WO2008059251A2 - Pressure relief vent maintaining fire rating integrity - Google Patents

Pressure relief vent maintaining fire rating integrity Download PDF

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Publication number
WO2008059251A2
WO2008059251A2 PCT/GB2007/004359 GB2007004359W WO2008059251A2 WO 2008059251 A2 WO2008059251 A2 WO 2008059251A2 GB 2007004359 W GB2007004359 W GB 2007004359W WO 2008059251 A2 WO2008059251 A2 WO 2008059251A2
Authority
WO
WIPO (PCT)
Prior art keywords
pressure relief
trailing edge
leading edge
relief vent
louvers
Prior art date
Application number
PCT/GB2007/004359
Other languages
French (fr)
Other versions
WO2008059251A3 (en
Inventor
Christopher Coxon
John Coxon
Paul Coxon
Original Assignee
Christopher Coxon
John Coxon
Paul Coxon
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 Christopher Coxon, John Coxon, Paul Coxon filed Critical Christopher Coxon
Publication of WO2008059251A2 publication Critical patent/WO2008059251A2/en
Publication of WO2008059251A3 publication Critical patent/WO2008059251A3/en

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
    • F24F13/15Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre with parallel simultaneously tiltable lamellae
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C2/00Fire prevention or containment
    • A62C2/06Physical fire-barriers
    • A62C2/12Hinged dampers
    • A62C2/14Hinged dampers with two or more blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K15/00Check valves
    • F16K15/02Check valves with guided rigid valve members
    • F16K15/03Check valves with guided rigid valve members with a hinged closure member or with a pivoted closure member
    • F16K15/035Check valves with guided rigid valve members with a hinged closure member or with a pivoted closure member with a plurality of valve members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K17/00Safety valves; Equalising valves, e.g. pressure relief valves
    • F16K17/02Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side
    • F16K17/12Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side weight-loaded
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F11/00Control or safety arrangements
    • F24F11/30Control or safety arrangements for purposes related to the operation of the system, e.g. for safety or monitoring
    • F24F11/32Responding to malfunctions or emergencies
    • F24F11/33Responding to malfunctions or emergencies to fire, excessive heat or smoke

Definitions

  • This invention relates to an automatic pressure relief vent that resists fire penetration through itself in the walls, ceilings and floors into which it is fitted whilst providing for efficient air pressure relief for an enclosure.
  • the most common application is in relieving the excess pressure from an enclosure in which a gas suppression system has been fitted for the purposes of suppressing or extinguishing a potential fire by releasing an inert or chemical gas into the enclosure. It is also necessary that once the extinguishing gas has been discharged its concentration must be held for extended periods there fore once the excess pressure has been released the enclosure must be sealed from major leakage. The action of such a discharge in a sealed room is that the increased pressure can lead to structural damage.
  • This invention relates to the relief of the potential damaging pressure spike whilst maintaining an effective barrier to any fire penetration from an outside source through the pressure relief vent itself.
  • the interlinked blades maintain a linked status even when bending and general heat distortion occurs under fire conditions therefore maintaining an effective barrier from fire penetration.
  • the trailing edge portion of each blade that forms part of the interlinking combination also acts as an aileron which greatly assists its opening at the kinds of pressures that if exceeded can cause enclosure damage, therefore allowing for smaller vents to do the same job as previous less efficient ones.
  • the vent consists of a casing with one or more louvers or control members.
  • each blade has a rear facing slot or flap into which the forward facing aileron trailing edge of the corresponding blade fits.
  • each louver has a pivot pin about which it is free to rotate under air pressure.
  • each louver extends below the level of the underneath surface of each louver.
  • each louver will be in front the center of gravity as defined by the route of each louver being a mean line drawn from leading edge to trailing edge of each blade or as defined as the pivot being in front of each louver in the direction of the pressure to be relieved.
  • the louver has one or more skins to form a non flat blade or box type section.
  • Figure 1 shows a cross section of a series of louvers A hung on pivot D in casing E.
  • the Louvers are in the closed position with leading edge B interlinked with trailing edge C trailing edges interlinked.
  • FIG. 2 shows the louvers A in open position having rotated about pivot D from the force provided by air flow Z which when pushing on aileron C causes a rotational moment about D. Also the Airflow Z passing over the top of the Louver A creates a negative pressure Y which has a lifting moment about D.
  • Figure 3 shows how the minimum opening pressure of the vent can be varied and set by the amount of forward offset V between the pivot and the route of the louver W W.
  • Vl is of lesser offset that V2 and there fore the mass of the louver is acting about D on a shorter lever therefore having less resistance to opening under air pressure P.
  • the offset can be increased as with V2.
  • Figure 4 shows a casing E into which are fitted louvers A with pivot pins D which fit through corresponding holes in casing E.
  • Fig 5. Shows louvers A in open position from force df air or gas flow Z.
  • Fig 6. Shows the potential addition of a motor operated opening only vent where drive arm G rotates about axis F which his driven by a motor where pin H can rotate to push on link K which is fixed to pivot D which in turn is fixed to louver A but free to rotate in casing E.
  • Drag arm J rotates about pivot I which transforms power drive to all louvers, hi this figure the motor is disengaged and the louvdr is closed.
  • Fig 7. Shows the vent in motor open position where drive arhi G has rotated about axis F under the power of a motor and driven pin H under push link K to open louvers A irrespective of air flow Z2 or Z3.
  • Fig 8. Shows the vent with the drive arm G in the disengaged position and with the louvers A open from the force of air flow Z.
  • Fig 9. Shows three variations of cross sections as variations of louver design to represent some of the variation possibilities of this invention.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Emergency Management (AREA)
  • Health & Medical Sciences (AREA)
  • Business, Economics & Management (AREA)
  • Public Health (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Air-Flow Control Members (AREA)
  • Special Wing (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)

Abstract

The invention consists of a metal box frame into which a series of hinged louvers are fitted. These louvers consist of a metal wing section with a- leading edge with an up stand or slot and a formed tab on the trailing edge that has the effect of an aileron. They are hinged on a pivot point that is offset from a point drawn from the leading edge to the trailing edge. This offset has the effect of using the weight of the louvers as a bias about the pivot point effectively holding the louvers closed and the overlap or interlinked portion together until a minimum air pressure is reached. The effective aileron on the trailing edge of each blade serves two purposes, one is to fit into a slot or up stand on the leading edge of the next blade for the purposes of protection from fire penetration and the other is to provide a mechanically advantageous position, that being the furthest point from the pivot, to best use the force of the passing air being relieved to efficiently open the vent at low pressures.

Description

DESCRIPTION
Title: INVENTION .'Improvements in enclosure pressure relief whilst maintaining fire rating integrity'.
Background: This invention relates to an automatic pressure relief vent that resists fire penetration through itself in the walls, ceilings and floors into which it is fitted whilst providing for efficient air pressure relief for an enclosure. The most common application is in relieving the excess pressure from an enclosure in which a gas suppression system has been fitted for the purposes of suppressing or extinguishing a potential fire by releasing an inert or chemical gas into the enclosure. It is also necessary that once the extinguishing gas has been discharged its concentration must be held for extended periods there fore once the excess pressure has been released the enclosure must be sealed from major leakage. The action of such a discharge in a sealed room is that the increased pressure can lead to structural damage. This invention relates to the relief of the potential damaging pressure spike whilst maintaining an effective barrier to any fire penetration from an outside source through the pressure relief vent itself.
Example: To overcome this the present invention proposes a metal box into which are fitted a series of interlinked metal louvers which automatically unlink and open via air pressure pushing on them.
Advantages: The interlinked blades maintain a linked status even when bending and general heat distortion occurs under fire conditions therefore maintaining an effective barrier from fire penetration. The trailing edge portion of each blade that forms part of the interlinking combination also acts as an aileron which greatly assists its opening at the kinds of pressures that if exceeded can cause enclosure damage, therefore allowing for smaller vents to do the same job as previous less efficient ones.
Preferably the vent consists of a casing with one or more louvers or control members.
Preferably the leading edge of each blade has a rear facing slot or flap into which the forward facing aileron trailing edge of the corresponding blade fits.
Preferably each louver has a pivot pin about which it is free to rotate under air pressure.
Preferably the trailing edge of each louver extends below the level of the underneath surface of each louver.
Preferably the pivot point of each louver will be in front the center of gravity as defined by the route of each louver being a mean line drawn from leading edge to trailing edge of each blade or as defined as the pivot being in front of each louver in the direction of the pressure to be relieved.
Preferably the louver has one or more skins to form a non flat blade or box type section. Introduction to Drawings. An example of the invention will now be described by referring to the accompanying drawings:
Figure 1 shows a cross section of a series of louvers A hung on pivot D in casing E. The Louvers are in the closed position with leading edge B interlinked with trailing edge C trailing edges interlinked.
Figure 2 shows the louvers A in open position having rotated about pivot D from the force provided by air flow Z which when pushing on aileron C causes a rotational moment about D. Also the Airflow Z passing over the top of the Louver A creates a negative pressure Y which has a lifting moment about D.
Figure 3 shows how the minimum opening pressure of the vent can be varied and set by the amount of forward offset V between the pivot and the route of the louver W W. Vl is of lesser offset that V2 and there fore the mass of the louver is acting about D on a shorter lever therefore having less resistance to opening under air pressure P. To increase the opening pressure the offset can be increased as with V2.
Figure 4 shows a casing E into which are fitted louvers A with pivot pins D which fit through corresponding holes in casing E.
Fig 5. Shows louvers A in open position from force df air or gas flow Z.
Fig 6. Shows the potential addition of a motor operated opening only vent where drive arm G rotates about axis F which his driven by a motor where pin H can rotate to push on link K which is fixed to pivot D which in turn is fixed to louver A but free to rotate in casing E. Drag arm J rotates about pivot I which transforms power drive to all louvers, hi this figure the motor is disengaged and the louvdr is closed.
Fig 7. Shows the vent in motor open position where drive arhi G has rotated about axis F under the power of a motor and driven pin H under push link K to open louvers A irrespective of air flow Z2 or Z3.
Fig 8. Shows the vent with the drive arm G in the disengaged position and with the louvers A open from the force of air flow Z.
Fig 9. Shows three variations of cross sections as variations of louver design to represent some of the variation possibilities of this invention.

Claims

1. A pressure relief vent which comprises a frame defining an opening, control members mounted in the opening for movement about a spindle having a pivot axis offset from the axis running from leading edge to trailing edge of control member whereby the effective offset weight of the member acts as a moment about the spindle so as to hold the control member in the closed position until a set minimum air pressure is met.
2. A pressure relief vent according to claim 1, wherein there is a slot or up stand formed onto the leading edge of the control member into which the trailing edge of the adjacent member fits or overlap's and through opening motion separate from each other.
3. A pressure relief vent according to claim 1, or 2, wherein the spindle is offset from the axis running from leading edge to trailing edge creating a weight bias from the mass of the blade effective in holding the control members in the closed position until a minimum pressure is met.
4. A pressure relief vent according to 1 to 3 which has a formed flap on the trailing edge that extends past the belly of the blade that acts to interlink with adjacent blade and provide an aileron formed into the down position onto which passing air can act as an assistance to the blade opening about its axis pivot.
5. A pressure relief vent according to 1 to 4 where the pivot axis of each control member is distanced so the down forrhed aileron of each control member fits into the corresponding slot in the leading edge of the next.
PCT/GB2007/004359 2006-11-17 2007-11-13 Pressure relief vent maintaining fire rating integrity WO2008059251A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0622913A GB2443841A (en) 2006-11-17 2006-11-17 Pressure relief vent
GB0622913.2 2006-11-17

Publications (2)

Publication Number Publication Date
WO2008059251A2 true WO2008059251A2 (en) 2008-05-22
WO2008059251A3 WO2008059251A3 (en) 2008-08-07

Family

ID=37605442

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2007/004359 WO2008059251A2 (en) 2006-11-17 2007-11-13 Pressure relief vent maintaining fire rating integrity

Country Status (2)

Country Link
GB (1) GB2443841A (en)
WO (1) WO2008059251A2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106369195A (en) * 2016-11-22 2017-02-01 广东申菱环境系统股份有限公司 Multi-leaf check valve
WO2018051331A1 (en) * 2016-09-13 2018-03-22 Beth-El Zikhron Yaaqov Industries Ltd. Blast valve utilizing an aerodynamically configured blade

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0821447D0 (en) * 2008-11-25 2008-12-31 Coxon Christopher J A pressure relief vent
US20110028081A1 (en) * 2009-07-29 2011-02-03 Huntair, Inc. Back draft damper
GB2478581A (en) * 2010-03-11 2011-09-14 Christopher Coxon Pressure relief vent
US10330334B2 (en) * 2014-01-28 2019-06-25 The Boeing Company Pressure equalization vent for use in an aircraft assembly
GB2540356A (en) * 2015-07-13 2017-01-18 Afp Air Tech Ltd Two way pressure relief vent
CN109311529B (en) * 2016-06-14 2022-06-10 加拿大空客有限合伙公司 Ventilation shutter
GB2600994A (en) * 2020-11-17 2022-05-18 Apreco Ltd Assembly and method of installing an assembly

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3346007A (en) * 1962-08-22 1967-10-10 Israel State Gas flow control louvres
US3543439A (en) * 1968-10-07 1970-12-01 Frederick William Pantland Fire dampers
US4185658A (en) * 1976-05-26 1980-01-29 Prefco Products, Inc. Rotating blade damper
US5060557A (en) * 1990-01-26 1991-10-29 Penn Ventilator Company, Inc. Smoke damper blade seal
US5277658A (en) * 1992-12-21 1994-01-11 Goettl George M Barometric damper apparatus
GB2408793A (en) * 2003-12-04 2005-06-08 Richard Gatley Gas vent with linked control members contra-rotating at a predetermined pressure differential
GB2424061A (en) * 2005-03-07 2006-09-13 John Richard Coxon A ventilation device

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017899A (en) * 1958-07-11 1962-01-23 Elgen Mfg Corp Swivel units and damper assemblies using same
GB1116831A (en) * 1964-04-27 1968-06-12 Beta Aluminium Products Ltd Improvements in or relating to pivoted window louvres
US3561345A (en) * 1969-03-04 1971-02-09 American Air Filter Co Damper arrangement

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3346007A (en) * 1962-08-22 1967-10-10 Israel State Gas flow control louvres
US3543439A (en) * 1968-10-07 1970-12-01 Frederick William Pantland Fire dampers
US4185658A (en) * 1976-05-26 1980-01-29 Prefco Products, Inc. Rotating blade damper
US5060557A (en) * 1990-01-26 1991-10-29 Penn Ventilator Company, Inc. Smoke damper blade seal
US5277658A (en) * 1992-12-21 1994-01-11 Goettl George M Barometric damper apparatus
GB2408793A (en) * 2003-12-04 2005-06-08 Richard Gatley Gas vent with linked control members contra-rotating at a predetermined pressure differential
GB2424061A (en) * 2005-03-07 2006-09-13 John Richard Coxon A ventilation device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018051331A1 (en) * 2016-09-13 2018-03-22 Beth-El Zikhron Yaaqov Industries Ltd. Blast valve utilizing an aerodynamically configured blade
US11073300B2 (en) 2016-09-13 2021-07-27 Beth-El Zikhron Yaaqov Industries Ltd. Blast valve utilizing an aerodynamically configured blade
CN106369195A (en) * 2016-11-22 2017-02-01 广东申菱环境系统股份有限公司 Multi-leaf check valve

Also Published As

Publication number Publication date
GB2443841A (en) 2008-05-21
GB0622913D0 (en) 2006-12-27
WO2008059251A3 (en) 2008-08-07

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