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US3460855A - Angular adjustable roof tubular coupling for mounting turbine ventilator - Google Patents

Angular adjustable roof tubular coupling for mounting turbine ventilator Download PDF

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Publication number
US3460855A
US3460855A US727395A US3460855DA US3460855A US 3460855 A US3460855 A US 3460855A US 727395 A US727395 A US 727395A US 3460855D A US3460855D A US 3460855DA US 3460855 A US3460855 A US 3460855A
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section
turbine ventilator
annular
base plate
locking
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Expired - Lifetime
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US727395A
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Merland C Belden
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LOUVER Manufacturing CO Inc
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LOUVER Manufacturing CO Inc
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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04DROOF COVERINGS; SKY-LIGHTS; GUTTERS; ROOF-WORKING TOOLS
    • E04D13/00Special arrangements or devices in connection with roof coverings; Protection against birds; Roof drainage ; Sky-lights
    • E04D13/14Junctions of roof sheathings to chimneys or other parts extending above the roof
    • E04D13/147Junctions of roof sheathings to chimneys or other parts extending above the roof specially adapted for inclined roofs
    • E04D13/1471Junctions of roof sheathings to chimneys or other parts extending above the roof specially adapted for inclined roofs using a hinge mechanism for adaptation to the inclined roof

Definitions

  • An adjustable mounting structure for a turbine ventilator including a flat base plate having an opening therein, and a centrally located upturned flange circumscribing said opening, and an annular lip integrally formed with said flange and projecting radially inwardly therefrom.
  • Upper and lower cylindrical sections interconnected together by annular engaging elements to permit relative rotation therebetween.
  • the lower section being telescopically positioned around the upturned flange on the base plate and releasably connected thereto by locking means, and the upper section adapted to be connected to a turbine ventilator.
  • the upper end of the upper section and the lower end of the lower section being disposed in a plane substantially normal to the longitudinal axis of the said sections, and the annular inner engaging elements on the sections being positioned in a plane angularly disposed with respect to the longitudinal axis to permit proper positioning of the turbine ventilator.
  • An adjustable mounting structure for turbine ventilator which is readily adjustable to permit proper positioning of the turbine ventilator so that its axis of rotation is disposed normal to the horizontal.
  • the adjustable mounting structure including an upper cylindrical section and lower cylindrical section releasably interlocked together and to a base plate by unique releasable locking means.
  • the base plate having an upturned flange telescopically engaged by the lower cylindrical section and providing a water-tight connection therebetween.
  • the releasable locking means serving to releasably lock the upper and lower sections together against relative rotation therebetween and serving to securely but releasably lock the lower section to the base plate.
  • FIG. 1 is a perspective view of the invention illustrated in supporting relation with respect to the turbine ventilator
  • FIG. 2 is a cross-sectional view taken approximately along line 2--2 of FIG. 1 and looking in the direction of the arrows,
  • FIG. 3 is a cross-sectional view taken approximately along line 3-3 of FIG. 1 and looking in the direction of the arrows,
  • FIG. 4 is a perspective view illustrating the mounting structure in supporting relation with a turbine ventilator and mounted on a building structure
  • FIG. 5 is a perspective view illustrating details of construction of one of the locking members.
  • the adjustable mounting structure 10 includes a substantially flat, generally rectangular shaped base plate 12 which is preferably constructed of a suitable rigid metallic material such as sheet steel or the like.
  • the base plate has a centrally located circular opening 13 therein.
  • An upturned annular flange .14 is integrally formed with the base plate and circumscribed said circular opening 13. It will be noted that the annular flange 14 has an annular lip 15 integrally formed therewith and projecting radially inwardly therefrom.
  • the base plate 12 is adapted to be mounted upon the upper surface or roof of a building structure so that the opening 13 is disposed in registery or communicating relation with an opening 0 formed in the roof.
  • the turbine ventilator serves to exhaust hot humid air from the attic space below the roof through the opening 0.
  • the base 12 may be secured to the roof structure by any suitable means, such as nails or the like in a well-known manner.
  • the mounting structure also includes a lower cylindrical section which is also constructed of a suitable rigid metallic material, such as sheet steel or the like.
  • This lower cylindrical section 16 has a lower edge 17 which as shown is disposed in a plane which is substantially normal to the longitudinal axis of the lower section.
  • the lower end portion of the lower section is telescopically positioned around the upturned annular flange 14 as best seen in FIGS. 1 and 2.
  • Means are provided for releasably locking the lower section 16 to the base plate and this means includes a plurality of similar locking members or clips 18.
  • Each of these locking members 18, as best seen in FIG. 5, is formed of an elongate, substantially flat, strip of metal which is normally generally vertically oriented during use and has the upper end thereof bent at substantial right angles to the major portion thereof as at 19, and which terminates in a reduced end that defines an anchoring element 20.
  • Each locking member 18 has a threaded aperture 21 therein and the lower portion of the locking member is bent first inwardly and then outwardly to form a channel shaped locking portion 22.
  • the lower cylindrical section 16 has a plurality of openings 23 therein through which project bolts 24, each of which engages a threaded aperture 21 of one of the locking members 18.
  • the anchoring element 20 of each locking member projects through an opening 25 in the lower cylindrical section 16 and this opening 25 is of generally rectangular configuration.
  • the channel shaped locking portion 22 of each locking member is adapted to engage and be clamped against the lip 15 when the bolt 24 is revolved to pull the locking member in an outward direction.
  • These locking members are disposed interiorly of the lower section and serve to very eflectively but releasably innerlock the lower section to the base plate 12.
  • the upper marginal portion of the lower cylindrical section 16 has an outwardly projecting annular bead 26 formed thereat to impart rigidity to this upper edge portion.
  • the upper edge of the lower cylindrical section is bent outwardly from the bead 26, as at 27, so that an outwardly facing annular groove 28 is defined. It will be noted that the bead 26, outwardly projecting upper edge 27, and annular groove 28 are all obliquely disposed with respect to the longitudinal axis of the lower section.
  • the mounting structure 10 also includes a generally cylindrical upper section 29 which is also formed from a suitable rigid metallic material, such as sheet steel or the like, and which has an upper end edge disposed in a plane substantially normal to the longitudinal axis of the upper section.
  • the upper cylindrical section 29 is adapted to support the turbine ventilator 11 thereon in a wellknown manner.
  • the steel throat band 30 of the turbine ventilator is fixedly but releasably secured to the upper cylindrical section 29 so that the axis of rotation of the turbine is disposed substantially vertically. Since the adjustable mounting structure It is often applied to a slanting roof structure, it is necessary to adjust the lower section and upper section relative to each other to dispose the axis of rotation of the turbine so that it is substantially normal to the horizontal.
  • the lower edge portion of the upper cylindrical section has an outwardly pressed annular head 31 formed thereat to impart rigidity thereto and the lower peripheral edge 32 of the upper cylindrical section projects radially inwardly from the bead.
  • This lower end edge 32 projects into the annular groove 28 and engages the upper exterior surface of the bead 26 on the lower cylindrical section.
  • the radially outwardly projecting edge 27 of the lower section projects into the annular groove defined by the head 31.
  • the upper and lower cylindrical sections are interconnected together by the inter-engaging parts so that these sections may be rotated relative to each other.
  • These inter-engaging annular elements of the upper and lower sections are disposed generally in a plane disposed obliquely or angularly with respect to the longitudinal axis of the sections. It will, therefore be seen that by rotating the sections relative to each other, a wide range of adjustment may be accomplished for the purpose of disposing the axis of rotation of the turbine so that it is positioned substantially normal to the horizontal.
  • the upper cylindrical section 29 is also provided with a plurality of similar locking members or clips 18 identical in construction to those used in conjunction with the lower section.
  • the upper section 29 has a plurality of openings 33 therein through which the bolts 24 project and threadedly engage the locking members.
  • the anchoring element 20 of each locking element also projects through a generally rectangular shaped opening 34 formed in the upper section.
  • the channel shaped locking portion 22 of each locking member engages the inwardly projecting marginal portion of the lower section which is defined by the annual groove 28.
  • the inwardly projecting annual convexity as defined by the annular groove 28 is very snugly but releasably engaged by the channel shaped locking portion of each locking member thus releasably locking the upper and lower sections against relative rotation therebetween.
  • the mounting structure 10, constituting the present invention allows the turbine ventilator supported thereby to be eflectively and properly mounted on a roof or similar structure even though the roof may be a slanted or pitched type roof. Since the lower edge portion of the lower section is telescopically disposed over the upturned flange 14, a very effective watertight connection is provided thereat so that water cannot flow interiorly through the opening 13. Further, the use of the unique locking members permits efiective but releasable interlocking of the upper and lower sections together and to the base plate 12.
  • An adjustable mounting structure for a turbine ventilator comprising:
  • a substantially fiat base plate having a centrally located circular opening therein, an upturned annular flange integrally formed with said base plate and circumscribing said opening,
  • a substantially cylindrical upper section having an upper end lying in a plane disposed substantially normal to the longitudinal axis of said upper section, and adapted to have a turbine ventilator mounted thereon,
  • each of said locking members has a threaded aperture therein which is threadedly engaged by a threaded element carried by said associated section, and each locking member includes an anchoring element integrally formed therewith and spaced from the threaded element and projecting into an aperture in the associated section.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Joining Of Building Structures In Genera (AREA)

Description

Aug. 12, 1969 M. c. BELDEN 3,460,855
ANGULAR ADJUSTABLE ROOF TUBULAR COUPLING FOR MOUNTING TURBINE VENTILATOR Filed May a, 1968 INVEN'TOR. Me'eLAA/D C. BEADEAJ United States Patent 3,460,855 ANGULAR ADJUSTABLE ROOF TUBULAR COU- PLING FOR MOUNTING TURBINE VENTILATOR Merland C. Belden, Eden Prairie, Minn., assignor to Louver Manufacturing Co. Inc., Minneapolis, Minn.,
a corporation of Minnesota Filed May 8, 1968, Ser. No. 727,395 Int. Cl. E04d 13/14; E03b 7/06; E04b /48 US. Cl. 285-44 3 Claims ABSTRACT OF THE DISCLOSURE An adjustable mounting structure for a turbine ventilator including a flat base plate having an opening therein, and a centrally located upturned flange circumscribing said opening, and an annular lip integrally formed with said flange and projecting radially inwardly therefrom. Upper and lower cylindrical sections interconnected together by annular engaging elements to permit relative rotation therebetween. The lower section being telescopically positioned around the upturned flange on the base plate and releasably connected thereto by locking means, and the upper section adapted to be connected to a turbine ventilator. The upper end of the upper section and the lower end of the lower section being disposed in a plane substantially normal to the longitudinal axis of the said sections, and the annular inner engaging elements on the sections being positioned in a plane angularly disposed with respect to the longitudinal axis to permit proper positioning of the turbine ventilator.
SUMMARY OF INVENTION An adjustable mounting structure for turbine ventilator which is readily adjustable to permit proper positioning of the turbine ventilator so that its axis of rotation is disposed normal to the horizontal. The adjustable mounting structure including an upper cylindrical section and lower cylindrical section releasably interlocked together and to a base plate by unique releasable locking means. The base plate having an upturned flange telescopically engaged by the lower cylindrical section and providing a water-tight connection therebetween. The releasable locking means serving to releasably lock the upper and lower sections together against relative rotation therebetween and serving to securely but releasably lock the lower section to the base plate.
BRIEF DESCRIPTION OF THE FIGURES OF THE DRAWINGS FIG. 1 is a perspective view of the invention illustrated in supporting relation with respect to the turbine ventilator,
FIG. 2 is a cross-sectional view taken approximately along line 2--2 of FIG. 1 and looking in the direction of the arrows,
FIG. 3 is a cross-sectional view taken approximately along line 3-3 of FIG. 1 and looking in the direction of the arrows,
FIG. 4 is a perspective view illustrating the mounting structure in supporting relation with a turbine ventilator and mounted on a building structure, and
FIG. 5 is a perspective view illustrating details of construction of one of the locking members.
DETAILED DESCRIPTION OF THE DRAWINGS Referring now to the drawings and more specifically to FIG. 1, it will be seen that one embodiment of the novel mounting structure designated generally by the reference numeral is there shown. This mounting structure 10 is illustrated in mounting relation with respect to turbine ventilator 11 which revolves in response to the action of wind upon the turbine blades. The adjustable mounting structure 10 includes a substantially flat, generally rectangular shaped base plate 12 which is preferably constructed of a suitable rigid metallic material such as sheet steel or the like. The base plate has a centrally located circular opening 13 therein. An upturned annular flange .14 is integrally formed with the base plate and circumscribed said circular opening 13. It will be noted that the annular flange 14 has an annular lip 15 integrally formed therewith and projecting radially inwardly therefrom.
The base plate 12 is adapted to be mounted upon the upper surface or roof of a building structure so that the opening 13 is disposed in registery or communicating relation with an opening 0 formed in the roof. The turbine ventilator serves to exhaust hot humid air from the attic space below the roof through the opening 0. The base 12 may be secured to the roof structure by any suitable means, such as nails or the like in a well-known manner.
The mounting structure also includes a lower cylindrical section which is also constructed of a suitable rigid metallic material, such as sheet steel or the like. This lower cylindrical section 16 has a lower edge 17 which as shown is disposed in a plane which is substantially normal to the longitudinal axis of the lower section. The lower end portion of the lower section is telescopically positioned around the upturned annular flange 14 as best seen in FIGS. 1 and 2.
Means are provided for releasably locking the lower section 16 to the base plate and this means includes a plurality of similar locking members or clips 18. Each of these locking members 18, as best seen in FIG. 5, is formed of an elongate, substantially flat, strip of metal which is normally generally vertically oriented during use and has the upper end thereof bent at substantial right angles to the major portion thereof as at 19, and which terminates in a reduced end that defines an anchoring element 20. Each locking member 18 has a threaded aperture 21 therein and the lower portion of the locking member is bent first inwardly and then outwardly to form a channel shaped locking portion 22.
The lower cylindrical section 16 has a plurality of openings 23 therein through which project bolts 24, each of which engages a threaded aperture 21 of one of the locking members 18. The anchoring element 20 of each locking member projects through an opening 25 in the lower cylindrical section 16 and this opening 25 is of generally rectangular configuration. With this arrangement, the channel shaped locking portion 22 of each locking member is adapted to engage and be clamped against the lip 15 when the bolt 24 is revolved to pull the locking member in an outward direction. These locking members are disposed interiorly of the lower section and serve to very eflectively but releasably innerlock the lower section to the base plate 12.
The upper marginal portion of the lower cylindrical section 16 has an outwardly projecting annular bead 26 formed thereat to impart rigidity to this upper edge portion. The upper edge of the lower cylindrical section is bent outwardly from the bead 26, as at 27, so that an outwardly facing annular groove 28 is defined. It will be noted that the bead 26, outwardly projecting upper edge 27, and annular groove 28 are all obliquely disposed with respect to the longitudinal axis of the lower section.
The mounting structure 10 also includes a generally cylindrical upper section 29 which is also formed from a suitable rigid metallic material, such as sheet steel or the like, and which has an upper end edge disposed in a plane substantially normal to the longitudinal axis of the upper section. The upper cylindrical section 29 is adapted to support the turbine ventilator 11 thereon in a wellknown manner. The steel throat band 30 of the turbine ventilator is fixedly but releasably secured to the upper cylindrical section 29 so that the axis of rotation of the turbine is disposed substantially vertically. Since the adjustable mounting structure It is often applied to a slanting roof structure, it is necessary to adjust the lower section and upper section relative to each other to dispose the axis of rotation of the turbine so that it is substantially normal to the horizontal.
Therefore, the lower edge portion of the upper cylindrical section has an outwardly pressed annular head 31 formed thereat to impart rigidity thereto and the lower peripheral edge 32 of the upper cylindrical section projects radially inwardly from the bead. This lower end edge 32 projects into the annular groove 28 and engages the upper exterior surface of the bead 26 on the lower cylindrical section. Similarly, the radially outwardly projecting edge 27 of the lower section projects into the annular groove defined by the head 31.
With this arrangement the upper and lower cylindrical sections are interconnected together by the inter-engaging parts so that these sections may be rotated relative to each other. These inter-engaging annular elements of the upper and lower sections are disposed generally in a plane disposed obliquely or angularly with respect to the longitudinal axis of the sections. It will, therefore be seen that by rotating the sections relative to each other, a wide range of adjustment may be accomplished for the purpose of disposing the axis of rotation of the turbine so that it is positioned substantially normal to the horizontal.
The upper cylindrical section 29 is is also provided with a plurality of similar locking members or clips 18 identical in construction to those used in conjunction with the lower section. In this regard, the upper section 29 has a plurality of openings 33 therein through which the bolts 24 project and threadedly engage the locking members. The anchoring element 20 of each locking element also projects through a generally rectangular shaped opening 34 formed in the upper section. It will be noted that the channel shaped locking portion 22 of each locking member engages the inwardly projecting marginal portion of the lower section which is defined by the annual groove 28. Thus the inwardly projecting annual convexity as defined by the annular groove 28 is very snugly but releasably engaged by the channel shaped locking portion of each locking member thus releasably locking the upper and lower sections against relative rotation therebetween.
The mounting structure 10, constituting the present invention, allows the turbine ventilator supported thereby to be eflectively and properly mounted on a roof or similar structure even though the roof may be a slanted or pitched type roof. Since the lower edge portion of the lower section is telescopically disposed over the upturned flange 14, a very effective watertight connection is provided thereat so that water cannot flow interiorly through the opening 13. Further, the use of the unique locking members permits efiective but releasable interlocking of the upper and lower sections together and to the base plate 12.
Thus it will be seen that I have provided a novel adjustable mounting structure, for turbine type ventilators, which is not only of simple and inexpensive construction but one which functions in a more efficient manner than heretofore known comparable devices.
It will, of course, be understood that various changes may be made in the form, details, arrangement and proportions of the various parts without departing from the scope of my invention.
What I claim is:
1. An adjustable mounting structure for a turbine ventilator comprising:
a substantially fiat base plate having a centrally located circular opening therein, an upturned annular flange integrally formed with said base plate and circumscribing said opening,
an inturned annular lip integral with said flange and extending readily inwardly therefrom,
a lower generally cylindrical section having one end thereof telescopically positioned around said flange in snug fitting relation therewith,
a substantially cylindrical upper section having an upper end lying in a plane disposed substantially normal to the longitudinal axis of said upper section, and adapted to have a turbine ventilator mounted thereon,
interengaging annular elements on the upper end edge portion of said lower section, and on the lower end edge portion of said upper section revolvably interconnecting said sections together to permit relative rotation therebetween, said interengaging anular elements being positioned generally in a plane disposed in angular relation to the longitudinal axis of said sections,
a plurality of similar locking members, one of which is secured to said lower section interiorly thereof and being releasably interlocked with said base plate, another of said locking members being secured to one of said sections interiorly thereof and releasably engaging the other of said sections adjacent said annular interengaging elements, each of said locking members has a threaded aperture therein which is threadedly engaged by a threaded element carried by said associated section, and each locking member includes an anchoring element integrally formed therewith and spaced from the threaded element and projecting into an aperture in the associated section.
2. The mounting stiucture as defined in claim 1 wherein said locking member on said lower section releasably engages the annular lip on said upturned flange.
3. The mounting structure as defined in claim 1 wherein certain of said locking members are detachably mounted on said upper section and engage the annular element on the upper edge portion of said lower section.
References Cited UNITED STATES PATENTS 885,318 4/1908 Bullard 285-44 2,614,867 10/1952 Artis 28544 2,643,901 6/1953 Manoogian 285-403 1,667,688 4/1928 Goetzelman 285-428 THOMAS P. CALLAGHAN, Primary Examiner US. Cl. X.R.
US727395A 1968-05-08 1968-05-08 Angular adjustable roof tubular coupling for mounting turbine ventilator Expired - Lifetime US3460855A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6352473B1 (en) * 2000-03-10 2002-03-05 Thomas L. Clark Windjet turbine
US20060037259A1 (en) * 2004-08-17 2006-02-23 West G L Roof vent and method for installation
US20090013620A1 (en) * 2004-08-17 2009-01-15 West G Leonard Roof vent base plate and installation methods
US20120073239A1 (en) * 2010-09-23 2012-03-29 Haines Jacob L Flexible-Based Roof Vent for Metal Roofing
US20120178357A1 (en) * 2011-01-10 2012-07-12 Dan Joseph Rheaume Solar-powered fan that fits inside new and/or existing roof vents
US20130306760A1 (en) * 2011-11-11 2013-11-21 Aurora Konrad G. Schulz Gmbh & Co. Kg Air Nozzle

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US885318A (en) * 1907-09-09 1908-04-21 Oscar Gumbinsky Roof flashing.
US1667688A (en) * 1926-08-30 1928-04-24 Appleton Electric Co Clamp for connection boxes
US2614867A (en) * 1949-09-23 1952-10-21 Jr Samuel W Artis Roof jack
US2643901A (en) * 1949-04-28 1953-06-30 Stanley Works Connecting means for tubular sections

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US885318A (en) * 1907-09-09 1908-04-21 Oscar Gumbinsky Roof flashing.
US1667688A (en) * 1926-08-30 1928-04-24 Appleton Electric Co Clamp for connection boxes
US2643901A (en) * 1949-04-28 1953-06-30 Stanley Works Connecting means for tubular sections
US2614867A (en) * 1949-09-23 1952-10-21 Jr Samuel W Artis Roof jack

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6352473B1 (en) * 2000-03-10 2002-03-05 Thomas L. Clark Windjet turbine
US6582291B2 (en) 2000-03-10 2003-06-24 Thomas L. Clark Windjet turbine
US20060037259A1 (en) * 2004-08-17 2006-02-23 West G L Roof vent and method for installation
US20090013620A1 (en) * 2004-08-17 2009-01-15 West G Leonard Roof vent base plate and installation methods
US7882670B2 (en) 2004-08-17 2011-02-08 West G Leonard Roof vent base plate and installation methods
US20120073239A1 (en) * 2010-09-23 2012-03-29 Haines Jacob L Flexible-Based Roof Vent for Metal Roofing
US20120178357A1 (en) * 2011-01-10 2012-07-12 Dan Joseph Rheaume Solar-powered fan that fits inside new and/or existing roof vents
US20130306760A1 (en) * 2011-11-11 2013-11-21 Aurora Konrad G. Schulz Gmbh & Co. Kg Air Nozzle
US9487064B2 (en) * 2011-11-11 2016-11-08 Aurora Konrad g. Shulz gmBH & Co. Kg Air nozzle

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