CA1155823A - Isolation damper - Google Patents

Isolation damper

Info

Publication number
CA1155823A
CA1155823A CA000386001A CA386001A CA1155823A CA 1155823 A CA1155823 A CA 1155823A CA 000386001 A CA000386001 A CA 000386001A CA 386001 A CA386001 A CA 386001A CA 1155823 A CA1155823 A CA 1155823A
Authority
CA
Canada
Prior art keywords
damper
damper blade
blade
duct
isolation
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
Application number
CA000386001A
Other languages
French (fr)
Inventor
Robert G. Stephenson
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.)
James Howden Australia Pty Ltd
Original Assignee
James Howden Australia Pty Ltd
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 James Howden Australia Pty Ltd filed Critical James Howden Australia Pty Ltd
Application granted granted Critical
Publication of CA1155823A publication Critical patent/CA1155823A/en
Expired 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L13/00Construction of valves or dampers for controlling air supply or draught
    • F23L13/06Construction of valves or dampers for controlling air supply or draught slidable only

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Supply (AREA)

Abstract

ABSTRACT
A slide type isolation damper for a gas duct wherein the damper blade is relatively thin and flexible so that it deforms under gas pressure to enter in sealing engagement with support bars positioned across the duct. The support bars provide structural integrity to the damper blade which would otherwise be excessively deformed by the gas pressure.

Description

The prcsent invention relates to an isolation damper for gas ducts and more particularly to an isolation damper of the slide type.
Isolation dampers are used to close off a gas duct. A
valve member of some type in the damper is brought into sealing engagement with the seat of the damper, or some other sealing element, to form a gas tight seal preventing gas leakage past the damper. Conventional dampers are of three types viz., the poppet type wherein a flexible sheet of steel is deformed onto the seat of the damper under system pressure or negative pressure; the slide type in which an inflexible steel plate is slid across the duct and into sealing engagement with sealing means on the damper seat and the butterfly type in which two pivotably connected inflexible plates are folded into or out of sealing engagement with the sealing means on the damper seat. Ihe poppet type valve cannot be conveniently used as an isolation damper intermediate the ends of a gas duct. The slide type suffers from the disadvantages that, firstly, a secondary seal system, which is susceptible to wear, is required to make sealing contact with the slide and, secondly, a housing is required to hold the plate when it has been withdrawn from the duct which is both unsightly and expensive to build.
The present invention is directed to a slide type isolation damper which does not have the disadvantages of known slide type dampers while having the advantage of the poppet type valve.
The present invention consists in an isolation damper for a gas duct comprising a damper blade, a pair of guide m0mbers adapted to guide the damper blade along a path transverse to the gas duct, and means to move the damper blade along the said path between a first position in which the damper blade extends across the duct and a second position in which it is substantially withdrawn from the duct, the arrangement being characterised in that the damper blade is relatively thin and flexible such that when in the first position and under an applied gas pressure it can elastically deform to enter into sealing engagement with the guide members and in that there is disposed intermediate the guide members, and in close juxtapostion with at least one side of the path of the damper blade, a plurality of support elements against which the damper plate can bear when pressure is applied to the face of the damper blade distal to the support elements.
The use of a thin, flexible damper blade allows the blade to be elastically deformed onto the guide members, which constitute the damper seat, without the need for a secondary sealing system. The flexibility of the blade also allows the blade to follow a non-linear path as it is introduced into, and drawn out of, the duct. The blade could, for instance lie in a plane parallel to and slightly above the gas duct and be turned through 90 just before entering the duct. In this way the isolation damper could be made more cheaply and would be less unsightly.
The damper blade is preferably formed of a material such as stainless steel and preferably has a thickness of no more than 5 mm., preferably no more than 3 mm. The use of such a thin damper blade facilitates the movement of the blade into and out of the duct as the thin blade can cut through any duct accumulation which occurs in the guide means.
The support elements preferably comprise an array of parallel bars or rods, however a grid of such bars or a perforate plate could also be used provided that the flow of gas through the duct is not unduly impeded. The support elements are preferably provided on each side of the damper blade path such that the damper blade will be supported against undue deformation upon the application of a positive pressure to either of its faces.
Hereinafter given by way of example only is a preferred embodiment of the invention described with reference to the accompanying drawings in which:-Fig. 1 is vertical sectional view through an isolationdamper according to this invention, and Fig. 2 is a view along A-A of Fig. 1.
The isolation damper 10 is mounted in a gas duct 11, the gas moving through the duct in the direction of the arrow B
of Fig. 1. The damper comprises a damper blade 12, a frame 13 surrounding the duct 11 which frame includes a pair of channel shaped side members 14 constituting guide members for the damper blade 12, and drive means 15 to move the damper blade 12 into and out of the duct 11.
The damper blade 12 comprises a sheet of stainless steel 3 mm. thick which is connected at its end remote from the duct to the drive means 15 as hereinafter described. The blade extends horizontally at the point of its connection to the drive means 15, it then turns through 90 before entering the guide slots 16 defined by side members 14.
The frame 13, in addition to the side members 14, includes a base member 17 and a top member 18. The base member 17 includes a longitudinally extending slot 19 in alignment with slots 16 in the side members 14, and into which the lower end of the damper blade 12 slides when the damper is fully closed. A flap 20 is hingedly connected to the underside of the base member 17 and can be opened to release dust which has lodged in the frame. A plurality of support bars 21 extends between the base member 17 and the top ~ember 18 on either side of the path traversed by the damper blade 12. The bars 21 are formed of mild steel or erosion resistant steel and may have an aerodynamically efficient cross sectional shape if desired.
The top member 18 may be formed with a removable top cover 22 such that the slot 23 in the top member through which the damper blade 12 is introduced into the frame 13 may be closed when the damper blade 12 is completely removed from the frame 13.

The drive means 15 comprises a reversible motor 24 which drives a pair of endless chains 25 about drums 26. The chains are connected to the free end of the damper blade 12.
Upon actuation of the motor 24 the damper blade 12 can be moved into or out of the duct 11.
If the damper blade 12 is introduced fully into the duct 11 and a force applied to one side of the blade 12 it will be elastically deformed against the edges of the slots 16, 19 and 23 of the frame 13 and will sealingly engage therewith in view of the relatively thin, flexible, nature of the damper blade 12. As the blade 12 is forced against the edges of the slots it will similarly be forced against the support bars 21 on the side of the slots opposite the direction from which the force is applied to the blade 12. The support bars 21 give to the damper blade 12 the structural integrity lacking due to its flexible nature.

Claims (6)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. An isloation damper for a gas duct comprising a damper blade, a pair of guide members adapted to guide the damper blade along a path transverse to the gas duct, and means to move the damper blade along the said path between a first position in which the damper blade extends across the duct and a second position in which it is substantially withdrawn from the duct, the arrangement being characterized in that the damper blade is relatively thin and flexible such that when in the first position and under an applied gas pressure it can elastically deform to enter into seal-ing engagement with the guide members and in that there is disposed intermediate the guide members, and in close juxtaposition with at least one side of the path of the damper blade, a plurality of support elements against which the damper plate can bear when pressure is applied to the face of the damper blade distal to the support elements.
2. An isolation damper as claimed in claim 1 in which the damper blade is formed of stainless steel having a thickness of no more than 5mm.
3. An isolation damper as claimed in claim 2 in which the damper blade has a thickness of no more than 3mm.
4. An isolation damper as claimed in any one of claims 1 to 3 in which support elements are provided on both sides of the path of the damper blade.
5. An isolation damper as claimed in claim 1 in which the support elements comprise an array of parallel bars or rods.
6. An isolation damper as claimed in claim 5 in which each of the bars or rods has an aerodynamically efficient cross sect-ional slope.
CA000386001A 1980-09-30 1981-09-16 Isolation damper Expired CA1155823A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AUPE582680 1980-09-30
AUPE5826/80 1980-09-30

Publications (1)

Publication Number Publication Date
CA1155823A true CA1155823A (en) 1983-10-25

Family

ID=3768739

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000386001A Expired CA1155823A (en) 1980-09-30 1981-09-16 Isolation damper

Country Status (5)

Country Link
EP (1) EP0061469B1 (en)
JP (1) JPS57501592A (en)
CA (1) CA1155823A (en)
WO (1) WO1982001234A1 (en)
ZA (1) ZA816395B (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3410311A (en) * 1966-04-22 1968-11-12 Universal Oil Prod Co Flexible curtain valve unit
AU419187B2 (en) * 1967-08-23 1971-11-25 Thermo-Technical Development Limited Improvements in or relating to isolators forthe gas-tight sectionalisation of flues and ducts
JPS5348225A (en) * 1976-10-14 1978-05-01 Osaka Shinku Kiki Seisakusho Vacuum gate valve
US4204662A (en) * 1979-03-23 1980-05-27 Reynolds Anthony C Valve for controlling the flow of fluids in conduits and the like

Also Published As

Publication number Publication date
WO1982001234A1 (en) 1982-04-15
EP0061469A4 (en) 1983-01-14
JPS57501592A (en) 1982-09-02
ZA816395B (en) 1982-10-27
EP0061469A1 (en) 1982-10-06
EP0061469B1 (en) 1986-05-07

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Legal Events

Date Code Title Description
MKEX Expiry