walls of the chambers 23 and 29 are substantially filled with low-density sound absorbing material preferably in the form of a preformed annular body 33 of deformable foam plastic material.
  • the ducts 3f) and 31 in the portions within the chambers have a peripherally and longitudinally distributed series of perforations 34 made in vthe walls thereof which form acoustic coupling means between the annular chambers 28 and 29 and the respective duct interiors. Imperforate portions of the ducts extend exteriorly of the chambers to provide means for direct connection to external fluid-flow systems. as shown.
  • the foam plastic material 33 while apparently filling the annular space between the ducts and the chamber walls, is composed of interconnected air cells which occupy about 97% of the total'preformed volume so that each of the annular chambers functions as an acousticaliy resonant chamber having dissipative characteristics for selectively absorbing sound in a predetermined frequency band.
  • This effective volume of the annular chamber is chosen in relation to the effective total aperture formed by the wall perforations 34 to provide a resonant chamber for trapping and attenuating sound waves in the frequency band where the maximum noise peak associated with the impeller blade frequency normally would occur as explained above.
  • the objectionable air-bourne whining noise inherent in the normal vortex fan structure when used for gas flow is effectively trapped out and absorbed by the structure of this invention at a point close to its origin and so cannot be transmitted to the external fluid flow system.
  • the noise-eliminating structure of this invention does not impose any material restrictions ⁇ on the air flow and so idoes not adversely effect the ⁇ fan performance.
  • Air flow through the perforated ducts 30 Iand 31 is hardly ldistinguishable aerodynamically from fiow through similar ducts without the perforations.
  • the structure is simple, has few parts, is easily assembled and can with facility and advantage be formed integrally as part of the existing casing structure.
  • the chambers form a low impedance path for sound waves of a desirably selected 'frequency band to which they are tuned.
  • the material in the chambers is selected to be especially dissipative of sound energy in this frequency region so that undesirable sound waves are selectively trapped and dissipated in the chambers and do not enter the air stream either at the inlet or the outlet openings.
  • the whining sound is severely attenuated and cannot be transmitted out of the ian casing with any intensity and so is no longer a human disturbing factor in the operation of the fan.
  • a suitable material 'for the preformed element 33 is polyurethane foam obtainable commercially from the Scott Paper Company and .known in the trade as Scott Industrial Foam and Scottfelt.
  • a casing for a vortex fan comprising a unitary casting, a semi-toroidal channel formed in one face thereof, a cylindrical motor-supporting housing formed in the opposite face thereof, a radial dividing wall in said channel, apertures formed in said casing in the region close to and on opposite sides of said dividing wall, said apertures communicating with said channel to provide openings for fiuid iiow into and out of said channel, separate straight self supporting fiuid guiding ducts connected to said openings and extending normally away from said casing on the same side thereof as the motor-supporting housing, cavity means formed integrally with said casing and surrounding each of said ducts, flange means carried by each duct and forming with said duct and cavity means a single References Cited UNITED STATES PATENTS 1,811,651 6/ 1931 Schlachter 103-96 1,811,762 6/1931 Schnell 230--233 2,260,237 10/19

Description

Nov. 28, 1967 1 w. HOLLENBERG 3,355,095
COMBINED CASING AND NOISE MUFFLER FOR A VORTEX FAN Filed Feb. 1, 1966 2 sheets-shawl Joel W. Hollenberg WITNESS;
BY www Maag/ WTLORNEY NOV- 28, 1967 J. w. HOLLENBERG 3,355,095
COMBINED CASINO AND NOISE MUFFLER FOR A VORTEX FAN Filed Feb. Il, 1966 2 Sheets-Sheet 2 INVENTOR.
Joel W. HollenbergA United States Patent Oiilice 3,355,095 COMBINED CASING AND NOISE MUFFL'ER FOR A VORTEX FAN Joel W. Hollenberg, Middlesex, NJ., assignor to The Singer Company, New York, N.Y., a corporation of New Jersey Filed Feb. 1, 1966, Ser. No. 524,132
. 1 Claim. (Cl. 230-125) ABSTRACT OF THE DISCLOSURE vA vortex fan has a single unitary casing in which are provided an open side channel, a housing for a driving electric motor and enlarged cavities communicating respectivelywith inlet and outlet openings in the side channel. Straight self-supporting ducts carried within the cavities and connected for fluid ow to the inlet and outlet openings form with the cavities acoustically resonant chambers. The ducts have a series of distributed wall perforations providing acoustical coupling between the interior ofthe ducts and the respective separate chambers. 'Ilhe ducts are flangedtoprovide a closure for the respective chambersand have an imperforate portion extending exteriorly beyond the flanged portion to provide means for direct connectionto external huid iiow systems. Preferably each chamber is filled with a preformed body of material having vfrequency-selective sound energy dissipative characteristics. v
This invention relates to a vortex fan and more particularly to a casing for such a fan which combines in one structurey means providing a side channel, inlet and outlet, ducts, and a muffler for reducing the noise level with'- out'compromising the fan performance.
Vortexlpumps for handling liquids are well known in the art and have Ibeen used successfully for obtaining high cut-olf pressures' with relatively low peripheral speeds of the impeller. 'Ihese pumps are characterized by having an open side channel which cooperates with a multi-bladed impeller to produce a' helical-toroidal path for iiuid flow through the pump, When this type of pump is used for handling air or gases, a serious noise problem arises which is not present when'liquids are being used. Previous attempts to correct the noise problem have resulted in severely degrading the performance as a fan tothe point where such performance is no longer attractive unless the noise can be tolerated. As a result, the vortex fan has not found general favor as a practical means for obtaining high pressures in air or gas flow-systems.
It is, therefore, an object of this invention to provide simple yand effective means for reducing the noise level of a vortex fan without adversely affecting the fan performance andnvvithout adding substantially to the size and weight of the fan or to the complexity of its assembly.
In one aspect thereof, this invention provides a unitary casing containing an open side channel for the impeller, inlet and outlet ducts for said channel and tuned resonant chambers having dissi-pative characteristics and formed as part of the casing and surrounding and acoustically coupled to said ducts for reducing the noise in a frequency band related to the number of impeller blades and the angular velocity of the impeller.
The features of the invention which are believed to be novel are set forth with particularity in the appended claim. The invention itself, however, both as to its organization and method of operation, together with further objects and advantages thereof may best be understood by reference to the following description taken in connection with the accompanying drawings.
3,355,095 Patented Nov. 28, 1967 In the drawings:
FIG. 1 is an end elevational view of a vortex fan embodying the invention with parts of the casing cut away to show the impeller and also the muffler construction.
FIG. 2 is a longitudinal sectional view of the device of FIG. l taken substantially on the line 2-2 of FIG. 1.
FIG. 3 is a disassembled perspective view of the device of FIG. 1.
Referring now to the drawings, there is shown a vortex fan comprising essentially a rotary impeller 10, a stationary casing 11 and a cover 12. l
The casing 11 is formed Iwith a semi-toroidal cavit 13 which forms the side channel for the fan. A radial dividing wall 14 in the cavity 13 interrupts the peripheral continuity of the semi-toroidal channel and apertures 15 and 16 Iformed in the casing and located adjacent to and on opposite sides of the dividing wall 14 provide inlet and outlet openings for fluid iiow in the channel.
The rotary impeller 10 is also formed with a semitoroidal cavity 17 substantially identical with the cavity 13 in the casing 11 except that a series of radially extending peripherally-spaced blades 18 are contained in cavity 17 and form a series of cells facing vand opening into the casing cavity 13 when the parts are in assembled position as in FIG. 2.
It will be seen that the impeller 10 forms with the cavity 13 a helical-toroidal path for'uid ilow with the pitch of the helix being determined by the peripheral spacing of the blades 18.
An electric motor stator core 19 with winding 20 is pressed into a bore 21 formed in the casing 11. Arotor core 22 -is secured to a shaft 23 journaled at one end in bearing 24 supported in the casing 11, and at the other end in bearing 25 supported in a removable end cover 26. The impeller 10 is secured to shaft 23 for rotation therewith and has a close running fit with all adjacent surfaces of the casing 11 to minimize air leakage. The cover 12 is itted to the casing 11 on a rabbeted shoulder 27 and the joint is sealed to form avsealed enclosure for the impeller The structure involving the impeller blades 18 recurrently sweeping past the air stream entering and exiting through the apertures 15 and 16 produces a siren effect which generates a disagreeable whining noise in the audible frequency range. The maximum noise level centers about a frequency related 'to thel number of blades and the angular velocity of the impeller and shows up on the noise spectrum as a-rather4 distinct peak. Efforts to reduce the peak noise level by thel use of a conventional plenum chamber lined with sound absorbing material were unsuccessfulbecause the loss-'in pressure head due-to redirected llow in the plenum chamber4 could not be tolerated. That is to say, this method of noise reduction resulted in a fan having a poor pressure-flow characteristic.
However, in accordance with the present invention, structure was discovered which reduced the noise level to a satisfactory value and at the same time had little or no adverse effect on the pressure-flow performance of the vortex fan and this structure will now be described in detail.
The casing 11 is formed on the side opposite to the cavity 13 with two separate extended cylindrical chambers 28 and 29 which communicate with the respective apertures 15 and 16 as shown. These chambers are of larger internal diameter than the associated apertures and have their axial directions preferably parallel with the motor shaft axis. Duets 30 and 31 having internal diameters that match those of the apertures 15 and 16 are inserted axially within said chambers and in aligned connection with said apertures to form straight Huid-guiding inlet and outlet means. A ange 32 secured to the ducts 30 and 31 forms a cover for the chambers 28 and 29. Securement of the flange 32 to the ducts and to the chambers may be readily effected by the use of well-known epoxy cements. Although a single flange is shown in the illustrative embodiment, separate fianges for each duct may be used if desired and it is possible to form the flange integrally Vwithithe chamber wall.
The annular spaces formed between the ducts 3f) and 31 and the walls of the chambers 23 and 29 are substantially filled with low-density sound absorbing material preferably in the form of a preformed annular body 33 of deformable foam plastic material.
The ducts 3f) and 31 in the portions within the chambers have a peripherally and longitudinally distributed series of perforations 34 made in vthe walls thereof which form acoustic coupling means between the annular chambers 28 and 29 and the respective duct interiors. Imperforate portions of the ducts extend exteriorly of the chambers to provide means for direct connection to external fluid-flow systems. as shown.
The foam plastic material 33, while apparently filling the annular space between the ducts and the chamber walls, is composed of interconnected air cells which occupy about 97% of the total'preformed volume so that each of the annular chambers functions as an acousticaliy resonant chamber having dissipative characteristics for selectively absorbing sound in a predetermined frequency band. This effective volume of the annular chamber is chosen in relation to the effective total aperture formed by the wall perforations 34 to provide a resonant chamber for trapping and attenuating sound waves in the frequency band where the maximum noise peak associated with the impeller blade frequency normally would occur as explained above. Thus, the objectionable air-bourne whining noise inherent in the normal vortex fan structure when used for gas flow is effectively trapped out and absorbed by the structure of this invention at a point close to its origin and so cannot be transmitted to the external fluid flow system. Of extreme importance is the fact that the noise-eliminating structure of this invention does not impose any material restrictions `on the air flow and so idoes not adversely effect the `fan performance. Air flow through the perforated ducts 30 Iand 31 is hardly ldistinguishable aerodynamically from fiow through similar ducts without the perforations. Furthermore, the structure is simple, has few parts, is easily assembled and can with facility and advantage be formed integrally as part of the existing casing structure.
The chambers form a low impedance path for sound waves of a desirably selected 'frequency band to which they are tuned. The material in the chambers is selected to be especially dissipative of sound energy in this frequency region so that undesirable sound waves are selectively trapped and dissipated in the chambers and do not enter the air stream either at the inlet or the outlet openings. Thus, the whining sound is severely attenuated and cannot be transmitted out of the ian casing with any intensity and so is no longer a human disturbing factor in the operation of the fan.
A suitable material 'for the preformed element 33 is polyurethane foam obtainable commercially from the Scott Paper Company and .known in the trade as Scott Industrial Foam and Scottfelt. The advantages of the preformed elements as compared with loose filling material for item 33, in addition to convenience and ease of manufacture, includes the ability to closely control the amount of material and its porosity and allows bonding the element 33 to the chamber or tube walls if desired to dampen vibration thereof.
The simplicity of the structure facilitates its assembly and the fact that there are few parameters subject to assembiy variation because of the integral-casting feature, promotes uniformity of performance.
While the invention has been explained by describing a particular embodiment thereof, it will be apparent that improvements and modifications may be made without departing from the scope of the invention as defined in the appended claim.
Having thus set forth the nature of this invention, what I Vclaim herein ist A casing for a vortex fan comprising a unitary casting, a semi-toroidal channel formed in one face thereof, a cylindrical motor-supporting housing formed in the opposite face thereof, a radial dividing wall in said channel, apertures formed in said casing in the region close to and on opposite sides of said dividing wall, said apertures communicating with said channel to provide openings for fiuid iiow into and out of said channel, separate straight self supporting fiuid guiding ducts connected to said openings and extending normally away from said casing on the same side thereof as the motor-supporting housing, cavity means formed integrally with said casing and surrounding each of said ducts, flange means carried by each duct and forming with said duct and cavity means a single References Cited UNITED STATES PATENTS 1,811,651 6/ 1931 Schlachter 103-96 1,811,762 6/1931 Schnell 230--233 2,260,237 10/1941 Stahl 230-232 3,181,646 5/1965 Edwards 230-233 3,259,072 7/ 1966 Carpenter 103--96 FOREIGN PATENTS 1,373,463 1 0/ 1964 France.
966,950 9/ 1957 Germany. 96,951 9/ 1939 Sweden.
HENRY F. RADUAZO, Primary Examiner. v
US524132A 1966-02-01 1966-02-01 Combined casing and noise muffler for a vortex fan Expired - Lifetime US3355095A (en)

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US524132A US3355095A (en) 1966-02-01 1966-02-01 Combined casing and noise muffler for a vortex fan
DE6604795U DE6604795U (en) 1966-02-01 1966-05-06 EDDY CURRENT FAN WITH NOISE ATTENUATION.
GB22807/66A GB1101966A (en) 1966-02-01 1966-05-23 Casing structure for vortex fan
NL6608229A NL6608229A (en) 1966-02-01 1966-06-14

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3411707A (en) * 1967-03-23 1968-11-19 Rotron Mfg Co Apparatus for preventing gas flow through bearings
US3421688A (en) * 1966-03-16 1969-01-14 Edwards High Vacuum Int Ltd Liquid sealed mechanical vacuum pumps
US3973865A (en) * 1974-02-07 1976-08-10 Siemens Aktiengesellschaft Side-channel ring compressor
US4412781A (en) * 1980-07-21 1983-11-01 Hitachi Ltd. Vortex blower
US4483656A (en) * 1981-12-18 1984-11-20 Hitachi, Ltd. Vortex blower
US5499900A (en) * 1992-12-29 1996-03-19 Joint Stock Company En & Fi Vortex flow blower
US5603601A (en) * 1993-12-03 1997-02-18 Gebr. Becker Gmbh & Co. Compressor with attachments mounted on stubs of a housing of the compressor
US6877511B2 (en) 1994-10-14 2005-04-12 Bird Products Corporation Portable drag compressor powered mechanical ventilator

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GB2246395A (en) * 1990-07-26 1992-01-29 Garrett Automotive Limited Noise attenuation in a turbocharger
DE4219249C2 (en) * 1992-06-12 1994-03-31 Kuehnle Kopp Kausch Ag Radial compressor, especially a turbocharger
GB2493703C (en) 2011-08-11 2020-03-04 Sca Ipla Holdings Inc OFDM subcarrier allocations in wireless telecommunications systems
GB2493702B (en) 2011-08-11 2016-05-04 Sca Ipla Holdings Inc OFDM subcarrier allocations in wireless telecommunications systems
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GB2493780B (en) 2011-08-19 2016-04-20 Sca Ipla Holdings Inc Telecommunications apparatus and methods
WO2016120056A1 (en) 2015-01-30 2016-08-04 Sony Corporation Telecommunications apparatus and methods
DE102016118574B4 (en) 2016-09-30 2021-02-11 Eberspächer Climate Control Systems GmbH Side channel blower, in particular for a vehicle heater

Citations (7)

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Publication number Priority date Publication date Assignee Title
US1811651A (en) * 1929-07-05 1931-06-23 Dempster Mill Mfg Company Primer for impulse pumps
US1811762A (en) * 1929-05-08 1931-06-23 Burgess Lab Inc C F Exhaust muffler
US2260237A (en) * 1939-04-08 1941-10-21 Hoover Co Suction cleaner
DE966950C (en) * 1943-02-18 1957-09-19 Siemens Ag Centrifugal machine for pumping liquids or gases
FR1373463A (en) * 1963-10-29 1964-09-25 Siemens Ag Annular wind tunnel built according to the bypass channel principle
US3181646A (en) * 1963-04-15 1965-05-04 Howard C Edwards Silencer having contiguous concentric layers of sound absorbent material
US3259072A (en) * 1964-10-26 1966-07-05 Gen Motors Corp Rotary fuel pump

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1811762A (en) * 1929-05-08 1931-06-23 Burgess Lab Inc C F Exhaust muffler
US1811651A (en) * 1929-07-05 1931-06-23 Dempster Mill Mfg Company Primer for impulse pumps
US2260237A (en) * 1939-04-08 1941-10-21 Hoover Co Suction cleaner
DE966950C (en) * 1943-02-18 1957-09-19 Siemens Ag Centrifugal machine for pumping liquids or gases
US3181646A (en) * 1963-04-15 1965-05-04 Howard C Edwards Silencer having contiguous concentric layers of sound absorbent material
FR1373463A (en) * 1963-10-29 1964-09-25 Siemens Ag Annular wind tunnel built according to the bypass channel principle
US3259072A (en) * 1964-10-26 1966-07-05 Gen Motors Corp Rotary fuel pump

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3421688A (en) * 1966-03-16 1969-01-14 Edwards High Vacuum Int Ltd Liquid sealed mechanical vacuum pumps
US3411707A (en) * 1967-03-23 1968-11-19 Rotron Mfg Co Apparatus for preventing gas flow through bearings
US3973865A (en) * 1974-02-07 1976-08-10 Siemens Aktiengesellschaft Side-channel ring compressor
US4412781A (en) * 1980-07-21 1983-11-01 Hitachi Ltd. Vortex blower
US4483656A (en) * 1981-12-18 1984-11-20 Hitachi, Ltd. Vortex blower
US5499900A (en) * 1992-12-29 1996-03-19 Joint Stock Company En & Fi Vortex flow blower
US5603601A (en) * 1993-12-03 1997-02-18 Gebr. Becker Gmbh & Co. Compressor with attachments mounted on stubs of a housing of the compressor
US6877511B2 (en) 1994-10-14 2005-04-12 Bird Products Corporation Portable drag compressor powered mechanical ventilator
US20050115564A1 (en) * 1994-10-14 2005-06-02 Devries Douglas F. Portable drag compressor powered mechanical ventilator
US7222623B2 (en) 1994-10-14 2007-05-29 Birds Products Corporation Portable drag compressor powered mechanical ventilator
US7849854B2 (en) 1994-10-14 2010-12-14 Bird Products Corporation Portable drag compressor powered mechanical ventilator

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GB1101966A (en) 1968-02-07
DE6604795U (en) 1970-02-26
NL6608229A (en) 1967-08-02

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