GB2399498A - Air flow controller and fire damper in an air flow duct - Google Patents
Air flow controller and fire damper in an air flow duct Download PDFInfo
- Publication number
- GB2399498A GB2399498A GB0306178A GB0306178A GB2399498A GB 2399498 A GB2399498 A GB 2399498A GB 0306178 A GB0306178 A GB 0306178A GB 0306178 A GB0306178 A GB 0306178A GB 2399498 A GB2399498 A GB 2399498A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- axle
- flap
- socket
- fire damper
- 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.)
- Granted
Links
- 238000009423 ventilation Methods 0.000 claims abstract description 3
- 239000000779 smoke Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000000605 extraction Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
- F24F13/00—Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
- F24F13/08—Air-flow control members, e.g. louvres, grilles, flaps or guide plates
- F24F13/10—Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
- F24F13/14—Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
- F24F13/1486—Air-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 bearings, pivots or hinges
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
- F24F11/00—Control or safety arrangements
- F24F11/30—Control or safety arrangements for purposes related to the operation of the system, e.g. for safety or monitoring
- F24F11/32—Responding to malfunctions or emergencies
- F24F11/33—Responding to malfunctions or emergencies to fire, excessive heat or smoke
- F24F11/35—Responding to malfunctions or emergencies to fire, excessive heat or smoke by closing air passages
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air-Flow Control Members (AREA)
- Duct Arrangements (AREA)
- Flow Control (AREA)
Abstract
A fire damper in a ventilation duct 2 comprises a flap 12 which is pivotally mounted in the duct for movement from an open position, allowing air flow along the duct, to a closed position to inhibit air flow or the passage of flame along the duct. The flap is pivotally mounted on a round cross section axle 14 which extends through the duct wall and a motor unit is mounted on the end of the axle using a socket 26 having a polygonal inner socket wall for rotation of the flap. A protuberance formed by a pin 40, 46 extending through the axle is provided on the axle surface for engagement with the socket wall to cause the axle to rotate with the socket.
Description
Air Flow Controller and Fire Damper in an Air Flow Duct The present
invention relates to a fire damper for use in an air flow duct, and to a damper which can be used to regulate the flow of air in the duct.
Dampers in air flow ducts are well known. A commonly used form of damper consists of a flap inside the duct, which is held in an open position, extending along the duct axis. A heavy spring biases the flap to a closed position where it is transverse to the duct axis to block off the duct. A temperature sensitive trigger holds the flap in the open position and releases the flap in the event of a temperature rise caused by fire, such as a flame front moving through the duct. Typically, the flap is mounted on an axle extending across the duct, and a handle may be provided on the axle end outside the duct to enable an operator to return the flap to the open duct position.
As well as or instead of manual operation, such flaps may be fitted with a motorised control. One leading supplier of such motors is Belimo (www.bellimo.com/pdf/FireAndSmoke.pdf). A DC motor is fitted on the duct housing, over an exposed end of the flap axle. Usually the operation is normally closed', so that the motor is actuated to open the flap, and loss of power allows the flap to close under the force of the return spring. Other arrangements are possible, for example for smoke extraction in the event of a fire a flap may be closed by the motor and power removed to open the flap.
A problem arises with the mounting of the electric motor on the shaft end.
Usually the shaft is of round cross-section, whereas a square section shaft is wanted for connection to the motor via a socket driven by the motor.
A first aspect of the present invention provides a fire damper in a ventilation duct, the damper comprising a flap which is pivotably mounted in the duct for movement from an open position, allowing air flow along the duct, to a closed position to inhibit air flow or the passage of flame along the duct, the flap is pivotally mounted on a round cross section axle which extends through the duct wall and a motor is mounted on the end of the axle for rotation of the flap, the motor having a polygonal socket for receiving the shaft end, wherein a protuberance is provided on the shaft surface for; engagement with the socket wall to cause the axle to rotate with the socket.
The protuberance may extend into an angle or corner formed between two sides to the socket.
Preferably, protuberances are provided substantially diametrically opposite one another on the shaft.
A protuberance may be formed by a pin which is positioned in a bore in the shaft. The end of the pin distal of the shaft may be tapered.
The pin may extend through the shaft, forming protuberances on opposite sides of the shaft. Preferably the pin is angled where it leaves the shaft, and directed lengthways of the shaft. The pin may pivot relative to the I shaft.
It has been found that with this arrangement the alignment between to socket and pin is less crucial, the protuberance providing something of a universal joint to take up misalignment of the shaft and socket, particularly where the protuberance is pivotable relative to the shaft.
Other aspects and preferred features of the invention will be apparent from the following description and the accompanying claims.
The invention will now be described by way of example with reference to the accompanying drawings, in which: Figure 1 shows schematically in cross-section a flap in an air flow duct; Figure 2 is a view on arrow A of Figure 1; Figure 3 is schematic view of a motor unit; Figure 4 is an end view of a drive socket of the motor unit of Figure 3 and illustrating one embodiment of the invention; Figure 5 is a perspective view of another embodiment of the invention, and Figure 6 shows the embodiment of Figure 5 in a socket.
Figures 1 and 2 show duct wall 2 which is circular in cross-section. A continuous circular rim 4 having an inwardly extending flange 6 is riveted to the duct wall 2 at several positions around the rim by sealed rivets (not shown). The rim 4 has a step 8, to form a wall portion 10 which is spaced from the duct wall 2. The rim serves to provide a mounting and a stable mating surface for a flap or blade 12, and also strengthens the duct to maintain the duct shape in the region of the flap 12 to provide improved operation.
The flap or blade 12 is pivotably mounted on the rim 4 and is shown in full outline in its closed position, and in dotted outline in the open position.
As seen in Figure 1, the blade is stepped or joggled at a diameter region 12a so that the halves of the flap 12b, 12c occupy planes to either side of and parallel to the plane of the flange 6, when the flap is in the closed position.
Referring to Figure 2 the flap 12 is mounted on an axle 14 which rotate in a blind socket 16a formed on the rim 4 at one end 14a and extends through a sleeve 16b in the duct wall at the other end 14b. The axle 14 is a good fit in the socket 16a and sleeve 16b to reduce any tendency of the flap to wobble, and also to provide a degree of sealing against the passage of smoke when the flap is closed.
Heavy duty, i.e. strong, coil springs 18 surround the axle 14, and have one leg 20 bearing on the flange 6, and the other leg 22 bearing on the flap 12 to bias the flap into the closed position, against the flange 6.
The flap 12 is cut away at the edge 12e of the diameter region 12a, near the axle 14, to just clear the flange 6.
The flap 12 is overturned at its outer perimeter to form an axially extending flange 12d and a corner 12f to embrace the rim at the corner 11 formed at the radially outer edge of the flange 6 in portion 12c, and sit snugly at the corner 11 formed between the flange 6 and wall 10 at flap portion 12b. The flange 12d serves to strengthen the flap 12 to retain the shape of the flap during repeated operation and also provides an improved seal, as will be described hereinafter.
The construction thus far described is generally as seen in WO02/043810.
Other constructions of flap are well known in the art, and examples can be seen in EP-A-300992, which shows a square or rectangular flap, and EP-A829689.
In operation, the motor is driven to rotate the flap 12 into the open position and hold it there, shown in dotted outline, against the force of the springs 18. In the event of a fire, the motor power is cut off, allowing the flap to rotate to the closed position under the force of the springs 18. The overlap of the perimeters of the flap portions 12b, 12c adjacent flange 12d with the flange 6, and particularly the overlap at the corners 11, 12f ensures a good seal. The regions 12e, where the flap 12 is cut away may allow a small mount of air or smoke to pass but this will be rapidly blocked by soot etc., in the event of a fire.
By means of the motor 24, the flap 12 can be held in an intermediate position, thus serving to control the flow of air through the duct during normal operation. Typically, the degree of opening of the flap 12 would be set on installation of the system to balance air flow through the system, and then left.
In the duct 2 the normal air flow is in the flow direction of arrow A. Thus the fixings, such as the rivets holding rim 4 are closed or sealed. This reduces the risk of smoke escaping through the fixings once the flap 12 is closed. It will be appreciated the arrangement could be reversed, with air flowing in the direction of arrow B. Referring to Figure 3 this shows schematically a motor unit 25 comprising a socket 26 which is coupled to the shaft 28 of a motor 30, by gearing 32, housed in a housing 34. Such motors are supplied by Belimo Automation AG of Switzerland. Typically, socket 26 may have an internal bore 27 of diameter 10 or 12 mm.
As seen in Figure 4, the wall 36 of socket bore 27 is a sixteen sided convex- concave polygon, having 8 apices or corners 38. Thus socket bore 27 will receive a square section shaft in a number of orientations to allow for easy fitting of the motor unit over the shaft end and onto the duct wall. Bore 27 could be a simple concave shape such as a square or hexagonal cross section, for example, or have more apices. The present invention is concerned with fitting a round cross section shaft, typically a circular cross section shaft, into socket 26 for rotation with the socket.
Shown in Figure 4 is a steel shaft 14 with a steel pin 40 which extends through a diametral bore 42 in the shaft 14 to form two protuberances or projections 44 extending from the shaft outer surface 14c so as to project between the adjacent walls of an apex 38. The ends 40a of the pin 40 are chamfered to sit more comfortably in the apices 38. It can be seen that pin allows for some play in the connection between the shaft 14 and socket 26, which will serve to accommodate a small amount of misalignment between the shaft 14 and socket 26. Pin 40 could be floating in bore 42 or fixed in position, for example by spot welding.
Referring to Figure 5, this shows in perspective view a shaft 14 with a pin 46 which extends through a diametral bore 42 in the shaft 14. Pin 46 is bent where it exits the shaft 14 to form protuberances in the form of two legs 46a, 46b which lay generally parallel to the shaft 14. The pin 46 is free to rotate in the bore 42, as signified by the dotted outline.
As seen in Figure 6, the legs 46 engage in the apices 38 of the socket bore 27.
Typically shaft 14 may be 9mm diameter, and pin 46 may be 3mm diameter, but the chosen dimension will depend on the required strength for shaft 14, and the size of the socket Various modifications will be apparent to those in the art. Although the invention has been described with particular reference to circular cross- section ducts, it can be used with rectangular or other cross-section ducts.
Claims (12)
- CLAIMS: 1. A fire damper in a ventilation duct, the damper comprising aflap which is pivotably mounted in the duct for movement from an open position, allowing air flow along the duct, to a closed position to inhibit air flow or the passage of flame along the duct, the flap is pivotally mounted on a round cross section axle which extends through the duct wall and a motor is mounted on the end of the axle for rotation of the flap, the motor having a polygonal socket for receiving the shaft end, wherein a protuberance is provided on the shaft surface for engagement with the socket wall to cause the axle to rotate with the socket.
- 2. A fire damper as claimed in claim 1, wherein the protuberance extends into an apex formed between two sides of the socket wall.
- 3. A fire damper as claimed in claim 1 or 2, wherein two protuberances are provided, substantially diametrically opposite one another on the shaft.
- 4. A fire damper as claimed in any one of claims 1 to 4, wherein the protuberance is formed by a pin which is positioned in a bore in the shaft.
- 5. A fire damper as claimed in claim 4, wherein the end of the pin distal of the shaft is tapered.
- 6. A fire damper as claimed in claim 3, wherein the pin extends through the shaft, forming protuberances on opposite sides of the shaft.
- 7. A fire damper as claimed in claim 6, wherein the pin is angled where it leaves the shaft, and directed lengthways of the shaft.
- 8. A fire damper as claimed in claim 7, wherein the pin is pivotable relative to the shaft.
- 9. A flap for a fire damper according to any one of claims 1 to 8, having an axle and a protuberance on the axle.
- 10. A fire damper comprising a flap mounted on a rotatable axle, and a socket receiving an end of the axle, the socket having a polygonal inner surface, wherein a protuberance is provided on the shaft outer surface, the protuberance engaging with the socket wall to transfer rotational movement between the socket and the axle.
- 11. A fire damper as claimed in claim 10, wherein the protuberance extends in the axial direction of the axle.
- 12. A fire damper as claimed in claim 11, wherein the protuberance is pivotable relative to the shaft to extend at an angle to the axial direction.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0306178A GB2399498B (en) | 2003-03-18 | 2003-03-18 | Air flow controller and fire damper in an air flow duct |
EP04251469A EP1460352B1 (en) | 2003-03-18 | 2004-03-15 | Air flow controller and fire damper in an air flow duct |
AT04251469T ATE345474T1 (en) | 2003-03-18 | 2004-03-15 | AIRFLOW CONTROL AND FIRE DAMPER IN A VENTILATION SHAFT |
DE602004003157T DE602004003157D1 (en) | 2003-03-18 | 2004-03-15 | Air flow control and fire damper in a ventilation shaft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0306178A GB2399498B (en) | 2003-03-18 | 2003-03-18 | Air flow controller and fire damper in an air flow duct |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0306178D0 GB0306178D0 (en) | 2003-04-23 |
GB2399498A true GB2399498A (en) | 2004-09-22 |
GB2399498B GB2399498B (en) | 2005-08-17 |
Family
ID=9954991
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0306178A Expired - Fee Related GB2399498B (en) | 2003-03-18 | 2003-03-18 | Air flow controller and fire damper in an air flow duct |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1460352B1 (en) |
AT (1) | ATE345474T1 (en) |
DE (1) | DE602004003157D1 (en) |
GB (1) | GB2399498B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004058144B3 (en) * | 2004-11-30 | 2006-08-24 | Frank Wiedenfeld | Self regulating flow mixing limiter for building ventilation duct has flow regulating flap with propeller to vary effective flow |
DE502006008719D1 (en) * | 2005-07-14 | 2011-02-24 | Belimo Holding Ag | ACTUATOR |
WO2012021724A2 (en) * | 2010-08-11 | 2012-02-16 | Board Of Regents, The University Of Texas System | Fabrication method of composite carbon nanotube fibers/yarns |
AU2014100858A4 (en) * | 2013-09-30 | 2014-08-28 | Framelock Structures Pty Ltd | Venting System |
JP6195326B1 (en) * | 2017-01-16 | 2017-09-13 | 株式会社野木製作所 | Damper unit |
CN110721537B (en) * | 2019-11-14 | 2024-08-16 | 安普科技有限公司 | Spark collecting box |
CN112546516B (en) * | 2021-01-13 | 2021-12-31 | 徐州市沂芯微电子有限公司 | Automatic accurate dolly of putting out a fire based on temperature scanner |
CN114251466A (en) * | 2022-01-06 | 2022-03-29 | 春意环境科技有限公司 | Fireproof device for smoke prevention and exhaust air pipe and installation method thereof |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2271166A (en) * | 1992-10-01 | 1994-04-06 | Halton Oy | Fire damper actuators |
GB2286239A (en) * | 1993-12-29 | 1995-08-09 | Jr Russell Gordon Attridge | Remote control of fire damper in ventilation duct |
US5501542A (en) * | 1994-09-23 | 1996-03-26 | Farmatic Research, Inc. | Rapid coupling for a supported, driven shaft |
WO2002043810A2 (en) * | 2000-12-01 | 2002-06-06 | Tri-Air Innovations Limited | Air flow controller and fire damper in an air flow duct |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2869907A (en) * | 1956-07-20 | 1959-01-20 | Deliso John | Socket and rod coupling |
US4193541A (en) * | 1978-03-27 | 1980-03-18 | Energy Vent, Inc. | Damper latch |
US5169121A (en) * | 1990-12-24 | 1992-12-08 | Mitsubishi Electronics America, Inc. | Damper control mechanism |
EP0924475A1 (en) * | 1997-12-15 | 1999-06-23 | Kyoritsu Air Tech Inc. | Airflow-adjusting damper |
US6431203B1 (en) * | 1999-02-01 | 2002-08-13 | Honeywell International Inc. | Actuator mounting assembly |
US6198243B1 (en) * | 1999-02-23 | 2001-03-06 | Johnson Controls Technology Co. | Method for automatically determining range of movement of an electromechanical actuator |
US6097123A (en) * | 1999-06-03 | 2000-08-01 | Johnson Controls Technology Company | Brake and stall detector for a motorized actuator |
-
2003
- 2003-03-18 GB GB0306178A patent/GB2399498B/en not_active Expired - Fee Related
-
2004
- 2004-03-15 AT AT04251469T patent/ATE345474T1/en not_active IP Right Cessation
- 2004-03-15 EP EP04251469A patent/EP1460352B1/en not_active Expired - Lifetime
- 2004-03-15 DE DE602004003157T patent/DE602004003157D1/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2271166A (en) * | 1992-10-01 | 1994-04-06 | Halton Oy | Fire damper actuators |
GB2286239A (en) * | 1993-12-29 | 1995-08-09 | Jr Russell Gordon Attridge | Remote control of fire damper in ventilation duct |
US5501542A (en) * | 1994-09-23 | 1996-03-26 | Farmatic Research, Inc. | Rapid coupling for a supported, driven shaft |
WO2002043810A2 (en) * | 2000-12-01 | 2002-06-06 | Tri-Air Innovations Limited | Air flow controller and fire damper in an air flow duct |
Also Published As
Publication number | Publication date |
---|---|
EP1460352A1 (en) | 2004-09-22 |
EP1460352B1 (en) | 2006-11-15 |
GB2399498B (en) | 2005-08-17 |
ATE345474T1 (en) | 2006-12-15 |
DE602004003157D1 (en) | 2006-12-28 |
GB0306178D0 (en) | 2003-04-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20070318 |