US3635580A - Centrifugal refrigerant gas compressor capacity control - Google Patents
Centrifugal refrigerant gas compressor capacity control Download PDFInfo
- Publication number
- US3635580A US3635580A US14471A US3635580DA US3635580A US 3635580 A US3635580 A US 3635580A US 14471 A US14471 A US 14471A US 3635580D A US3635580D A US 3635580DA US 3635580 A US3635580 A US 3635580A
- Authority
- US
- United States
- Prior art keywords
- throttle
- disk
- intake passage
- piston
- impeller
- 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
- F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/462—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
- F04D29/464—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0253—Surge control by throttling
-
- 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
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
-
- 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
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B1/00—Compression machines, plants or systems with non-reversible cycle
- F25B1/04—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type
- F25B1/053—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type of turbine type
-
- 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
- F05D2250/51—Inlet
Definitions
- ABSTRACT A capacity control for a refrigerant gas compressor is comprised of a throttle disk in a throttle in nozzle intake passage extending to rotatable centrifugal gas impeller an are positioned within the nozzle i [2]] Appl. No.:
- a throttle intake passage leads through a nozzle intake passage that extends to the rotatable centrifugal gas compressor impeller.
- a throttle disk is pivotally mounted with the throttle intake passage and is movable from a minimum capacity position with the disk positioned transverse to the gas flow to a maximum capacity position with the disk positioned in parallel to the gas flow.
- a plurality of flowdirecting vanes are positioned within the nozzle intake passage that extends between the throttle disk passage and the impeller vanes.
- the throttle disk may be provided with at least one aperture to predetermine the gas flow for the minimum capacity of the gas compressor.
- a ring piston is concentrically positioned about the outer walls of the throttle intake passage and is connected by suitable linkage such as a bellcrank to translate the reciprocatory movement of the piston to pivotal movement of the piston to pivotal movement of the throttle disk.
- a cylinder is arranged concentric to the outer walls of the throttle intake passage and surrounding the piston so that fluid under pressure may be selectively applied to either side of the piston to move the piston accordingly.
- FIG. 1 is a fragmentary sectional view partly in elevation of a centrifugal gas compressor with the capacity control of the invention and showing the throttle disk in the full capacity position;
- FIG. 2 is a view similar to FIG. I but showing only the throttle passage and the intake nozzle passage with the throttle disk in the minimum capacity position;
- FIG. 3 is a fragmentary section on the line lIIIIl of FIG. 2;
- FIG. 4 is an even more fragmentary view similar to FIG. 2 but showing the throttle disk in an intermediate capacity position
- FIG. 5 is a section on the line V-V of FIG. 4.
- the centrifugal refrigerant gas compressor is shown to include the rotatable impeller 10 mounted on the end of the impeller shaft 111 for rotation therewith, A gas-collecting scroll 12 is positioned to surround the impeller 10 and collect through the diffuser structure the compressed gases issuing; from the compressed gas passages 13 of the impeller 10.
- the impeller 10 is also provided with intake gas passages 14 that are centrally located and the rotation of the impeller 10 causes the gas entering the impeller intake passages 14 and passing between the impeller vanes such as shown at 15, to be discharged under pressure from the discharge passages such as shown at 13 around the periphery of the impeller 10 as is well known to those skilled in the art.
- this invention provides for a novel arrangement of movable throttle disk 20 and a plurality of gas directing vanes such as shown at 20 through 23. It should be understood that the invention is not limited to any particular number or precise configuration or angle of direction of the gas flow directing vanes 20-23.
- the throttle disk 20 is mounted within a throttle intake housing 30 and is pivotal therein from the maximum capacity position shown in FIG. 1 to the minimum capacity position shown by FIG. 2 of the drawings.
- the throttle disk 20 is secured to pivotal stub shafts 31 and 32.
- the stub shaft 31 is connected by a bellcrank 33 and the stub shaft 32 is connected by a bellcrank 34 to respective pins 35 and 36 received in a groove 37 of a reciprocatory piston 38.
- the piston 38 is a ring piston concentrically mounted around the outer wall 39 of the throttle intake passage 30.
- a cylinder wall 40 is also concentrically mounted around the outer wall 39 of the throttle intake passage 30 in a manner to enclose the reciprocatory piston 38 and fluid under pressure is introduced within the cylinder selectively to either or both sides of the piston 38 for reciprocating the piston accordingly in a manner to move or maintain the throttle disk 20 at a desired position.
- the aforementioned US. Pat. Nos. 3,350,897 and 3,362,185 disclose various ways for valving fluid under pressure to either or both sides of a capacity control piston such as the piston 38 as used in the present invention. Since the arrangement for supplying fluid under pressure selectively to either or both sides of the piston 38 is not a part of the present invention, and any suitable arrangements well known to those skilled in the art may be used, the details of such an arrangement have been omitted from the present disclosure.
- a nozzle intake passage 50 is positioned between the throttle intake passage 30 and the impeller 10 to converge and direct the gas flow from the throttle disk 20 into the intake passages 14 of the centrifugal gas compressor impeller 10.
- a feature of the invention is the provision of the aforementioned gas flow directing vanes such as shown at 2043, to direct the flow of gas coming from the throttle disk 20 to the centrifugal gas impeller.
- the throttle disk 20 is provided with the aperture 25, which, when the throttle disk 20 is in the minimum capacity position shown by FIG. 2 of the drawings, provides a minimum gas flow into the intake nozzle 50 and the gas impeller.
- This invention is not limited to the provision of a centrally located aperture such as shown at 25 but one or more apertures :may be used in various positions as will be obvious to those skilled in the art.
- a capacity control for a centrifugal refrigerant gas compressor having a rotatable impeller with centrally located intake passages and peripherally located compressed gas passages comprising, a throttle intake passage, a nozzle intake passage extending from said throttle intake passage to the centrally located intake passages of said impeller, a throttle disk pivotally mounted in said throttle intake passage and having at least one aperture for determining the minimum capacity of said compressor when the throttle disk is in a minimum capacity position, means to move said disk from a position transverse to the gas flow for minimum capacity to a position parallel to the gas flow for full capacity and any position therebetween, and a plurality of gas flow directing and straightening vanes extending within said nozzle intake passage to direct the flow of gas into said impeller after passage from said throttle disk.
- the means to move said disk is comprised of a ring piston concentrically mounted on the outside of said throttle intake passage and connected to said disk by means of a bellcrank to translate reciprocatory movement of said piston to pivotal movement of said disk, and means to enclose said piston in a cylinder concentric with said throttle intake passage for applying a fluid under pressure within said cylinder to either side of said piston for reciprocating the piston in accordance therewith.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Air Conditioning Control Device (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1447170A | 1970-02-26 | 1970-02-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3635580A true US3635580A (en) | 1972-01-18 |
Family
ID=21765707
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14471A Expired - Lifetime US3635580A (en) | 1970-02-26 | 1970-02-26 | Centrifugal refrigerant gas compressor capacity control |
Country Status (5)
Country | Link |
---|---|
US (1) | US3635580A (enrdf_load_stackoverflow) |
JP (1) | JPS461736A (enrdf_load_stackoverflow) |
BE (1) | BE763359A (enrdf_load_stackoverflow) |
FR (1) | FR2079045A5 (enrdf_load_stackoverflow) |
GB (1) | GB1287867A (enrdf_load_stackoverflow) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4213307A (en) * | 1978-11-13 | 1980-07-22 | Westinghouse Electric Corp. | Oil separation and return system for centrifugal refrigerant compressors |
US4789300A (en) * | 1983-06-16 | 1988-12-06 | Rotoflow Corporation | Variable flow turbine expanders |
US4850796A (en) * | 1988-05-25 | 1989-07-25 | Sundstrand Corporation | Centrifugal pump with splitter vane/shut-off valve system |
US5224820A (en) * | 1991-09-25 | 1993-07-06 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Operating mechanism for variably settable blades of a turbomachine |
US5408708A (en) * | 1993-10-29 | 1995-04-25 | Vico Products Manufacturing Co., Inc. | Flow-control for a pump |
US20050263199A1 (en) * | 2002-11-26 | 2005-12-01 | David Meheen | Flow laminarizing device |
WO2008036832A1 (en) * | 2006-09-21 | 2008-03-27 | Borg Warner Inc. | Turbine housing with integrated ribs |
DE102014101213A1 (de) * | 2014-01-31 | 2015-08-06 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Verdichteranordnung für einen Turbolader eines Kraftfahrzeuges |
CN105715360A (zh) * | 2014-12-17 | 2016-06-29 | 霍尼韦尔国际公司 | 配平可调式离心压缩机和具有该压缩机的涡轮增压器 |
CN106104006A (zh) * | 2014-03-31 | 2016-11-09 | 三菱重工业株式会社 | 离心压缩机、增压器及离心压缩机的制造方法 |
EP3534014A1 (en) * | 2018-02-28 | 2019-09-04 | Garrett Transportation I Inc. | Turbocharger compressor having adjustable-trim mechanism including vortex reducers |
CN110219822A (zh) * | 2018-03-01 | 2019-09-10 | 盖瑞特交通一公司 | 具有包括涡流导风轮的可调调整机构的涡轮增压器压缩机 |
US11680582B2 (en) * | 2017-09-25 | 2023-06-20 | Johnson Controls Tyco IP Holdings LLP | Two piece split scroll for centrifugal compressor |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0893682A (ja) * | 1994-09-22 | 1996-04-09 | Kobe Steel Ltd | 遠心圧縮機 |
JP5223642B2 (ja) * | 2008-12-10 | 2013-06-26 | 株式会社Ihi | 遠心圧縮機 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE736207C (de) * | 1939-02-03 | 1943-06-09 | Ernst Beck Dr Ing | Stufenlos regelbares Geblaese |
GB727649A (en) * | 1950-05-16 | 1955-04-06 | Borg Warner | Improvements in or relating to overspeed control for air turbine driven pump |
US3160112A (en) * | 1958-07-31 | 1964-12-08 | Westinghouse Electric Corp | Check valve and application thereof |
US3289919A (en) * | 1964-11-16 | 1966-12-06 | Westinghouse Electric Corp | Centrifugal gas compressors |
-
1970
- 1970-02-26 US US14471A patent/US3635580A/en not_active Expired - Lifetime
-
1971
- 1971-02-24 JP JP869671A patent/JPS461736A/ja active Pending
- 1971-02-24 BE BE763359A patent/BE763359A/xx not_active IP Right Cessation
- 1971-02-25 FR FR7106393A patent/FR2079045A5/fr not_active Expired
- 1971-04-19 GB GB2320771A patent/GB1287867A/en not_active Expired
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE736207C (de) * | 1939-02-03 | 1943-06-09 | Ernst Beck Dr Ing | Stufenlos regelbares Geblaese |
GB727649A (en) * | 1950-05-16 | 1955-04-06 | Borg Warner | Improvements in or relating to overspeed control for air turbine driven pump |
US3160112A (en) * | 1958-07-31 | 1964-12-08 | Westinghouse Electric Corp | Check valve and application thereof |
US3289919A (en) * | 1964-11-16 | 1966-12-06 | Westinghouse Electric Corp | Centrifugal gas compressors |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4213307A (en) * | 1978-11-13 | 1980-07-22 | Westinghouse Electric Corp. | Oil separation and return system for centrifugal refrigerant compressors |
US4789300A (en) * | 1983-06-16 | 1988-12-06 | Rotoflow Corporation | Variable flow turbine expanders |
US4850796A (en) * | 1988-05-25 | 1989-07-25 | Sundstrand Corporation | Centrifugal pump with splitter vane/shut-off valve system |
US5224820A (en) * | 1991-09-25 | 1993-07-06 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Operating mechanism for variably settable blades of a turbomachine |
US5408708A (en) * | 1993-10-29 | 1995-04-25 | Vico Products Manufacturing Co., Inc. | Flow-control for a pump |
US20050263199A1 (en) * | 2002-11-26 | 2005-12-01 | David Meheen | Flow laminarizing device |
US7089963B2 (en) | 2002-11-26 | 2006-08-15 | David Meheen | Flow laminarizing device |
WO2008036832A1 (en) * | 2006-09-21 | 2008-03-27 | Borg Warner Inc. | Turbine housing with integrated ribs |
US20090280006A1 (en) * | 2006-09-21 | 2009-11-12 | Borgwarner Inc. | Turbine housing with integrated ribs |
US9068499B2 (en) | 2006-09-21 | 2015-06-30 | Borg Warner Inc. | Turbine housing with integrated ribs |
DE102014101213A1 (de) * | 2014-01-31 | 2015-08-06 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Verdichteranordnung für einen Turbolader eines Kraftfahrzeuges |
DE102014101213B4 (de) | 2014-01-31 | 2022-06-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Verdichteranordnung für einen Turbolader eines Kraftfahrzeuges |
CN106104006A (zh) * | 2014-03-31 | 2016-11-09 | 三菱重工业株式会社 | 离心压缩机、增压器及离心压缩机的制造方法 |
EP3128184A4 (en) * | 2014-03-31 | 2017-08-16 | Mitsubishi Heavy Industries, Ltd. | Centrifugal compressor, supercharger, and method for manufacturing centrifugal compressor |
CN106104006B (zh) * | 2014-03-31 | 2019-06-18 | 三菱重工业株式会社 | 离心压缩机、增压器、离心压缩机的制造方法及消音器 |
CN105715360A (zh) * | 2014-12-17 | 2016-06-29 | 霍尼韦尔国际公司 | 配平可调式离心压缩机和具有该压缩机的涡轮增压器 |
EP3043045A3 (en) * | 2014-12-17 | 2016-11-02 | Honeywell International Inc. | Adjustable-trim centrifugal compressor, and turbocharger having same |
US9708925B2 (en) | 2014-12-17 | 2017-07-18 | Honeywell International Inc. | Adjustable-trim centrifugal compressor, and turbocharger having same |
CN105715360B (zh) * | 2014-12-17 | 2019-10-25 | 盖瑞特交通一公司 | 配平可调式离心压缩机和具有该压缩机的涡轮增压器 |
US11680582B2 (en) * | 2017-09-25 | 2023-06-20 | Johnson Controls Tyco IP Holdings LLP | Two piece split scroll for centrifugal compressor |
US12044249B2 (en) | 2017-09-25 | 2024-07-23 | Tyco Fire & Security Gmbh | Two piece split scroll for centrifugal compressor |
EP3534014A1 (en) * | 2018-02-28 | 2019-09-04 | Garrett Transportation I Inc. | Turbocharger compressor having adjustable-trim mechanism including vortex reducers |
CN110219822A (zh) * | 2018-03-01 | 2019-09-10 | 盖瑞特交通一公司 | 具有包括涡流导风轮的可调调整机构的涡轮增压器压缩机 |
Also Published As
Publication number | Publication date |
---|---|
JPS461736A (enrdf_load_stackoverflow) | 1971-09-30 |
BE763359A (fr) | 1971-08-24 |
GB1287867A (enrdf_load_stackoverflow) | 1972-09-06 |
FR2079045A5 (enrdf_load_stackoverflow) | 1971-11-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3635580A (en) | Centrifugal refrigerant gas compressor capacity control | |
US3545890A (en) | Regenerative compressor | |
US3362625A (en) | Centrifugal gas compressor | |
US3362624A (en) | Centrifugal gas compressor | |
US4378194A (en) | Centrifugal compressor | |
US3289919A (en) | Centrifugal gas compressors | |
US2101051A (en) | Rotary fluid displacement device | |
CN105114327A (zh) | 多级压缩机及具有其的制冷系统 | |
US2101428A (en) | Rotary fluid displacement device | |
US2205902A (en) | Reversible fan | |
JPH1162894A (ja) | 自由ロータ | |
US3319877A (en) | Machines of the cross-flow type for inducing movement of fluid | |
US4902200A (en) | Variable diffuser wall with ribbed vanes | |
CN110173445A (zh) | 压缩机及空调系统 | |
US2083447A (en) | Centrifugal compressor | |
US2653754A (en) | Axial flow fan regulator | |
US20060115358A1 (en) | Centrifugal compressor | |
JP2020537077A (ja) | 再循環構造を備える遠心圧縮機 | |
US2490066A (en) | Diffuser | |
US2474410A (en) | Multistage compressor | |
US2817475A (en) | Centrifugal compressor and method of controlling the same | |
US2193243A (en) | Refrigerating apparatus | |
JP3342914B2 (ja) | ターボ装置 | |
US2819837A (en) | Compressor | |
CN110678659B (zh) | 螺旋桨式风扇以及制冷循环装置 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: MCQUAY-PERFEX, INC., A CORP. OF MN, MINNESOTA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:WESTINGHOUSE ELECTRIC CORPORATION, A CORP. OF PA;REEL/FRAME:003954/0610 Effective date: 19820204 Owner name: MCQUAY-PERFEX, INC., MINNEAPOLIS, MN A CORP. OF MN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:WESTINGHOUSE ELECTRIC CORPORATION, A CORP. OF PA;REEL/FRAME:003954/0610 Effective date: 19820204 |
|
AS | Assignment |
Owner name: MCQUAY INC. Free format text: CHANGE OF NAME;ASSIGNOR:MCQUAY-PREFEX INC.;REEL/FRAME:004190/0553 Effective date: 19830528 |
|
AS | Assignment |
Owner name: SNYDER GENERAL CORPORATION, STATELESS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:MCQUAY INC.;REEL/FRAME:004607/0047 Effective date: 19860327 Owner name: SNYDER GENERAL CORPORATION Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:MCQUAY INC.;REEL/FRAME:004607/0047 Effective date: 19860327 |
|
AS | Assignment |
Owner name: CITICORP INDUSTRIAL CREDIT, INC., 2700 DIAMOND SHA Free format text: SECURITY INTEREST;ASSIGNOR:MCQUAY INC., A MN CORP.;REEL/FRAME:004690/0296 Effective date: 19841102 |
|
AS | Assignment |
Owner name: CITICORP INDUSTRIAL CREDIT INC.,TEXAS Free format text: SECURITY INTEREST;ASSIGNOR:SNYDERGENERAL CORPORATION;REEL/FRAME:004765/0735 Effective date: 19870630 Owner name: CITICORP INDUSTRIAL CREDIT INC., 2700 DIAMOND SHAM Free format text: SECURITY INTEREST;ASSIGNOR:SNYDERGENERAL CORPORATION;REEL/FRAME:004765/0735 Effective date: 19870630 |
|
AS | Assignment |
Owner name: CITICORP NORTH AMERICA, INC., NEW YORK Free format text: SECURITY INTEREST;ASSIGNOR:SNYDERGENERAL CORPORATION, A MN CORP.;REEL/FRAME:005013/0592 Effective date: 19881117 |
|
AS | Assignment |
Owner name: MCQUAY INC., A CORP. OF MINNESOTA, MINNESOTA Free format text: RELEASED BY SECURED PARTY;ASSIGNOR:CITICORP NORTH AMERICA, INC.;REEL/FRAME:005278/0013 Effective date: 19881117 Owner name: SNYDERGENERAL CORPORATION, A CORP. OF MINNESOTA, T Free format text: RELEASED BY SECURED PARTY;ASSIGNOR:CITICORP NORTH AMERICA, INC.;REEL/FRAME:005278/0013 Effective date: 19881117 |
|
AS | Assignment |
Owner name: SNYDERGENERAL CORPORATION A CORP. OF DELAWARE Free format text: RELEASE BY SECOND PARTY OF A SECURITY AGREEMENT RECORDED AT REEL 5013 FRAME 592.;ASSIGNOR:CITICORP NORTH AMERICA, INC. A CORP. OF DELAWARE;REEL/FRAME:006104/0270 Effective date: 19920326 |