LU92841B1 - Flexible seal for a regenerative rotary preheating device - Google Patents
Flexible seal for a regenerative rotary preheating device Download PDFInfo
- Publication number
- LU92841B1 LU92841B1 LU92841A LU92841A LU92841B1 LU 92841 B1 LU92841 B1 LU 92841B1 LU 92841 A LU92841 A LU 92841A LU 92841 A LU92841 A LU 92841A LU 92841 B1 LU92841 B1 LU 92841B1
- Authority
- LU
- Luxembourg
- Prior art keywords
- blade
- assembly
- base section
- leaf
- distal end
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
- F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
- F28D19/047—Sealing means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D19/00—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
- F28D19/04—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
- F28D19/041—Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier with axial flow through the intermediate heat-transfer medium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2230/00—Sealing means
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
Abstract
A seal assembly includes a leaf assembly and a supplemental leaf assembly. The leaf assembly includes a first leaf having a first base section. The first base section defines a first fastening area for securing the first leaf to a diaphragm of the preheater. The first leaf has a first elongate section extending away from the first base section and terminating at a first distal end thereof. The leaf assembly further includes a second leaf that engages a portion of the first leaf. The second leaf has a second base section. The second base section defines a second fastening area for securing the second leaf to the diaphragm. The second leaf has a second elongate section extending away from the second base section and terminating at a second distal end thereof. The supplemental leaf assembly is secured to the first leaf and slidingly engaging the second leaf
Description
FLEXIBLE SEAL FOR A ROTARY REGENERATIVE PREHEATER
Technical Field [0001] This invention relates to a flexible seal for a rotary regenerative preheater, and more particularly to a flexible seal having multiple leafs.
Background [0002] As shown in FIG. 1, a rotary regenerative air preheater (hereinafter referred to as the “preheater”) is generally designated by the numeral 10. The preheater 10 includes a rotor assembly 12 rotatably mounted on a rotor post 16. The rotor assembly 12 is positioned in and rotates relative to a housing 14. For example, the rotor assembly 12 is rotatable about an axis A of the rotor post 16 in the direction indicated by the arrow R. The rotor assembly 12 includes partitions 18 (e.g., diaphragms) extending radially from the rotor post 16 to an outer periphery of the rotor assembly 12. Adjacent pairs of the partitions 18 define respective compartments 20 for receiving a heat transfer assembly 1000. Each of the heat transfer assemblies 1000 include a plurality of heat transfer sheets 100 and/or 200 stacked upon one another.
[0003] As shown in FIG. 1, preheater 10 is a bisector configuration in which the housing 14 includes a flue gas inlet duct 22 and a flue gas outlet duct 24 for channeling the flow of heated flue gases through the preheater 10. The housing 14 further includes an air inlet duct 26 and an air outlet duct 28 for channeling the flow of combustion air through the preheater 10. The preheater 10 includes an upper sector plate 30A extending across the housing 14 adjacent to an upper face of the rotor assembly 12. The preheater 10 includes a lower sector plate 30B extending across the housing 14 adjacent to lower face of the rotor assembly 12. The upper sector plate 30A extends between and is joined to the flue gas inlet duct 22 and the air outlet duct 28. The lower sector plate 30B extends between and is joined to the flue gas outlet duct 24 and the air inlet duct 26. The upper and lower sector plates 30A, 30B, respectively, are joined to one another by a circumferential plate 30C. The upper sector plate 30A and the lower sector plate 30B divide the preheater 10 into an air sector 32 and a gas sector 34.
[0004] As illustrated in FIG. 1, the arrows marked ‘A’ indicate the direction of a flue gas stream 36 through the gas sector 34 of the rotor assembly 12. The arrows marked ‘B’ indicate the direction of a combustion air stream 38 through the air sector 32 of the rotor assembly 12. The flue gas stream 36 enters through the flue gas inlet duct 22 and transfers heat to the heat transfer assembly 1000 mounted in the compartments 20. The heated heat transfer assembly 1000 is rotated into the air sector 32 of the preheater 10. Heat stored in the heat transfer assembly 1000 is then transferred to the combustion air stream 38 entering through the air inlet duct 26. Thus, the heat absorbed from the hot flue gas stream 36 entering into the preheater 10 is utilized for heating the heat transfer assemblies 1000, which in turn heats the combustion air stream 38 entering the preheater 10.
[0005] As shown in FIG. 2, a prior art seal 40 extends axially from (i.e., parallel to the axis A) and radially along an edge of each of the diaphragms 18 towards the sector plate 30A. Another seal 40 extends axially from and radially along an opposite side of each of the diaphragms 18 towards the sector plate 30B (only one seal 40 shown in FIG. 1). The seal 40 typically includes a flexible seal leaf 42 having a base portion 42B that is positioned between an L-shaped backing bar 43 and an elongate holding bar 41. A base portion 4 IB of the holding bar 41, the base portion 42B of the flexible seal 42 and a base portion 43B of the backing bar 43 are secured by a plurality of bolts 45 and nuts 46 between a spacer bar 44 and the diaphragm 18, radially along a length of the diaphragm 18.
[0006] During operation of the preheater 10, a surface 31’ of the sector plates 30A and 30B is spaced apart from a distal end of the seal 40. However, during start-up conditions when the preheater 10 and ducts 22, 24, 26 and 28 are relatively cold, the surface 31 of the sector plates 30A and 30B slidingly engage the respective seal 40. Such sliding engagement causes the flexible seal leaf 42 to wear and results in bypass leakage between the air sector 32 and the gas sector 34. In addition, through laboratory testing, the inventors have surprisingly found that such sliding engagement of the seal 40 with the respective sector plate 30A and 30B results in oscillatory vibration of the seal 40, as indicated by the arrow V, causing fatigue failure thereof.
In addition, the inventors have discovered that because the seal 40 is mounted on a leading edge of the diaphragm 18, the edge of the diaphragm 18 acts as an abrupt fulcrum 47 upon which the seal 40 is bent over and causes stress concentrations at the mating portion of the seal 40. Such stress concentrations cause premature failure of the seal 40.
Summary of the Invention [0007] There is disclosed herein a seal assembly for a rotary preheater. The seal assembly includes a leaf assembly and a supplemental leaf assembly. The leaf assembly includes a first leaf having a first base section. The first base section defines a first fastening area for securing the first leaf to a diaphragm of the preheater. The first leaf has a first elongate section extending away from the first base section and terminating at a first distal end thereof. The leaf assembly further includes a second leaf that engages a portion of the first leaf. The second leaf has a second base section. The second base section defines a second fastening area for seeming the second leaf to the diaphragm. The second leaf has a second elongate section extending away from the second base section and terminating at a second distal end thereof. The supplemental leaf assembly is secured to ±e first leaf and slidingly engaging the second leaf.
[0008] In one embodiment, the second distal end of the second leaf terminates between the first distal end and the first base section of the first leaf.
[0009] In one embodiment, the supplemental leaf assembly includes a spacer secured to the first leaf and a third leaf secured to the spacer, for example by one or more rivets or spot welds. The third leaf slidingly engages the second leaf.
[0010] In one embodiment, the second distal end of the second leaf terminates between the first distal end and the first base section; the supplemental leaf assembly includes a spacer secured to the first leaf and a third leaf secured to the spacer, the third leaf slidingly engages the second leaf; and the spacer is positioned between the first leaf and the third leaf, the spacer is spaced apart from the second distal end thereby defining a gap between the spacer and the second distal end to accommodate movement of the spacer relative to the second distal end. [0011] In one embodiment, the seal assembly includes a one or more displacement members. Each of the displacement members has a first engagement portion configured to displace a portion of the leaf assembly a predetermined distance. In one embodiment, the each of displacement members has an L-shaped configuration defining a first leg and a second leg. The first leg defines a third base portion that is secured to the diaphragm and the second leg has the engagement portion thereon. The displacement members are arranged to establish a predefined contour of the leaf assembly. The predetermined contour is configured to compensate for movement of the preheater during operation.
[0012] In one embodiment, the seal assembly incudes a strip (e.g., guard and/or limiter) having fourth base section engaging the second base section such that the second base section is positioned between ±e first base section and ±e fourth base section. The strip defines a deflector section extending away from ±e fourth base section and away from the second leaf. [0013] There is also disclosed herein a preheater assembly. The preheater assembly includes a rotor assembly rotatably mounted on a rotor post and disposed in a housing. The rotor assembly defines diaphragms extending radially from the rotor post to an outer periphery of the rotor assembly. Adjacent pairs of the diaphragms define respective compartments for receiving a heat transfer assembly. Each of the heat transfer assemblies include a plurality of heat transfer sheets stacked upon one another. The housing including a flue gas inlet duct and a flue gas outlet duct for channeling the flow of heated flue gases through the preheater The housing also includes an air inlet duct and an air outlet duct for channeling the flow of combustion air through the preheater. The preheater includes an upper sector plate extending across the housing adjacent to an upper face of the rotor assembly and a lower sector plate extending across the housing adjacent to lower face of the rotor assembly. The upper sector plate extends between and is joined to ±e flue gas inlet duct and the air outlet duct; and the lower sector plate extends between and is joined to the flue gas outlet duct and the air inlet duct. The upper and lower sector plates, respectively, are joined to one another by a circumferential plate. The upper sector plate and/or the lower sector plate define a leading edge and a trailing edge. One or more of the leading edge and the trailing edge defines a ramped configuration. A seal assembly is positioned on an axial edge of each diaphragm. The seal assembly includes a leaf assembly and a supplemental leaf assembly. The leaf assembly includes a first leaf having a first base section. The first base section defines a first fastening area for securing the first leaf to a diaphragm of the preheater. The first leaf has a first elongate section extending away from the first base section and terminating at a first distal end thereof. The leaf assembly further includes a second leaf that engages a portion of the first leaf. The second leaf has a second base section. The second base section defines a second fastening area for securing the second leaf to the diaphragm. The second leaf has a second elongate section extending away from the second base section and terminating at a second distal end thereof. The supplemental leaf assembly is secured to the first leaf and slidingly engages the second leaf. A portion of the first leaf slidingly engages the leading edge and disengages the trailing edge.
[0014] In one embodiment, the second distal end terminates between the first distal end and the first base section.
[0015] In one embodiment, the supplemental leaf assembly includes a spacer secured to the first leaf and a third leaf secured to the spacer. The third leaf slidingly engages the second leaf.
Brief Description of the Drawings [0016] FIG. 1 is a perspective view of a preheater shown in a partial cut away view; [0017] FIG. 2 is a cross sectional view of a prior art seal secured to a diaphragm of a preheater; [0018] FIG. 3 is a plan view of the seal assembly of the present invention viewed from a trailing side of the diaphragm; [0019] FIG. 4 is a plan view of the seal assembly of the present invention viewed from a leading side of the diaphragm; [0020] FIG. 5 is a top view of the seal assembly of FIG. 4 taken across line 5-5 of FIG. 4; [0021] FIG. 6 is a cross sectional view of the seal assembly of FIG. 3 taken across line 6-6 of FIG. 4; [0022] FIG. 7 is another embodiment of the seal assembly of FIG. 6 shown with a sector plate having a ramped configuration; [0023] FIG. 8 is another embodiment of the seal assembly of FIG. 7 wherein the ramped configuration includes a ramp attachment secured to each of the leading and trailing edges of the sector plates; [0024] FIG. 9 is a cross sectional view of a portion of another embodiment of the seal assembly of FIG. 6 and having one leaf extending outwardly from the other leaves; [0025] FIG. 10 is a cross sectional view of a portion of another embodiment of the seal assembly of FIG. 6 wherein the spacer is formed by a bend in a first leaf; [0026] FIG. 11 is a cross sectional view of a portion of another embodiment of the seal assembly of FIG. 6 wherein the spacer is formed by a rivets and spacer rings; and [0027] FIG. 12 is a cross sectional view of a portion of another embodiment of the seal assembly of FIG. 6 wherein the spacer is formed by a bend in a second leaf.
Detailed Description [0028] As shown in FIG. 6, a seal assembly of the present invention is generally designated by the numeral 140. One of the seal assemblies 140 is secured to opposing axially edges of each of the diaphragms 18 of the bisector type preheater of FIG. 1 by a suitable fastener system such as a plurality of bolts 145 and nuts 146. However, other methods of fastening the seal assemblies 140 to the diaphragms 18 may be employed such as but not limited to welding and brazing. Each of the seal assemblies 140 are a generally elongate member that extends between the rotor post 16 and a radially outward peripheral edge of the diaphragm 18, as shown in FIGS. 3 and 4. While the seal assembly 140 is described as being employed in a bisector type preheater, the present invention is not limited in this regard as the seal assembly may be employed in a tri-sector or quad sector preheater, without departing from the broader aspects disclosed herein.
[0029] Referring to FIG. 6, each of the seal assemblies 140 includes a leaf assembly 50 having a first leaf 52 having a first base section 52B. The first base section 52B defines a first fastening area, for example, a flat section and a bore extending therethrough for receiving one of the bolts 145 for securing the first leaf 52 to the diaphragm 18 of the preheater 10 of FIG. 1. The first leaf 52 has a first elongate section 52L extending away from the first base section 52B and terminating at a first distal end 52D thereof.
[0030] Referring to FIG. 6, each of the seal assemblies 140 includes a second leaf 54 engaging a portion of the first leaf 52 and having a second base section 54B. The second base section 54B defines a second fastening area, for example, a flat section and a bore extending therethrough for receiving one of the bolts 145 for securing the second leaf 54 to the diaphragm 18 of the preheater 10 of FIG. 1. The second leaf 54 has a second elongate section 54L extending away from the second base section 54B and terminating at a second distal end 54D thereof. The second distal end 54D terminates along a length of the first leaf 52 between the first distal end 52D and the first base section 52B of the first leaf 52.
[0031] As shown in FIG. 6, each of the seal assemblies 140 includes a supplemental leaf assembly 60 secured to (e.g., via suitable fastening structures 61 such as rivets or spot welds) the first leaf 52 and slidingly engages the second leaf 54. The supplemental leaf assembly 60 includes a spacer 62 (e.g., a spacer leaf) secured to (e.g., via the fastening structures 61) the first leaf 52. The spacer 62 defines a distal end 62D. The supplemental leaf assembly 60 includes a third leaf 64 secured to (e.g., via the fastening structures 61) the spacer 62. The third leaf 64 slidingly engages a portion of the second leaf 54. The third leaf 64 defines a third distal end 64D. The spacer 62 is positioned between the first leaf 52 and the third leaf 64. The spacer 62 is spaced apart from the second distal end 54D thereby defining a gap G between the spacer 62 and the second distal end 54D to accommodate movement of the spacer 62 relative to the second distal end 54D. While the spacer 62 is described and shown in FIG. 6 as being a leaf, the present invention is not limited in this regard as other spacer configurations may be employed including but not limited to: 1) a spacer 162L formed as a leg as a result of a bend 152D in ±e first leaf 152 as shown in FIG. 10; 2) a spacer ring 262B disposed around a rivet 261 and positioned between the first leaf 252 and a third leaf 264 as shown in FIG. 11; and 3) a spacer 362L formed as a leg as a result of a bend 364D in the third leaf 364 as shown in FIG. 12. The inventors have surprisingly discovered that the sliding engagement of the sliding engagement of the third leaf 64 with the portion of the second leaf 54 increases the performance and life of the seal assembly 140 by reducing vibrations compared to prior art single leaf seals or improvements with only two leaves.
[0032] As shown in FIG. 6, in one embodiment the distal ends 52D, 62D and 64D are aligned with one another. In the configuration shown in FIG. 6, the distal end 52D of the first leaf 52 is shown slidingly engaging the surface 31 of the sector plate 30A during reduced (e.g., 30 percent load or less) or zero load operation. Another of the spacers 62 of a seal assembly 140, positioned on an opposite side of the diaphragm 18, slidingly engages the surface 31 of the sector plate 30B. For loads greater than 30 percent the distal end 54D is spaced apart from the surface 31’ of the sector plate 30A by a gap G1 that reduces hot end radial seal gap by fifty percent at full load compared to the prior art seal assemblies 40.
[0033] While in FIG. 6 the distal ends 52D, 62D and 64D are aligned with one another, the present invention is not limited in this regard as one or more of the distal ends 52D, 62D and 64D may extend outwardly from one another, as shown in FIG. 9 wherein the distal end 62D extends outwardly from the distal ends 52D and 64D. In one embodiment portions of the spacer 62 on and adjacent to the distal end 62 D are formed of a wear resistant configuration such as but not limited to a surface hardfacing weld overlay (e.g., a cobalt based weld material), a case hardened layer (e.g., nitriding, carburizing or other diffusion type hardening) and a precipitation hardened material. The spacer 62 of slidingly engages the surface 31 of the sector plate 30A.
[0034] In one embodiment, the first leaf 52, the second leaf 54, the third leaf 62 and/or the fourth leaf 64 are manufactured from an austenitic stainless steel, for example a 301 stainless steel. In one embodiment the first leaf 52, the second leaf 54, the third leaf 62 and/or the fourth leaf 64 are about 0.02 to 0.025 inches thick.
[0035] As shown in FIG. 4, the seal assembly 140 includes three displacement members 70 having side edges 70E that abut one another. While three displacement members 70 are shown the present invention is not limited in this regard as the displacement members 70 may be formed in one integral piece or any number of segments to facilitate installation. In one embodiment illustrated in FIG. 6, each of the plurality of displacement members 70 has an L-shaped configuration defining a first leg 71 and a second leg 72. The first leg defines a third base section 7IB. The third base section 7IB defines a third fastening area, for example, a flat section and a bore extending therethrough for receiving one of the bolts 145 for securing the displacement member 70 to the diaphragm 18 of the preheater 10 of FIG. 1.
[0036] As shown in FIG. 5, each of second legs 72 defines an engagement portion 72T configured to engage a surface 52F of the first leaf 52 and to displace a portion of the leaf assembly 50 a predetermined distance, as described further herein. Each of the engagement portions 72T have a contoured edge configuration. For example, the engagement portion 72T of the two radially outwardly positioned displacement members 70 have a linear tapered edge; and the engagement portion 72T’ of the radially inner most positioned displacement member 70 has an arcuate edge that is complementary in shape to the surface 52F of the first leaf 52. However, any of the displacement members 70 may employ an arcuate edge and/or a linear tapered edge. [0037] As shown in FIG. 6 the second leg 72 has a length LN (e.g., L7 shown in FIG. 6, Ll-L10 shown in FIG. 5) extending between the first leg 71 and the engagement portion 72T. As shown in FIG. 5 each of L1-L10 are of a different magnitude and displace the leaf assembly 50 a different magnitude. For example, the lengths L1-L10 progressively increase (i.e., L10 is greater than L9, L9 is greater ±an L8, L8 is greater than L7, L7 is greater than L6, L6 is greater than L5, L5 is greater than L4, L4 is greater than L3, L3 is greater than L2, L2 is greater than LI). The displacement members 70 are arranged to establish a predefined contour of the leaf assembly 50. The predetermined contour is configured to compensate for movement of the preheater 10 during operation. As shown in FIG. 3, the first leaf 52 and the second leaf 54 have a trapezoidal shape.
[0038] Referring to FIG. 6, when the distal end 52D of the seal assembly 140 engages the surface 31 of the sector plate 30A’ a pressure Pl (shown on a left hand side of the leaf assembly 50 in FIG. 6) is present in the air outlet duct 28 of the air sector 32 of FIG. 1 ; and a pressure P2 (shown on a right hand side of the leaf assembly in FIG. 6) is present in the flue gas inlet duct 22 of the gas sector 34 of FIG. 1. The pressure Pl is greater than the pressure P2, thereby creating a pressure differential ΔΡ across the seal assembly 140. When the seal assembly 140 is in the area of the sector plate 30A’, without the displacement members 70 properly set, the differential pressure ΔΡ causes the leaf assembly 50 to deflect in the direction indicated by the arrow XX tending to open up a leakage gap between the distal end 52D of the seal assembly 140 and the surface 31 of the sector plate 30A’. However, the displacement members 70 apply a preload or predetermined deflection to the leaf assembly 50 so that the leaf assembly remains in a generally upright position with the distal end 52D of the seal assembly 140 engaging the surface 31 of the sector plate 30A’ and thereby overcoming the differential pressure ΔΡ induced deflection.
[0039] When the seal assembly rotates about 180 degrees into the area of the sector plate 30A a pressure ΡΓ (shown on a right hand side of the leaf assembly 50 in FIG. 6) is present in the air outlet duct 28 of the air sector 32 of FIG. 1; and a pressure P2’ (shown on a left hand side of the leaf assembly in FIG. 6) is present in the flue gas inlet duct 22 of the gas sector 34 of FIG. 1.
The pressure ΡΓ is greater than the pressure P2’ thereby creating a differential pressure ΔΡ’ across the leaf assembly 50. When the seal assembly 140 is in the area of the sector plate 30A the differential pressure ΔΡ’ tends to cause the leaf assembly 50 to deflect in the direction indicated by the arrow YY. When the seal assembly 140 is in the area of the sector plate 30A the displacement members 70 hold the leaf assembly 50 in a predetermined position in which the distal end 52D of the seal assembly 140 engages the surface 31 of the sector plate 30A to minimize leakage between the air sector 32 and the gas sector 34.
[0040] As shown in FIGS. 3 and 6, the seal assembly 140 includes a strip 80 having fourth base section 80B that engages the second base section 54B of the second leaf 54. The fourth base section 80B defines a fourth fastening area, for example, a flat section and a bore extending therethrough for receiving one of the bolts 145 for securing the strip 80 to the diaphragm 18 of the preheater 10 of FIG. 1. The second base section 54B is positioned between the first base section 52B and the fourth base section 80B. The strip 80 defines a deflector section 80L extending away from the fourth base section 80B and away from the second leaf 54. The deflector section 80L terminates at a distal end 80D. For example, the strip 80 has a bend 80Y so that the deflector section 80L is set at an angle Q away from the second leaf 54. The strip 80 has utility in protecting the leaf assembly 50 from potential obstructions such as soot blowing equipment projecting into the preheater 10. In addition, the strip 80 is a limit stop for limiting the amount of deflection of the leaf assembly 50.
[0041] As shown in FIGS. 4 and 6 a bar 90 (e.g., a spacer bar, or elongate washer) is aligned with a portion of the first base section 52B and the second base section 54B. The bar 90 extends along a length of the leaf assembly 50 and is positioned between the nuts 146 and the diaphragm 18. The bar 90 provides structural stability and helps uniformly secure the first leaf 52, second leaf 54 and the strip 80 to the diaphragm 18.
[0042] As shown in FIG. 6, the sector plate 31 defines a sharp leading edge 31L and a sharp trailing edge 31T. The leading edge 31L is defined by an angle 01; and the trailing edge 31T is defined by an angle 02. In one embodiment, the angle 01 and/or the angle 02 is about 90 degrees.
[0043] Through analysis and experimentation, the inventors have surprisingly discovered that as the seal assembly 50 rotates with the rotor assembly 12, the first distal end 52D of ±e first leaf 52 abruptly and scrapingly engages the leading edge 31L in a scissor-like operation; and abruptly and scrapingly disengages the trailing edge 3IT in the scissor-like operation, which causes premature wear of the seal. Contrary to engineering intuition, the inventors have found that the wear is more prominent radially inward towards the rotor post 16.
[0044] As prompted by the results of the experimentation and testing, the inventors have modified the sharp leading edge 31L and trailing edge 3 IT to a ramped configuration as shown in FIG. 7. The ramped configuration includes a ramped leading edge 31L’ and a ramped trailing edge 3IT’. The ramped leading edge 31L’ defines a ramp angle 01, and the ramped trailing edge defines a ramp angle 02. In one embodiment the ramp angles 01 and/or 02 are between about 15 and 25 degrees relative to the surface 31 of the sector plate 30A or 30B. In one embodiment the ramp angles 01 and/or 02 are between about 25 and 45 degrees relative to the surface 31 of the sector plate 30A or 30B. While the ramped leading edge 31L’ and the ramped trailing edge 3 IT’ is shown as a chamfer in the sector plate 30A the present invention is not limited in this regard as similar configurations may be employed in the sector plate 30B (or other sector plates in trisector and quad sector preheaters) and/or other ramp configurations may be employed such as but not limited to ramp attachments 13 IL and 13 IT secured to the sector plate 30A and/or 30B as shown in FIG. 8. As shown in FIG. 8, the ramp attachment 131L has a leading surface 13 ILA and a trailing surface 131LB each oriented at a ramp angle Θ1 relative to the surface 31 of the sector plate 30A. Likewise, the ramp attachment 131T has a leading surface 131TA and a trailing surface 131TB each oriented at a ramp angle Θ2 relative to the surface 31 of the sector plate 30A. The ramp attachments 13IL and 13 IT are secured to the sector plates 30A and/or 30B by a suitable fastening configuration such as but not limited to bolting and welding. The ramp attachments 131L and 13 IT are configured to be installed as original equipment as part of a new preheater installation or retrofitting of an existing preheater.
[0045] As a resulted of laboratory test simulations of preheater operation, the inventors have found that the ramped configuration having a 20 degree ramp angle results in a total wear rate of the seal assembly 50 of less than 0.0016 inches per hour at less than 30 percent load operation at locations along the seal assembly between 50 and 150 inches from the axis A; and less than 4 x 10"4 inches per hour at less than 30 percent load operation at locations along the seal assembly between radially outward of 150 inches from the axis A. While the wear rates are based upon laboratory testing, the inventors expect that they are a reasonable prediction of wear during operation.
[0046] Although this invention has been shown and described with respect to the detailed embodiments thereof, it will be understood by those of skill in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed in the above detailed description, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (15)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LU92841A LU92841B1 (en) | 2015-10-05 | 2015-10-05 | Flexible seal for a regenerative rotary preheating device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LU92841A LU92841B1 (en) | 2015-10-05 | 2015-10-05 | Flexible seal for a regenerative rotary preheating device |
Publications (1)
Publication Number | Publication Date |
---|---|
LU92841B1 true LU92841B1 (en) | 2017-05-02 |
Family
ID=54345566
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
LU92841A LU92841B1 (en) | 2015-10-05 | 2015-10-05 | Flexible seal for a regenerative rotary preheating device |
Country Status (1)
Country | Link |
---|---|
LU (1) | LU92841B1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59231396A (en) * | 1983-06-14 | 1984-12-26 | Gadelius Kk | Sealing device of rotational regenerating type heat exchanger |
US4593750A (en) * | 1985-08-19 | 1986-06-10 | The Air Preheater Company, Inc. | Radial seal assembly for rotary regenerative heat exchanger |
WO1997037186A1 (en) * | 1996-04-01 | 1997-10-09 | Abb Air Preheater, Inc. | Radial seal for air preheaters |
US20130105105A1 (en) * | 2011-10-31 | 2013-05-02 | Harlod L. O'Brien | Bimetallic seal for air heaters |
GB2515531A (en) * | 2013-06-26 | 2014-12-31 | Power System Services Ltd | A Seal for a Rotary Heat Exchanger |
-
2015
- 2015-10-05 LU LU92841A patent/LU92841B1/en active IP Right Grant
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59231396A (en) * | 1983-06-14 | 1984-12-26 | Gadelius Kk | Sealing device of rotational regenerating type heat exchanger |
US4593750A (en) * | 1985-08-19 | 1986-06-10 | The Air Preheater Company, Inc. | Radial seal assembly for rotary regenerative heat exchanger |
WO1997037186A1 (en) * | 1996-04-01 | 1997-10-09 | Abb Air Preheater, Inc. | Radial seal for air preheaters |
US20130105105A1 (en) * | 2011-10-31 | 2013-05-02 | Harlod L. O'Brien | Bimetallic seal for air heaters |
GB2515531A (en) * | 2013-06-26 | 2014-12-31 | Power System Services Ltd | A Seal for a Rotary Heat Exchanger |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8225614B2 (en) | Shim for sealing transition pieces | |
US11333446B2 (en) | Flexible seal for a rotary regenerative preheater | |
US9808889B2 (en) | Gas turbine including sealing band and anti-rotation device | |
US9291065B2 (en) | Gas turbine including bellyband seal anti-rotation device | |
KR102188910B1 (en) | High Temperature Air Sealing Butterfly Valve | |
US9897317B2 (en) | Thermally free liner retention mechanism | |
US10295273B2 (en) | Flexible seal for a rotary regenerative preheater | |
LU92841B1 (en) | Flexible seal for a regenerative rotary preheating device | |
US10704840B2 (en) | Flexible seal for a rotary regenerative preheater | |
AU2011253595B2 (en) | Gas turbine and method for reconditioning such a gas turbine | |
WO2021181962A1 (en) | Combustion cylinder mounting method and combustion cylinder mounting jig | |
Lacy et al. | Shim for sealing transition pieces |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Patent granted |
Effective date: 20170502 |