EP4201232A1 - Système de régulation de la chaleur pour une conduite d'eau - Google Patents

Système de régulation de la chaleur pour une conduite d'eau Download PDF

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Publication number
EP4201232A1
EP4201232A1 EP22193891.3A EP22193891A EP4201232A1 EP 4201232 A1 EP4201232 A1 EP 4201232A1 EP 22193891 A EP22193891 A EP 22193891A EP 4201232 A1 EP4201232 A1 EP 4201232A1
Authority
EP
European Patent Office
Prior art keywords
fuel
control ring
regulation system
air inlet
carrier
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.)
Pending
Application number
EP22193891.3A
Other languages
German (de)
English (en)
Inventor
Ibrahim Dabes
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of EP4201232A1 publication Critical patent/EP4201232A1/fr
Pending legal-status Critical Current

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Classifications

    • A—HUMAN NECESSITIES
    • A24—TOBACCO; CIGARS; CIGARETTES; SIMULATED SMOKING DEVICES; SMOKERS' REQUISITES
    • A24F—SMOKERS' REQUISITES; MATCH BOXES; SIMULATED SMOKING DEVICES
    • A24F1/00—Tobacco pipes
    • A24F1/30—Hookahs

Definitions

  • the invention relates to a heat regulation system for a hookah.
  • Water pipes also called shisha or hookah, usually consist of a water container, the so-called bowl, and a locking head that is attached to the water container.
  • a smoke pipe is attached to the breech head, at the upper end of which a tobacco head is arranged, on which tobacco is burned or vaporized together with fuel, e.g. glowing coal.
  • the smoke tube extends through the closure head into the water tank and opens into the water tank with its lower end below the water level.
  • a connection option for at least one smoke hose is provided on the closure head, which opens out via a corresponding recess into the air space provided in the water tank between the head and the liquid level.
  • the tobacco vaporizes with heavy smoke development. If the temperature is too low, there will be little or no smoke. If the temperature is too high, the tobacco burns and the smoke tastes unpleasantly bitter.
  • the optimal temperature in the tobacco head is of crucial importance for enjoyment. The consumption of tobacco and fuel changes the temperature conditions during use of the hookah.
  • Known tools for regulating the optimum temperature are fuel holders with an air-permeable fuel tray that is larger than the tobacco head.
  • the fuel is placed by the user in a suitable manner centered or off-center on the fuel tray above the tobacco bowl to increase or decrease the temperature in the tobacco bowl.
  • Fuel carriers are also known which enclose the fuel by means of a housing. Air inlet openings are provided in an upper area of the housing above the fuel and a lateral area of the housing next to the fuel, and air outlet openings which open into the tobacco head are provided in a bottom area of the housing below the fuel.
  • the air inlet openings above the fuel supply it with combustion air. If a lot of combustion air is supplied, the temperature in the tobacco head increases.
  • the air inlet openings on the side next to the fuel supply cool ambient air to the air outlet openings and reduce the temperature in the tobacco bowl. The temperature can be controlled accordingly by changing the cross-section of the side air intake openings.
  • a fuel carrier is provided with a fuel carrier cover which rests on a side wall of the fuel carrier and has a peripheral side wall which extends into an interior of the fuel carrier.
  • the peripheral side wall of the fuel carrier cover and the peripheral side wall of the fuel carrier each have a plurality of lateral air inlet openings.
  • an upper portion of the fuel tray above the side wall of the fuel tray has a plurality of upper air inlet holes, and the bottom wall of the fuel tray has a plurality of lower air outlet openings.
  • a heat regulation system for a water pipe has a fuel carrier for receiving fuel, e.g. coal, a fuel carrier cover for closing the fuel carrier and a control ring for controlling an air flow through at least one lateral air inlet opening.
  • the fuel carrier has a bottom wall with at least one lower air outlet opening and a peripheral side wall with at least one lateral air inlet opening.
  • the fuel carrier cover has at least one upper air inlet opening.
  • the control ring is provided separately from the fuel carrier cover and has at least one blocking area for blocking the flow of air.
  • the control ring can be moved between a first position and a second position with respect to the fuel carrier, such that in the first position the at least one blocking area overlaps with the at least one lateral air inlet opening in a radial direction and in the second position the at least one blocking area overlaps with the at least one side air intake opening in the radial direction less than in the first position.
  • control ring If the control ring is in the first position, then an effective opening cross section of the side air inlet opening is reduced due to the overlap with the blocking area and air supply through the side air inlet openings is reduced or blocked. On the other hand, when the control ring is in the second position, the overlap is reduced and the effective opening area is larger than in the first position. Thus, by moving the control ring between the first position and the second position control or regulate a heat or temperature of the air exiting from the at least one lower air outlet opening.
  • a radial direction is one perpendicular from a rotation axis A1 (see Fig. 1a ) of the control ring emanating from or towards it.
  • the axis of rotation extends in the vertical and "top/bottom” or “top/bottom” are defined in relation to the vertical.
  • the axis of rotation goes through the middle of the fuel carrier cover, the control ring and the fuel carrier.
  • the basic shape of the fuel carrier cover, control ring and fuel carrier are essentially rotationally symmetrical with respect to the axis of rotation A1. However, embodiments are not limited thereto.
  • the translation may include a translation in a direction perpendicular to the bottom wall of the fuel tray. That is, the blocking area of the control ring can be made to overlap or less overlap with the side air inlet opening, for example, by sliding the control ring along the vertical.
  • the control ring can be arranged, for example, in the first position in the vertical direction at the same level as the side air inlet opening, so that the blocking area blocks the side air inlet opening and can be arranged in the second position in the vertical direction above or below the first position, so that the blocking area blocks the side air intake opening less or not at all.
  • the displacement can include a rotation about an axis of rotation extending perpendicular to the bottom wall of the fuel carrier. Ie by turning the control ring around this axis of rotation, the blocking area of the control ring is made to overlap with the side air inlet opening (first position) or the overlap between the blocking area and the side air inlet opening is reduced (second position).
  • the latter can take place, for example, in that the control ring has a passage area in the form of a cutout, which is brought into an overlap with the lateral air inlet opening in the radial direction.
  • control ring may also be slidable with respect to the fuel tray cover.
  • a cross section of the lateral air inlet openings can thus be adjusted without the fuel carrier cover having to be moved as well. This can simplify handling compared to the prior art.
  • control ring can further comprise at least one displacement implementation extension by means of which a user can perform the displacement of the control ring.
  • the shift bushing extension may be releasably attached to the control ring. This can simplify manufacture of the thermal regulation system.
  • the displacement bushing extension may further include a holding portion formed of a heat insulating material. This can prevent a user from being burned on it when performing the move.
  • the shifting passage extension can have a radially outwardly extending section which extends radially outwardly, for example through a recess in the side wall of the fuel carrier. This allows the control ring to be moved even when the fuel carrier cover is closed, i.e. when the fuel carrier cover is connected to the fuel carrier.
  • the recess can have a circumferential direction section which extends in a circumferential direction of the side wall.
  • the recess may further include an insertion portion extending to an upper edge of the side wall of the fuel tray.
  • the recess can have a second circumferential direction section which is arranged at a different distance from the bottom wall than the first circumferential direction section, and a connecting section which connects the first circumferential direction section to the second circumferential direction section.
  • the combustible material support cover can have a handle for holding the combustible material support cover and/or the fuel support can have a handle for holding the combustible material support.
  • the handle is preferably made of a heat-insulating material.
  • the fuel carrier can have at least one projection in the radial direction on its side wall and the control ring can be arranged to rest on this projection when it is attached to the fuel carrier.
  • the projection can be a peripheral projection or just segmented.
  • control ring can be arranged to be arranged inside the fuel carrier and according to another aspect, the control ring can be arranged to be arranged outside of the fuel carrier.
  • the combustible material carrier cover and the combustible material carrier can be connected by means of a positive fit.
  • the form fit can be such that it counteracts a displacement of the fuel carrier cover with respect to the fuel carrier in a plane parallel to the bottom wall and/or a translation of the fuel carrier cover with respect to the fuel carrier in a direction perpendicular to the bottom wall and/or counteracts a rotation of the fuel carrier cover with respect counteracts the fuel carrier about an axis of rotation extending perpendicularly to the bottom wall.
  • the fuel carrier cover may be configured to rest on an upper edge of the fuel carrier and may have at least one engagement element configured to engage at least one complementary engagement element of the fuel carrier.
  • the heat regulation system 1 shown for a hookah comprises a fuel carrier 2 for receiving fuel, a fuel carrier cover 3 for closing the fuel carrier 2 and a control ring 4 for controlling an air flow through at least one lateral air inlet opening 24.
  • the fuel can be coal, for example, which is brought to glow by means of a suitable heat source, e.g. fire or electric heater.
  • the fuel carrier 2 has a bottom wall 21 and a peripheral side wall 22 .
  • the bottom wall 21 is formed as a flat surface, for example, but is not limited thereto.
  • the side wall 21 can, for example, be essentially rotationally symmetrical to an axis of rotation A1 extending through the center point of the bottom wall 21 (see also 3a, b ).
  • Essentially rotationally symmetrical means here and below that it is sufficient for the basic shape to be rotationally symmetrical.
  • At least one lower air outlet opening 23 is provided in the bottom wall 21 and the at least one lateral air inlet opening is in the side wall 21 24 provided.
  • the at least one lower air inlet openings 23 and the lateral air inlet openings 24 have an elongated shape, for example.
  • the control ring 3 is formed separately from the fuel carrier cover 3 (and thus displaceable with respect to the fuel carrier cover 3) and has at least a blocking area 41 for blocking the air flow and a passage area 42 for letting the air flow through.
  • the control ring 4 is designed, for example, as a hollow cylinder with at least one cutout in the cylinder wall, with the cutout forming the at least one passage area 42 and an area of the cylinder wall without a cutout forming the at least one blocking area 41.
  • the hollow cylinder can, for example, be milled from one piece or formed by means of a band.
  • the material of the control ring 4 is preferably heat-resistant, for example a metal such as steel or aluminium.
  • An outer diameter of the control ring 3 is slightly smaller than an inner diameter of the fuel carrier 2, so that the control ring 4 can be arranged inside the fuel carrier 2 (see FIG Fig. 1b ), Such that the cylinder wall overlaps with the side wall 21 of the fuel carrier 2 in the radial direction.
  • the control ring 4 is designed in such a way that, when it is fitted within the fuel carrier 2, with its lower edge 44 (ie the edge facing the bottom wall 21) as in FIG Fig. 1b shown on at least one radially inwardly extending projection 25 of the side wall 22 of the fuel carrier 2 rests.
  • the projection 25 can, for example, be a circumferential projection and the control ring 4 can rest on an upper edge 251 (ie an edge facing the combustible material carrier cover 3) of the projection 25.
  • the control ring 4 is displaceable with respect to the fuel carrier 2 between a first position and a second position. More precisely, the control ring 4 can be rotated about an axis of rotation A1 (see Fig. 1a or 3a, b ) from a first position to a second position and vice versa.
  • the at least one blocking area 41 overlaps with the at least one lateral air inlet opening 24 in the radial direction (see FIG Fig. 1b , 2 B ).
  • the at least one blocking region 41 overlaps the at least one lateral air inlet opening 24 less in the radial direction than in the first position, for example not at all.
  • the at least one passage area 42 overlaps with the at least one lateral air inlet opening 24 in the radial direction.
  • an effective opening cross section of the at least one lateral air inlet opening 24 is smaller in the first position than in the second position. In the first position, less air is thus sucked in through the at least one lateral air inlet opening 24 than in the second position. As a result, proportionately more air flows over the fuel located in the fuel carrier 2 and the temperature of the combustion air increases. If, on the other hand, the control ring 4 is in the second position, then more cool ambient air is drawn into the fuel carrier 2 via the lateral air inlet openings 24, which leads to a reduction in the temperature of the combustion air.
  • the at least one blocking section 41 can completely close the at least one lateral air inlet opening 24 (see FIG Figure 2b ), so that the effective opening cross section of the at least one side air inlet opening 24 is minimal (e.g. zero) and in the second position the at least one passage area 42 can completely overlap with the at least one side air inlet opening 24 (see Figure 2a ), so that the effective opening cross section is at a maximum (corresponding, for example, to the actual opening cross section of the at least one lateral air inlet opening 24).
  • the control ring 4 can also have at least one displacement implementation extension 43, by means of which a user can perform the displacement of the control ring 4 between the first position and the second position.
  • the displacement bushing extension 43 may be attached to the wall of the control ring 4 and have a radially outwardly extending portion 431 .
  • the side wall 22 of the fuel tray 2 may further include a recess 27 through which the shift bushing extension 43 (and particularly the radially outwardly extending portion 431) extends to an exterior of the fuel tray 2 such that the shift bushing extension 43 can be accessed by a user even when the fuel tray is closed Fuel carrier cover 3 can be operated.
  • the recess 27 can also have a first circumferential direction section 271 which extends in a circumferential direction of the side wall 22 .
  • the direction of rotation generally corresponds to a direction of rotation of the control ring 4 when it is in its correct position in the fuel carrier 2 .
  • a length of the circumferential direction section 271 may be dimensioned such that when the circumferential direction shift bushing extension 43 touches a first edge 2711 of the first circumferential direction section 271, the control ring 4 is in the first position (see FIG Figure 2b ), and when the shift operation extension 43 touches a second edge 2712 of the first circumferential direction portion 271, which is opposite to the first edge 2711 in the circumferential direction, the control ring 4 is in the second position (see Figure 2a ).
  • This means that the control ring 4 can be displaced between the first position and the second position by displacing the displacement passage extension 43 within the recess 27 in the circumferential direction.
  • the recess 27 can also have an insertion section 272 which extends, for example vertically upwards, to an upper edge 221 of the side wall 22 of the fuel carrier 2 .
  • the insertion portion 272 is dimensioned such that the outwardly extending portion 431 of the shift passage extension 43 can be inserted through it into the first circumferential direction portion 271 .
  • the displacement performing extension 43 may further include a holding portion configured to be held by a user while performing the displacement of the control ring 4 .
  • the holding portion may be formed of a thermally insulating material or coated with a thermally insulating material (e.g., a heat-resistant polymer or plastic) (see Fig 3a, b ).
  • the holding portion may also be knurled to improve handling.
  • the fuel carrier cover 3 is designed to rest on an upper edge 221 of the fuel carrier 2 .
  • the combustible material carrier cover 3 can be essentially rotationally symmetrical to the axis of rotation A1 extending through the center point of the bottom wall 21 .
  • the fuel carrier cover 3 can be dome-shaped, for example.
  • the fuel carrier 2 and the fuel carrier cover 3 can be set up in such a way that they can be connected to one another by means of a positive fit.
  • the side wall 22 of the fuel carrier 2 can have at least one first engagement element 29 in an upper area (i.e.
  • the fuel carrier cover 3 can have at least a second engagement element in a lower area (ie in an area facing the fuel carrier 2). Having engagement element 33, which is complementary to the first engagement element 29, such that it can come with the first engagement element 29 in engagement.
  • the first engagement element 29 can be a radially inwardly directed projection and the second engagement element 33 can be a radially outwardly directed projection on a section of the fuel carrier cover 3 that extends into the interior of the fuel carrier 2, which, when the fuel carrier cover 3 is on an upper edge 221 of the fuel carrier 2 rests, comes into contact from below with the inwardly pointing projection, such that a form fit is created which prevents a displacement of the fuel carrier cover 3 with respect to the fuel carrier 2 in a direction perpendicular to the bottom wall 21 of the fuel carrier (e.g. the direction in the the axis of rotation A1 extends) counteracts.
  • the at least one first engagement element 29 can, as in Figures 1a and 1b shown, comprise, for example, three first engagement elements 29, which are arranged at the same distance from one another in the circumferential direction of the side wall 22 (or the direction of rotation defined by the axis of rotation A1), and the at least one second engagement element 33 can, as in Fig.la and 1b shown, for example, comprise three second engagement elements 33, which are arranged at the same distance from one another in the direction of rotation (or the direction of rotation defined by the axis of rotation A1).
  • a first handle 28 for holding the fuel carrier 2 can be provided on the fuel carrier 2
  • a second handle 38 for holding the fuel carrier cover 3 can be provided on the fuel carrier cover 3
  • the handle 28 of the fuel carrier 2 and/or the handle 38 of the fuel carrier cover 3 can consist of a heat-insulating material or be covered with such a material in order to prevent the user from being burned, for example when removing the fuel carrier cover.
  • the first and second holding handles 28, 38 may be formed so as to overlap in a projection from above (i.e., along the direction defined by the rotation axis A1) in a state where the fuel tray cover is locked to the fuel tray 2. As a result, handling of the heat regulation system 1 can be improved.
  • Figures 3a and 3b 12 and 12 show a top view and a bottom view, respectively, of a modification of the water pipe heat regulation system described above. It is modified in that the displacement bushing extension 43 has a knurled retaining portion 432 .
  • the heat regulation system 1 shown for a hookah according to a second embodiment essentially corresponds to the heat regulation system 1 according to the first embodiment.
  • the second embodiment differs from the first embodiment in that the displacement bushing extension 43 is detachably attached to the control ring 4, for example by means of a screw connection. This has the advantage that when inserting the control ring 4 into the fuel carrier 2, the displacement lead-through extension 43 can be removed, so that the introduction section 272 described in the first exemplary embodiment can be dispensed with.
  • the control ring 4 is displaced from the first position into the second position and vice versa by means of a rotation about an axis of rotation A1 extending perpendicularly to the bottom wall 21 of the fuel carrier 2 .
  • the third exemplary embodiment described in the third exemplary embodiment described can, instead of or in addition to the rotation, also include a translation in a direction perpendicular to the bottom wall 21 of the fuel carrier 2 (e.g. along the axis A1 from Fig. 1a ).
  • the control ring 4 can be, for example, a hollow cylinder which, in the first position, is arranged in the vertical direction (i.e.
  • the cylinder wall of the control ring 4 is thus a blocking area 41 for blocking the air flow.
  • the control ring 4 it is not necessary in this configuration for the control ring 4 to have a passage area 42 in the form of a recess.
  • the side wall 21 of the fuel carrier 2 can have a recess 27 with a first circumferential section 271 extending in the circumferential direction of the side wall 22 and a second circumferential section 271 extending in the circumferential direction of the Having side wall 22 extending circumferential direction section 273, which are arranged at a different distance from the bottom wall 22 of the fuel carrier 2 and connected to each other via a connecting portion 274.
  • the distance between the first circumferential direction section 271 and the bottom wall 22 of the fuel carrier 2 is selected, for example, so that the control ring 4 is in the first position when a
  • the section 431 of the at least one displacement leadthrough extension 43 which extends radially outwards through a recess 27 in the side wall 22 of the fuel carrier 2, rests on a lower edge 2713 of the first circumferential direction section 271 (see Figures 6a and b ).
  • the distance between the second circumferential direction section 274 and the bottom wall 22 of the fuel carrier 2 is selected, for example, so that the control ring 4 is in the second position when a section 431 extending radially outwards through a recess 27 in the side wall 22 of the fuel carrier 2 the at least one displacement leadthrough extension 43 rests on a lower edge 2733 of the second circumferential direction section 273 (see Figures 6c and d ).
  • the thermal regulation system 1 can also be set up such that the control ring 4 rests either in the first position or the second position on the bottom wall 22 or on a radially extending projection 25 of the side wall 22 (not shown). A first circumferential direction section 271 is then sufficient.
  • control ring 4 is designed to be arranged inside the fuel carrier 2 (internal control ring). However, there is also the possibility of providing the control ring 4 outside of the fuel carrier 2 (external control ring). Instead of on a radially inwardly extending projection 25 of the side wall 22 of the fuel carrier 2, the control ring 4 would then rest on a radially outwardly extending projection of the side wall 22 of the fuel carrier 2 (not shown).
  • an internal control ring 4 can also rest on the bottom wall 21 of the fuel carrier 2.
  • the first and second engagement elements 29, 33 for connecting the fuel carrier cover 3 to the fuel carrier 2 can also be designed differently than described above.
  • the at least one first engagement element 29 can be a downward-pointing depression (i.e. extending towards the bottom wall 21) in an upper edge 221 of the side wall 22 of the fuel carrier 2
  • the at least one second engagement element 33 can be a complementary downward-pointing projection on the fuel carrier cover 3, which is designed to be plugged into the recess to form a plug-in connection.
  • a form fit is created which counteracts a displacement of the fuel carrier cover 3 with respect to the fuel carrier 2 in a plane parallel to the bottom wall 21, and - depending on whether the projection comes into contact with a wall delimiting the recess in the direction of rotation - a rotation of the Fuel carrier cover 3 counteracts with respect to the fuel carrier 2 about an axis of rotation A1 extending perpendicularly to the bottom wall 21 .
  • the latter would not be the case, for example, if the depression is designed as a circumferential groove, because then there is no wall delimiting the depression in the circumferential direction.
  • a screw connection could also be formed.
  • the first engagement element 29 can be provided with an internal thread and the second engagement element 33 can be provided with a complementary external thread, so that the fuel carrier cover 3 and the fuel carrier can be screwed together.
  • a form fit is created which counteracts a displacement of the fuel carrier cover 3 with respect to the fuel carrier 2 in a plane parallel to the base wall 21 and in a direction perpendicular to the base wall 21 .
  • what has been described in relation to the first engagement element 29 can be applied to the second engagement element 33 and vice versa.
  • control ring 3 was shown with only one displacement bushing extension. However, it may also have a plurality of shift passage extensions circumferentially arranged at regular or irregular intervals. In particular in the case of an embodiment according to the third exemplary embodiment, it can be advantageous to have several Provide displacement implementation extensions. For ease of handling, the shift bushing extensions may be connected together at ends of their radially outwardly extending portions.
  • the number, shape and arrangement of the side air inlet opening 24, lower air outlet opening 23 and upper air inlet opening 31 are not limited to the configurations shown in the exemplary embodiments, but can deviate from them.
  • the recess 27 can also be provided in the fuel carrier cover 3 instead of in the side wall 22 of the fuel carrier.
  • the fuel carrier 2 has been shown and described with a flat bottom wall 21 .
  • the shape of the fuel carrier 2 is not limited to this, the fuel carrier can also have the shape of a spherical segment, for example.
  • a direction perpendicular to the bottom wall 21 of the fuel carrier 2 is the direction in which the axis of rotation, with respect to which the bottom wall 22 is essentially rotationally symmetrical, extends.

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EP22193891.3A 2021-11-11 2022-09-05 Système de régulation de la chaleur pour une conduite d'eau Pending EP4201232A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE202021106167.7U DE202021106167U1 (de) 2021-11-11 2021-11-11 Wärmeregulationssystem für eine Wasserpfeife

Publications (1)

Publication Number Publication Date
EP4201232A1 true EP4201232A1 (fr) 2023-06-28

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP22193891.3A Pending EP4201232A1 (fr) 2021-11-11 2022-09-05 Système de régulation de la chaleur pour une conduite d'eau

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EP (1) EP4201232A1 (fr)
DE (1) DE202021106167U1 (fr)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016081920A1 (fr) * 2014-11-20 2016-05-26 Kaloud, Inc. Foyer de narguilé et accessoire de gestion de la chaleur
US20160198762A1 (en) * 2012-06-06 2016-07-14 Kaloud, Inc. Hookah heat management accessory
DE202019005307U1 (de) * 2019-01-30 2020-02-21 Schmidt Innovations GmbH Wärmeregulationssystem für eine Wasserpfeife
DE102019125344B3 (de) * 2019-09-20 2021-01-21 Shisha Cloud GmbH Kaminaufsatz für einen Wasserpfeifenkopf
DE202021102986U1 (de) * 2021-05-31 2021-06-29 Cem Hamdi Bozkurt Tabakaufnahmeteil und mit einem Tabakaufnahmeteil ausgestattete Wasserpfeife

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160198762A1 (en) * 2012-06-06 2016-07-14 Kaloud, Inc. Hookah heat management accessory
WO2016081920A1 (fr) * 2014-11-20 2016-05-26 Kaloud, Inc. Foyer de narguilé et accessoire de gestion de la chaleur
DE202019005307U1 (de) * 2019-01-30 2020-02-21 Schmidt Innovations GmbH Wärmeregulationssystem für eine Wasserpfeife
DE102019125344B3 (de) * 2019-09-20 2021-01-21 Shisha Cloud GmbH Kaminaufsatz für einen Wasserpfeifenkopf
DE202021102986U1 (de) * 2021-05-31 2021-06-29 Cem Hamdi Bozkurt Tabakaufnahmeteil und mit einem Tabakaufnahmeteil ausgestattete Wasserpfeife

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