WO1980000742A1 - Damper for an air distribution system - Google Patents

Damper for an air distribution system Download PDF

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Publication number
WO1980000742A1
WO1980000742A1 PCT/US1979/000744 US7900744W WO8000742A1 WO 1980000742 A1 WO1980000742 A1 WO 1980000742A1 US 7900744 W US7900744 W US 7900744W WO 8000742 A1 WO8000742 A1 WO 8000742A1
Authority
WO
WIPO (PCT)
Prior art keywords
closure element
axis
damper
reference axis
input port
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.)
Ceased
Application number
PCT/US1979/000744
Other languages
English (en)
French (fr)
Inventor
D Gorchev
H Willke
T Rodgers
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MITCO CORP
Original Assignee
MITCO CORP
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
Application filed by MITCO CORP filed Critical MITCO CORP
Publication of WO1980000742A1 publication Critical patent/WO1980000742A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1426Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1406Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by sealing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1413Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre using more than one tilting member, e.g. with several pivoting blades
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D23/00Control of temperature
    • G05D23/185Control of temperature with auxiliary non-electric power
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1426Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means
    • F24F2013/1466Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means with pneumatic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1426Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means
    • F24F2013/1473Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means with cams or levers

Definitions

  • the invention relates generally to air distribution systems for buildings, and particularly to outside air dampers for such systems.
  • an actuator selectively translates the disk elements along their axes between a first position seated against their respective circular opening and a second position displaced from that opening.
  • an efficient seal is established, and when the elements are displaced from the openings, outside air flow is permitted.
  • Such a disk system is highly efficient compared to the blade approach with respect to leakage, since in the disk system, the closure force is applied to the center of the disk and that force is transferred to the disk edges at the sealing point in a manner substantially independent of an angle.
  • this system is inefficient in terms of required damper area to provide a desired air flow when open due to the blockage in air flow path caused by the disk elements.
  • an outside air damper has a fixed plate having a perimeter portion defining an opening, or orifice.
  • the orifice perimeter is preferably circular, although in some forms the perimeter may be elliptical.
  • the damper further ineludes a disk-like closure element having a perimeter seatable on the outside of the plate perimeter portion, an actuator for selectively directing a driving element between a first and second limit position.
  • the disk element is coupled to the driving element and a reference point by a linkage assembly.
  • the closure element moves between a closed position having the disk perimeter flush with the orifice, and a second position displaced from the plate and forming an angle with a plane defined by the orifice perimeter.
  • An array of such outside air dampers may be configured with a controller adapted to selectively control the position of the driving elements of the respective actuators. In this configuration, proportionate control of the various damper assemblies may be achieved to accommodate desired flow of outside air.
  • Fig. 1 is an elevation view of a damper assembly, looking from outside the air intake chamber;
  • Fig . 2 is a top view of the assembly of Fig .
  • Fig. 3 is an elevation view of the assembly of Fig. 1, as seen from inside the air intake chamber;
  • Fig. 4 is a detailed view of a section of the assembly of Fig. 1 along the lines 4-4;
  • Fig. 5 is a top view of the section of Fig. 4 along the lines 5-5;
  • Fig. 6 is a sectional view along the lines 6-6 of Fig. 3;
  • Figs. 7A and 7B are perspective views of the damper assembly of Fig. 1 in the closed and full open positions, respectively;
  • Figs. 8A and 8B show top and side elevation views, respectively, of an alternative actuator, linkage and disk assembly for the damper assembly of Fig. 1;
  • Fig. 9 shows a controlled array of the damper assemblies, each having a form similar to the damper assembly shown in Figs. 1-6.
  • Figs. 1-6 show an exemplary damper assembly 10 in accordance with the present invention.
  • the damper 10 is in the closed position.
  • Damper 10 includes a plate 12 with astrengthening frame 14.
  • the plate 12 has a perimeter portion defining a circular opening 18.
  • a dish-shaped disk 20 is shown with its outer perimeter 22 seated on an elastomer gasket 24 mounted on the perimeter portion of the plate 12.
  • the gasket24 may be mounted on the perimeter of disk 20.
  • the plate 12, for example is made of 1/8" aluminum, and is approximately 36" high and 36" wide.
  • the radius of the circular opening 18 in the plate 12 is about 34".
  • the closure element, or disk 20 is made of sheet aluminum.
  • disk 20 is a spherical shell section, i.e. essentially dish-shaped, with a 4" height and having its concave side extending toward the exterior (i.e. outside air side) of the damper assembly.
  • the diameter of the disk 20 is about 35", thereby overlapping the circular opening 18 when coaxial with opening 18 and flush with plate 12.
  • the open limit position for the disk 20 may be selected so that desired mixing may occur between the air flowing through opening 18 and return air ducted into the interior of the air intake chamber.
  • the disk 20 may have its concave side extending toward the interior of the damper assembly. In still other embodiments, the disk 20 may be substantially flat.
  • the frame 14 is an aluminum channel with dimensions of about 1" in height and 2" in depth.
  • the frame 14 is connected to the plate with fasteners or rivets (exemplified by the rivet 26 in Fig. 1).
  • the first support rod 30 is positioned on the inside of damper 10 in order to support the actuator as described below.
  • rod 30 is a 1 3/4" aluminum tube mounted across the rear of the opening 18 of the plate 12. Rod 30 extends directly across the opening 18, slightly off center, and is fastened to the plate 12 on either side of the opening 18 by U-bolts 32A and 32B, and associated nuts 34.
  • a screw fastener 36 (shown in Fig. 6) passes through the plate 12 and into rod 30 to resist any turning torque in rod 30.
  • the second support rod 40 is a linkage support and is a 1/2" standard pipe in the present embodiment.
  • the position of rod 40 is established by angle members 42 on either side of the opening 18.
  • the angle members 42 are connected to the plate 12 by spot welds 44.
  • the rod 40 passes through holes 46 of the angles 42 and is restrained on the other side of angles 42 by cotter pins 48 (shown in Fig. 6). With this configuration, rod 40 extends across opening 18 outside of an approximately 7 inches from that opening.
  • an actuator support member 50 is affixed to the actuator support rod 30.
  • a pneumatic actuator 52, and associated air hose 54, is mounted on the support member 50 by fasteners 56.
  • Actuator 52 includes a drive element or rod 58 which is adapted for movement between two limit positions along an actuatoraxis 59.
  • Rod 58 is coupled to disk 20 by a first linkage assembly.
  • This first linkage assembly includes a steel "T" bar having a shaft 62 coupled by pin 60 to rod 58 and passing through a bushing 63 mounted on support member 50.
  • the actuator mount and bushing 63 constrain shaft 62 to linear motion along its central axis.
  • the shaft 62 is joined at a T-connection 64 to a disk mounting shaft 66.
  • the disk mounting shaft 66 is mounted to the inside face of the disk 20 substantially at its center.
  • the connection is made by way of straps 68 wrapped around the ends of the shaft 66.
  • the straps 68 are secured on either side of the shaft 66 to the disk 20 by bolts 70 in a manner providing enough clearance so that the shaft 66 may rotate freely within the straps 68 about a pivot axis 82 which is perpendicular to and intersects with the actuator axis 59.
  • the shaft 66 provides a pivotal coupling between rod 58 and the center of the disk 20 about axis 82.
  • the disk 20 is supported by a second linkage assembly 72 connected to the linkage support rod 40.
  • the linkage assembly 72 consists essentially of two principal elements. One is the element 74 connected directly to the face of the disk 20 at its center and having a body 74A and a pair of arms 74B extending transversely awa ⁇ from the disk 20 along axes forming a predetermined angle with disk 20.
  • the other element is a pair of arms 76A and 76B rigidly affixed to the linkage support rod 40, as by welds.
  • the transverse arms 74B fit between the arms 76A and 76B connected to the linkage support rod 40.
  • the arms 74A and 76A are pivotally connected to each other, as are the arms 74B and 76B.
  • these pivotal connections are provided by a thin rod 80 which passes through hole 78 in arms 74A and 76A at one end of rod 80 and through corresponding holes in arms 74B and 76B at the other end of rod 80.
  • the rod 80 is bent on the outside of the arm overlap to keep the rod 80 in place.
  • the arms 74A, 74B, 76A and 76B form a two-bar linkage, with the first bar having one end fixedly coupled to disk 20, and the other end pivotally coupled to the second bar.
  • the second bar has its other end pivotally coupled by rod 40 about a reference axis 86 which is perpendicular to the actuator axis and is fixed with respect to plate 12.
  • the pivot axis 82 of the shaft 66 (which is rotatable within the straps 68).
  • Another is the axis 84 of rod 80 i.e. the axis of the connection of the ends of transverse arm 74A and the arm 76A and the connection of the ends of transverse arm 74B and arm 76B.
  • the axis 86 is perpendicular to and 1 1/2 inches from the central axis of hole 18.
  • the axis of rod 80 and axis 86 are 4 1/2 inches apart, and the axis of rod 80 and axis 82 are 4 1/4 inches apart.
  • Arms 74A and 74B are positioned so that each of those arms has a reference axis which passes through axes 82 and 84 and forms a 45 degree angle with respect to the central axis of the shaft 62.
  • the damper assembly 10 illustrated in Figs. 1 through 6, and in Fig. 7A, shows the assembly in a "closed” position, that is, with disk 20 flush against the elastomer seal 24 on plate 12.
  • rod 58 is positioned at its inner limit of travel.
  • a pneumatic control signal applied in hose 54 causes actuator 52 to drive rod 58 in the direction away from actuator 52.
  • the force applied to rod 58 is transferred to the center of the disk 20 by means of the rod 58 and shafts 62 and 66. Initially, the disk 20 is displaced from the gasket 24 along the axis of rod 58, breaking the seal between disk 20 and gasket 24.
  • the disk 20 begins to turn about the axis 82 of the cross shaft 66.
  • the shaft axis 82 is at the same time moving away from the opening 18. In effect, the disk 20 is first lifted off the gasket 24 and then turned.
  • damper assembly 10 The full open position of damper assembly 10 is illustrated in the dotted configuration shown in Fig. 5 and the perspective view of Fig. 7B. As shown, the rod 58 has reached its outer limit of travel. In addition, the disk 20 is oriented approximately 90° to the plate 12, with a portion of disk 20 passing through the circular opening 18. With this configuration, the effective cross section of the disk 20 seen by air entering the damper assembly is relatively small, providing correspondingly little resistance to air flow.
  • the disk 20 returns to its closed position.
  • the last part of its travel results in its being pulled against the gasket 24 surrounding the circular opening 18 of the plate 12 and pressed there by the retraction of the rod 58 and shaft 62.
  • the symmetry of the disk 20 about its center with the returning force of the rod 58 being placed at the center of the disk 20 means that the force sealing the disk 20 is equally distributed around its periphery 22, creating an airtight seal.
  • the linkage which couples the drive element to the closure element (disk 20) and the reference point (axis 86) includes two portions.
  • the first portion includes pin 60, shafts 62 and 66 and the straps 68 which establishes the pivotal connection between rod 58 and disk 20.
  • the second portion includes shaft 40 and its mounting assembly, and arms 74A, 74B, 76A and 76B and their interconnection means.
  • the first linkage portion is on one side (the "outside") of the disk 20, and the second linkage portion is on the other side (the "inside") of the disk 20.
  • FIGs. 8A and 8B show such a linkage assembly 90 which is suitable for coupling rod 58, disk 20 and plate 12.
  • elements corresponding to similar elements in Figs. 1-6 are denoted by identical reference designations.
  • the linkage assembly of Figs. 8A and 8B (which shows the disk 20 in the closed position) is entirely on one side (the "outside") of disk 20 (i.e. on the same side as actuator 52).
  • a rod 30 is rigidly connected across the circular opening in plate 12, in a similar manner to that shown in the embodiment of Figs. 1-6.
  • a pair of brackets 102 and 104 are rigidly connected (for example, by welds) to the centralportion of rod 30.
  • Rods 106, 108 and 110 are pivotally connected about axes 106A, 108A and 110A, respectively, between the two bracket members 102 and 104.
  • the actuator 52 is rigidly affixed to mounting bracket 112.
  • Bracket 112 is pivotally connected about axis 106A tothe rod 106.
  • the actuator 52 is controlled by electrical signals applied by way of cable 54 in a manner similar to that in the embodiment of Figs. 1-6.
  • a U-bracket 114 is affixed to the concave portion of disk 20 by upper fasteners 116A and 116B and bylower fasteners 118A and 118B.
  • the arm portions 120 and 122 of bracket 114 extend generally perpendicular to the interior of disk 20.
  • Cross bars 126, 128 and 130 are all pivotally connected about axes 126A, 128A and 130A, respectively, between the arms 120 and 122 of U-bracket114.
  • the driving element 58 of actuator 52 is coupled by the means of a fastener assembly 134 to the rod 126.
  • the first pair of link elements 136 and 138 are pivotally connected to the bars 110 and 128.
  • a second pair of linking elements 140 and 142 are pivotally connected to bars 108 and 130.
  • Spacer members 146 and 148 are positioned between link elements 140 and 102, and between linkage element 142 and bracket 104, respectively. With this configuration, the linkage assembly 90 provides a coupling between disk 20, the driving element 58 of actuator 52 and the plate 12.
  • disk 20 is a spherical shell section having a 4 inch height and a 35 inch diameter. Disk 20 is adapted formotion with respect to a 34 1/2 inch circular hole 18 of plate 12.
  • the bracket 122 includes mounting holes for rods 126, 128, and 130 so that the central axes 126A, 128A and 130A of those rods intersect with the central axis of disk 20 at distances 1 1/8 inches, 2 5/8 inchesand 3 1/8 inches from that disk, respectively.
  • the brackets 102 and 104 include mounting holes for rods 30, 106, 108, and 110 so that the central axes of those rods are located in accordance with the dimensions A-F denoted in Fig.
  • brackets 102 and 104 with rod 30 is adapted so that the direction of measurement of the dimensions A, B and C is parallel to the central axis 18A of hole 18 in plate 12 and so that axis 106A intersects with axis 18A.
  • link elements 140 and 142 connect axes 130A and 108 with a separation of 4 inches and link elements 136 and 138 connect axes 128A and 110A with a separation of 3 1/4 inches.
  • the linkage assembly 90 controls the disk 20 to move from the closed position (having its perimeter flush against plate 12), initially away from plate 12 and then in a pivotal motion about an axis parallel to axis 106A so that the plane of the perimeter of disk 12 forms a non-zero angle with the plane of plate 12, with the angle being functionally related to the linear displacement of driving element 58.
  • the embodiment of Figs. 8A and 8B may be configured with desired stop members to provide limits of the open position of the disk 20.
  • the actuator 52 may be controlled for proportional operation in the same manner as the embodiment of Figs. 1-6.
  • an array of damper assemblies 10 may be utilized in a building to provide an outside air damper system. Such an array is shown in Fig. 9.
  • a controller 92 provides pneumatic control signals to the actuators of the damper assemblies 10 so that the various ones may be opened to selected intermediate positions. For example, variations in the opening of the air intake can be accomplished by full opening some but not others of the damper assemblies 10.
  • the controller 92 may be a conventional digital computer system which has been programmed to generate the appropriate control signals for the various actuators to achieve a desired time sequence of openings and closings and degree of openings of the various damper assemblies.
  • environmental sensors may be used in conjunction with the controller, with the controller being programmed to control the damper operation in an adaptive manner. For example, such sensors may generate signals responsive to wind intensity and direction, and the controller may utilize these signals to selectively control various dampers in the array.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Air-Flow Control Members (AREA)
  • Air Conditioning Control Device (AREA)
PCT/US1979/000744 1978-09-20 1979-09-20 Damper for an air distribution system Ceased WO1980000742A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/944,135 US4223832A (en) 1978-09-20 1978-09-20 Damper for an air distribution system
US944135 1992-09-11

Publications (1)

Publication Number Publication Date
WO1980000742A1 true WO1980000742A1 (en) 1980-04-17

Family

ID=25480855

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1979/000744 Ceased WO1980000742A1 (en) 1978-09-20 1979-09-20 Damper for an air distribution system

Country Status (5)

Country Link
US (1) US4223832A (https=)
EP (1) EP0020462A1 (https=)
JP (1) JPS55500728A (https=)
CA (1) CA1143992A (https=)
WO (1) WO1980000742A1 (https=)

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CA1266199A (en) * 1985-01-28 1990-02-27 Waldemar H. Greiner Damper construction
US5103856A (en) * 1991-02-11 1992-04-14 Kohler Co. Anti-siphoning valve assembly
US5701117A (en) * 1996-01-18 1997-12-23 Brian Page Platner Occupancy detector
US5922095A (en) 1997-03-20 1999-07-13 Acoustiflo, Llc Air handling system for buildings and clean rooms
WO2002101198A2 (de) * 2001-06-13 2002-12-19 Thyssenkrupp Hiserv Gmbh Absaugvorrichtung für einen tunnel
US7410144B2 (en) * 2005-05-31 2008-08-12 Fisher Controls International Llc Pivot and bearing assembly for a manual valve operator
JP5631791B2 (ja) * 2011-03-28 2014-11-26 空研工業株式会社 差圧ダンパ装置
US10030882B2 (en) 2013-07-12 2018-07-24 Best Technologies, Inc. Low flow fluid controller apparatus and system
US11815923B2 (en) 2013-07-12 2023-11-14 Best Technologies, Inc. Fluid flow device with discrete point calibration flow rate-based remote calibration system and method
US10175669B2 (en) 2013-07-12 2019-01-08 Best Technologies, Inc. Fluid control measuring and controlling device
US11429121B2 (en) 2013-07-12 2022-08-30 Best Technologies, Inc. Fluid flow device with sparse data surface-fit-based remote calibration system and method
US10088821B2 (en) 2013-07-12 2018-10-02 Best Technologies, Inc. Self balancing air fixture
WO2015006777A2 (en) 2013-07-12 2015-01-15 Karamanos John C Fluid control measuring device
US11300319B2 (en) 2018-06-12 2022-04-12 Ademco Inc. Retrofit damper assembly
US11149980B2 (en) 2018-06-12 2021-10-19 Ademco Inc. Retrofit damper with pivoting connection between deployment and operational configurations
US11306941B2 (en) * 2018-06-12 2022-04-19 Ademco Inc. Retrofit damper optimized for universal installation
US10907858B2 (en) * 2018-08-29 2021-02-02 Air Distribution Technologies Ip, Llc Concentric shaft actuation mechanism

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2535525A (en) * 1948-08-23 1950-12-26 Fred E Wolfe Gate valve
US2674412A (en) * 1951-09-14 1954-04-06 Standard Thomason Corp Thermostatic valve
US3241568A (en) * 1964-09-04 1966-03-22 Allis Chalmers Mfg Co Valve and operating mechanism therefor
US3658293A (en) * 1970-01-21 1972-04-25 Ludwig Gaebel Butterfly valve with an articulated control
US3843090A (en) * 1972-01-15 1974-10-22 Zimmermann & Jansen Gmbh Damper
US3982583A (en) * 1974-12-30 1976-09-28 Honeywell Inc. Optimized air conditioning system
US4065097A (en) * 1976-05-17 1977-12-27 Airco, Inc. Slot sealing valve for vacuum coating apparatus

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2535525A (en) * 1948-08-23 1950-12-26 Fred E Wolfe Gate valve
US2674412A (en) * 1951-09-14 1954-04-06 Standard Thomason Corp Thermostatic valve
US3241568A (en) * 1964-09-04 1966-03-22 Allis Chalmers Mfg Co Valve and operating mechanism therefor
US3658293A (en) * 1970-01-21 1972-04-25 Ludwig Gaebel Butterfly valve with an articulated control
US3843090A (en) * 1972-01-15 1974-10-22 Zimmermann & Jansen Gmbh Damper
US3982583A (en) * 1974-12-30 1976-09-28 Honeywell Inc. Optimized air conditioning system
US4065097A (en) * 1976-05-17 1977-12-27 Airco, Inc. Slot sealing valve for vacuum coating apparatus

Also Published As

Publication number Publication date
EP0020462A1 (en) 1981-01-07
JPS55500728A (https=) 1980-10-02
CA1143992A (en) 1983-04-05
US4223832A (en) 1980-09-23

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