SHELL-AND-TUBE APPARATUS WITH BAFFLES
20200049412 ยท 2020-02-13
Assignee
Inventors
Cpc classification
F28F9/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F9/0131
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F2265/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F9/013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D7/1607
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F28D7/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F9/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Shell-and-tube apparatus comprising a plurality of baffles (5) which are arranged along the tube bundle, perpendicular to an axis of the tube bundle and passed through by the said tubes, wherein each baffle is an essentially flat body having openings (11) through which the tubes pass, and in the region of said openings (11) the baffle comprises tabs (12) which protrude from the surface of said baffle.
Claims
1. Shell-and-tube apparatus comprising a plurality of baffles (5) which are arranged along the tube bundle, perpendicular to an axis (20) of the tube bundle (3) and passed through by said tubes, characterized in that: each baffle is an essentially flat body and comprises a metal plate (10) with openings (11) for the passage of the tubes through said baffle; at said openings (11) the baffle comprises tabs which protrude away from the metal plate, said tabs are configured to operate as elastic supports for the tubes and/or to operate as fluid-dynamic tabs adapted to deviate a fluid traversing the shell side of the apparatus.
2. Apparatus according to claim 1, wherein all tabs of each baffle extend from the same side (13) of the respective baffle.
3. Apparatus according to claim 1 or 2, wherein the shell-side gaseous flow is axial or predominantly axial.
4. Apparatus according to claim 3, wherein at least some of said tabs are fluid-dynamic tabs adapted to deviate the shell-side gaseous flow from the main axial direction.
5. Apparatus according to any of claims 1 to 4 comprising first baffles (5a) having a first configuration of tabs and second baffles (5b) having a second configuration of tabs, wherein the first baffles and the second baffles alternate along at least a part of the tube bundle and wherein said first configuration and second configuration of tabs are conjugate to impart to the shell-side flow a movement component transverse to the axis (20) of the tube bundle (3).
6. Apparatus according to claim 5, wherein: the first baffles (5a) have tabs (112a) configured to direct the shell-side flow in a first direction forming, in a reference plane, a first angle (a1) with the axis of the tubes, the second baffles (5b) have tabs (112b) configured to direct the shell-side flow in a second direction (2a) forming, in said reference plane, a second angle with the axis of the tubes, said second angle having a sign opposite to the first angle, thus obtaining shell-side flow lines which, passing through the baffles, are alternately deviated in different directions.
7. Apparatus according to claim 6, wherein the shell-side flow lines are substantially sinusoidal.
8. Apparatus according to claim 5, wherein the first baffles (5a) and the second baffles (5b) comprise tabs (212a, 212b) directed so as to impart to the shell-side fluid a substantially helical flow about the axis of the tube bundle.
9. Apparatus according to claim 8, wherein the tabs (212a, 212b) protrude from opposite sides (13a, 13b) of the respective first baffles and second baffles (5a, 5b) and the baffle tabs facing each other are angularly offset.
10. Apparatus according to any one of the preceding claims, wherein at least one baffle comprises tabs of varying configuration.
11. Apparatus according to any one of the preceding claims, wherein each baffle occupies all or substantially all of the cross-sectional area of the shell side, or only a portion of said area.
12. Apparatus according to any one of the preceding claims, wherein tabs of adjacent baffles rest on opposite sides on each tube.
13. Apparatus according to any one of the preceding claims, wherein the baffles are formed in such a way that: each opening for one or more tubes comprises at least a first region suitable to receive the tube or tubes with play and a second region suitable to receive the tube or tubes with less play or with substantially zero play; each tube of the bundle is received in a first region of a respective seat when the baffle is in a so-called assembly position and is received in a second region of the seat when the baffle is in an operating position.
14. Apparatus according to claim 13, wherein the tabs are positioned relative to the openings (11) so that the tubes move towards said tabs when the baffles are arranged in the operating position, such that the tabs define elastic supports for the tubes when the baffles are in the operating position.
15. Apparatus according to any one of the preceding claims, wherein the tabs are formed by sheet-metal elements mounted on the metal plate in correspondence of the openings.
16. Apparatus according to any one of claims 1 to 14, wherein the openings are punched or cut in the metal plate, and said tabs are formed by strips of material of the metal plate generated by the cutting or punching of the openings, and suitably bent.
17. Apparatus according to any one of the preceding claims, wherein the baffles comprise an outer reinforcing ring having a thickness greater than the thickness of the metal plate.
Description
DESCRIPTION OF THE FIGURES
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DETAILED DESCRIPTION
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[0065] Each of the baffles 5 (
[0066] The openings 11 and the tabs 12 may be formed using various methods. For example: the openings 11 are obtained by means of partial punching and the tabs 12 are formed by strips of the material of the disc 10, which instead of being removed, remain attached to the disc; the openings 11 may be obtained using a suitable cutting method, preferably laser or water-jet cutting, and subsequent bending of strips to form the tabs 12; the tabs 12 are thin sheet-metal elements which are mounted on the disc 10. These examples are provided by way of a non-limiting example and other manufacturing methods are possible.
[0067] Each opening 11 is passed through by a tube 4 or several tubes 4 depending on the specific embodiment.
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[0069] For this purpose, for example, the openings 11 have an essentially trapezoidal form comprising a base portion suitable to receive a tube with play, and flanks converging towards a tapered head portion for locking the tube. Such an embodiment is also shown in
[0070] The set of baffles 5 comprises first baffles 5a having a first configuration of tabs 112a and second baffles 6b having a second configuration of tabs 112b in which the first baffles 5a and the second baffles 5b alternate with each other in the longitudinal direction of the tube bundle. The figure also shows a tube plate 6. In the example the baffles 5a and 5b can be locked on the tube bundle by means of the linear displacements +f, f, respectively.
[0071] The tabs 112a with said first configuration protrude from the respective baffles 5a in a direction forming, in a reference plane, a first angle a1 with the direction of the direction of the axis 14 of the tubes and the axis 20 of the tube bundle 3.
[0072] The tabs 112b with said second configuration protrude from the respective baffles 5b in a second direction forming with said direction of the axes 14 and 20, in the same reference plane, a second angle a2 with a sign opposite to that of the first angle a1 (
[0073] Preferably said second angle is equal and opposite to said first angle, i.e. a2=a1.
[0074] More advantageously, the absolute value (modulus) of said first angle a1 and second angle a2 is comprised between 30 and 60 degrees, and is preferably 45 degrees.
[0075] Said reference plane is for example the plane shown in
[0076] With reference to
[0077] As a result of this arrangement, as shown in particular in
[0078] In
[0079] In
[0080] It can be understood that the tabs 112a, 112b have both a fluid dynamic function, determining sinusoidal flow lines, and a structural function of elastically supporting the tubes 4, compensating for play due to the constructional tolerances, and preventing vibrations.
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[0083] In said twist-lock embodiment, the set of baffles 5 advantageously comprises first baffles 5a and second baffles 5b with tabs 212a, 212b configured to impart a helical motion to the shell-side fluid.
[0084] In greater detail, according to the shown embodiment, the tabs 212a, 212b extend from opposite sides of the baffles, for example the tabs 212a extend from front sides 13a of the baffles 5a and the tabs 212b extend from rear sides 13b of the baffles 5b. The tabs 212a, 212b are also angularly offset. As a result of this arrangement, as shown in
[0085] In
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[0092] Openings with an essentially trapezoidal form as shown in
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[0094] It should be noted that the constructional form shown in
[0095] It should be finally noted that embodiments of the invention, for example similar to embodiments of