US20130153184A1

US20130153184A1 - Heat exchanger

Info

Publication number: US20130153184A1
Application number: US13/677,773
Authority: US
Inventors: Andrew Martin Rolt; Rory Douglas Stieger
Original assignee: Rolls Royce PLC
Current assignee: Rolls Royce PLC
Priority date: 2011-12-19
Filing date: 2012-11-15
Publication date: 2013-06-20
Also published as: EP2607831A1; GB201121754D0

Abstract

This invention relates to a heat exchanger, comprising a plurality of stacked corrugated plates, each plate having a plurality of parallel main corrugations each having longitudinal peak ridges and trough ridges, wherein either or both of the peak ridges and trough ridges have an undulating profile so as to define a plurality of summits in a common plane.

Description

TECHNICAL FIELD OF INVENTION

This invention relates to heat exchangers. In particular, the invention relates to cross-corrugated heat exchangers.

BACKGROUND OF INVENTION

The use of heat exchangers to transfer the thermal energy from a hot fluid to a cold fluid is well known and finds application in many different industries. One type of heat exchanger having good thermal and pneumatic performance is a cross-corrugated plate heat exchanger 10 as shown in FIG. 1.
The cross corrugated plate heat exchanger 10 shown in FIG. 1 includes a number of corrugated plates 12 which are stacked on top of one another such that the channels formed 14 by the corrugations lie at an angle to one another (90 degrees in this case). The plates are joined together by any suitable application led manufacturing technique such as brazing or welding. The material will also be application led but will typically be aluminium or other metal with a high thermal conductivity.
Although not shown for the sake of clarity, the ends of the plates 12 are connected to manifolds such that hot and cold air or other fluids can be supplied in use and complex flow patterns induced between the plates 12. The complex flow patterns aid the heat transfer between the hot and cold air flows but at a penalty of increasing the pressure loss across the plates or a reduction in velocity and mass flow for a given pressure differential.
FIG. 1 b shows a portion of the heat exchanger of Figure la in more detail. Thus there can be seen a lower plate 12 a, mid plate 12 b and upper plate 12 c having corrugations which are orthogonal to the adjacent plate. Cold 16 and hot 18 air flows are passed through the channels formed by the corrugations as denoted by the dashed and solid lines respectively. These airflows 16, 18 result in a heat transfer from the hot flow 18 to the cold flow 16. The heat exchanger 10 is shown in Figure lb as having crossed hot 18 and cold 16 flows in each layer. However, the matrix can be configured to have parallel-, cross- or contra-flows as desired.
Growing demand for environmentally viable energy systems has increased the need for efficient and compact heat exchangers. For example, the use of advanced cycles such as intercooled and recuperated gas turbine cycles for the aero industry requires compact low weight heat exchangers. Cross-corrugated heat exchangers have good thermal and pneumatic properties and there have been recent efforts in the art to modify the shape of the corrugations so as to improve thermal and pneumatic performance in the heat exchangers.
For example, EP0403353 describes a heat exchanger formed from superimposed corrugated plates separating the fluid channels. The plates have alternate long and short facets which are oriented in opposite direction on adjacent plates. This is described as ensuring an optimum fluid flow along the plates and a reduction in friction.
U.S. Pat. No. 4,420,039 describes a heat exchanger having a corrugated core structure with corrugated plates. The walls of the corrugations are provided with pairs of projections and recesses along their length which are successively separated by smooth wall portions. This is described as having the effect of successive throttling of the heat-transfer agent flow.
U.S. Pat. No. 5,806,584 describes a heat exchanger composed of corrugated plates, the facets of which are provided with bosses and hollows in order to reduce pressure drops.
EP1933105 describes a heat exchanger plate for the use in a plate heat exchanger having a first contact side and a second contact side, each comprising a pattern which provides respective uneven surfaces respective contact points for contacting a corresponding heat exchanger plate within a heat exchanger. The patterns are made up from a series of dents, indents, recesses, protrusions and/or additional corrugations between or outside the contact points.
Cross-corrugated plate heat exchangers have high potential for meeting the requirements of the gas turbine engines and the present invention seeks to provide an improved heat exchanger which is suitable for aero applications amongst others.

STATEMENT OF INVENTION

In a first aspect, the present invention provides a heat exchanger, comprising: a plurality of stacked corrugated plates, each plate having a plurality of parallel main corrugations each having longitudinal peak ridges and trough ridges, wherein either or both of the peak ridges and trough ridges have an undulating profile so as to define a plurality of summits in a common plane.
Either or both of the main corrugations and undulations may be periodic. Preferably, the main corrugations and undulations will be substantially sinusoidal.
The pitch of the undulations may be equal to the pitch of the main corrugations in an adjacent plate.
The longitudinal axes of the main corrugations of adjacent plates may be angled relative to each other. The angle may be 90 degrees. Alternatively, the angle may be substantially 0 degrees or any angle between 0 and 180 degrees.
The depth between adjacent ridges may be greater than the depth of the undulations.
One or more of the summits may provide a seat portion for abutting a corresponding summit of an adjacent plate.
The undulations of adjacent peak ridges and trough ridges in a plate may be in phase relative to the longitudinal axis of the main corrugations.
Substantially the entirety of each plate may have undulating ridges.
At least one of the corrugated plates may include straight ridges.
The main corrugations may be asymmetric.
The main corrugations may have a saw toothed profile.
The main corrugations may be tortuous along the longitudinal axis of the main corrugation.

DESCRIPTION OF DRAWINGS

Embodiments of the present invention are described below with the aid of the following drawings in which:

FIGS. 1 a and 1 b show a known cross-corrugated heat exchanger matrix.

FIG. 2 shows a heat exchanger plate of the invention.

FIGS. 3 a and 3 b show a partial cross-section of two heat exchanger plates in a stacked orthogonal arrangement according to the invention and prior art respectively.

FIG. 4 shows an alternative embodiment of the invention having out phase undulations.

FIG. 5 shows an alternative embodiment of the invention in which the summits include seat portions.

FIGS. 6 a and 6 b show velocity magnitudes normal to the surface of a heat exchanger plate of the prior art and invention respectively.

FIGS. 7 a and 7 b show Nusselt number distributions for a heat exchanger plate of the prior art and invention respectively.

FIG. 8 shows a schematic representation of two heat exchanger plates stacked one on top of the other and with an angle of intersection between the axes of their major corrugations.

FIGS. 9 a, b, c and d show various orientations of stacked heat exchanger plates according to the invention.

FIGS. 10 a, b, c and d show various alternative orientations of stacked heat exchanger plates according to the invention.

FIGS. 11 to 13 show various alternative embodiments of heat exchanger plates according to the present invention.

DETAILED DESCRIPTION OF INVENTION

Corrugated plate heat exchanger matrices typically have high thermal transfer coefficients and good pneumatic performance. However, conventional corrugated plate matrices have non-uniform heat transfer coefficients across the surface of each corrugated plate, with, for example, a lower heat transfer coefficient in a trough of the corrugations. This non-uniformity in heat transfer results in a non-uniform temperature distribution in the heat exchanger plates and a reduction in performance as a consequence. A typical figure for this reduction in performance can be as high as 7%, which is unnecessarily high. Further, the non-uniformity of heat transfer can lead to local thermal stresses in the heat exchanger matrix which are generally undesirable.
A further consideration of heat exchangers for aero-engines is the minimum flow cross-section area dimension through the matrix. Typically, it can be necessary for 1 mm diameter particles to be able to pass through an aero engine heat exchanger so that a given performance can be expected and blockages avoided. Nevertheless, it would be advantageous for larger particles to be able to pass through to help improve performance and reduce blockages further.
One way to achieve this would be to construct larger flow passages inside the heat exchanger matrix but this would result in an increase in the size of the heat exchanger for an equivalent performance. Hence, one aim of the invention is to help increase the minimum flow dimension within the flow channels of the heat exchanger to allow for a greater particle size to pass through, without increasing the overall size of the heat exchanger matrix.
FIG. 2 shows a portion of a corrugated plate 210 according to the present invention. In use, the plate 210 would be stacked with a plurality of similar corrugated plates to provide a heat exchanger matrix similar to that shown in FIG. 1. The corrugated plate 210 includes a plurality of parallel longitudinal main corrugations defined by peak ridges 212 a and trough ridges 212 b extending substantially the length of the plate 210 (of which only a portion is shown for the sake of clarity). The semi-enclosed space defined by each main corrugation can be thought of as a channel 218 through which an air flow passes in use.
Each of the peak ridges 212 a and trough ridges 212 b have an undulating profile 216 so as to define a plurality of summits 220 on the upper 222 and lower 224 surfaces of the plate 210 as shown in FIG. 2. The summits 220 are provided in a common plane and have a pitch 226 which matches the pitch 228 of the ridges of an adjacent corrugated plate. Hence, each summit 220 provides a seat portion which is abutted and attached to a corresponding summit 220 of an adjacent plate, as can be seen in FIG. 3 a, where two plates 210 a and 210 b are stacked in a crossed arrangement (in this case at 90 degrees to one another).
The profile of the undulations 216 and peaks and troughs of the main corrugation in the described embodiment are periodic, specifically sinusoidal, and extend across the majority of the plate. Hence, the undulations and main corrugation includes a pitch 226, 228 and amplitude 230, 232 which is uniform across the plate 210. The maximum possible amplitude of the undulations 216 is the amplitude of the corrugations.
Although the main corrugation and undulations of the embodiment are sinusoidal, it will be appreciated that other shapes of corrugations may be used. For example, rounded triangular or saw tooth profiles. Further, they may be out of phase.
The plates 210 may be made from any suitable material as dictated by a particular application. Typically, the plates will be made from aluminium, stainless steel, titanium or nickel alloy for an aero application and would be provided with inlet and outlet manifolds and housings or casings in similar materials.
FIG. 3 a shows an end view of an upper plate 210 a and lower plate 210 b having sinusoidal corrugations and undulations, respectively, which have corresponding pitches such that the summits 220 of the adjacent plates 210 a, 210 b are joined together to provide a unitary structure.
As can be seen in FIG. 3 a, the dip 234 of the undulation in the lower plate 210 b is aligned with the dip 236 of the upper plate 210 a undulation. This keeps the maximum height of the airflow path defined by the two plates more or less the same as would be the case if there were no undulations (as shown in FIG. 3 b). As the channel defined by the main corrugation of the upper plate 210 a progresses into the page, the undulating upper ridge 212 a increases in height to a summit 238 which vertically opposes the summit (not shown) of the lower plate 210 b. Thus, the airflow path between the plates is a meandering, sinuous path which naturally churns up the airflow, as indicated by arrows 240 in FIG. 2. This leads to an increase in the heat transfer coefficient along the troughs of the main corrugations and a more uniform temperature in the plate 210 a, 210 b. This results in a smaller heat resistance due to the transverse heat conductance and lower thermal stress. Further, the churning results in a more energetic flow and greater heat transfer between the air flows and plates.
Further, the minimum flow area is increased with respect to prior art cross-corrugated arrangements 242 as shown in FIG. 3 b, which means that the spherical particle size which can pass along the airflow paths is larger. This can help reduce the likelihood of blocking.
Typical values of pitch and amplitude for the main corrugations and undulations will be just a few millimetres. In one example, the geometry of the corrugations and undulations both have 3.3 mm pitch and the corrugations have 1.5 mm amplitude and the undulations have 0.5 mm amplitude, with a 90 degrees angle between the ridges of the corrugations on adjacent plates. However, it will be appreciated that other ratios of amplitude and pitch may be advantageous. For example, the amplitudes may be in the range between 1 mm and 5 mm, and the pitch may be between 0.5 to 5 times the amplitude. One preferable range is a pitch which is between 2 and 4.5 times the amplitude.
An alternative embodiment is shown in FIG. 4 in which the undulating profiles superimposed on the heat exchanger plate's peak and trough ridges 412 a, 412 b are out of phase as can be seen by the dashed lines which are 180 degrees out of phase with respect each other along the longitudinal axis of the main corrugations.
In use, multiple plates are placed in a stacked arrangement and the corresponding summits of adjacent plates attached to each other so as to form a heat exchanger matrix in a similar manner to that shown in FIG. 1 but with the undulating corrugated plates. The matrix may be connected to hot and cold airflows via a manifold which is configured to provide cross-, parallel- or contra-flowing streams of air.
Any suitable method of attachment may be used, for example, brazing or welding. In the embodiment shown in FIG. 5, the joining of adjacent plates is aided by providing each of the summits 520 of a plate 510 with a seat portion in the form of a flat area 546 which is configured to abut another corresponding seat portion of an adjacent plate. The seat portions provide an increased area of surface contact which helps increase the strength of the mechanical connection between adjacent plates. It will be appreciated that the seat portions may advantageously include surface features or roughness which aids the attachment of the corresponding seat portion. In one embodiment, the individual plates may be stamped or electroformed and then brazed together. In this case, the summits may be prepared with a preferential application of braze on each of the seat portions as is known in the art.
To demonstrate the technical effect of the undulating main corrugations, FIGS. 6 a and 6 b respectively show comparative plots 610 a, 610 b of the velocity magnitude normal to the surface (i.e. V_y) for a prior art corrugated plate 612 a and a plate 612 b according to the present invention. It can be seen from this plot that the effect of the undulations is to create increased velocity flows 648 near to the surface of the plate 612 b which increases the thermal transfer between the airflows and the plates.
Another indicator of improved performance is given in FIGS. 7 a and 7 b which show Nusselt number distributions 710 a, 710 b on the bottom plate of a heat exchanger unit cell for a prior art plate 712 a and a plate according to the present invention 712 b. The largest Nusselt number occurs at the joining point of the peak ridge for both cases. For the present invention, however, it is observed that the variation of Nusselt number from peak to trough (as indicated by the corresponding encircled areas 750 a, 750 b in each Figure) is less steep than that of conventional plate. This results in a simulated friction factor which is approximately 15% lower than the conventional model and a slight increase in Nusselt number. These changes produced an approximate 4% increase in volume goodness factor and 16% increase in area goodness factor, which can provide a more compact heat exchanger installation compared to a heat exchanger matrix not having the undulations.
It will be understood that the volume goodness factor referred to is that defined as the Stanton number divided by the one third root of the fanning friction factor and is inversely proportional to matrix volume. The area goodness factor is the Colburn j factor divided by the fanning friction factor and is inversely proportional to the frontal area of a heat exchanger matrix. As will be appreciated, any change in matrix geometry which increases both parameters simultaneously is beneficial to the overall design and performance of a heat exchanger.
Adjacent plates in the matrix may be angled relative to each other by a given angle of intersection. By angle of intersection it is meant the angle between the longitudinal axes of the corrugations as shown in the graphical representation in FIG. 8 in which the dotted lines represent the peak 810 a and trough 812 a ridges of the main corrugations of a first plate, and the peak 810 b and trough 812 b ridges of the main corrugations of a second plate, which are separated by an angle of intersection 814. It will be appreciated that the direction of airflow for the arrangement shown in FIG. 8 relative to the angle of intersection is from left to right.
The stacked heat exchanger plates described in embodiments above are arranged with intersection angles of 90 degrees. With reference to FIG. 8, if the main corrugation peaks and troughs of an upper plate and the main corrugation peaks and troughs of a lower plate are skewed or rotated relative to each other by some angle, it is possible to get cross-flow arrangement of various intersection angles.
For example, if sinusoidal periodic profiles are assumed for the main corrugations and undulations, the surface of skewed plate can be expressed as follows:
$\begin{matrix} z (x, y) = \frac{H}{2} [a_{h} \cos (\frac{2 π (x - \tan (π / 2 - θ) y)}{P_{h}}) \cos (\frac{2 π y}{P}) + (1 - a_{h}) \cos (\frac{2 π y}{P})] & Eq . 1 \end{matrix}$
where H is the height of corrugation, P the pitch of main corrugation, P_his the pitch of the undulation a_his a dimensionless undulation amplitude (zero to unity) and θ is the complementary angle of the intersection angle from 90 degrees. Hence, if θ is zero then the angle between the plates becomes 90 degrees.
It will be appreciated any approximation by a similar function or a general Bezier curve or line and circular arc segment may be substituted for the above function to define the surface of the plates.
FIG. 9 shows plan and isometric views of unit cells of two stacked cross-corrugated heat exchanger plates 910 a-d,912 a-d, for various skew angles in which the plates have intersection angles of 90 degrees—FIG. 9 a, 60 degrees—FIG. 9 b, 45 degrees—FIG. 9 c and 30 degrees—FIG. 9 d. For each case it is assumed that P/H=2.2, Ph/H=2.2 and a_h=0.2. If the hot side of heat exchanger plate in an orthogonal cross-flow matrix has a given angle of intersection, the angle of intersection for the cold side is the supplementary angle, and unless both angles are 90 degrees, the heat transfer and pressure loss characteristics of each side become different. Therefore, by varying the angle of intersection, it is possible to separately control the heat exchanger performances of the hot and cold sides in order to optimise a matrix design as is known in the art. For example, in a cross-flow cross-corrugated air-to-air intercooler the frontal area can be reduced if the flow resistance to the lower density and larger volume cold-side flow is reduced by reducing the angle of intersection to 80 degrees, while accepting the increased angle of intersection of 100 degrees for the higher density, but lower Mach number, hot-side flow.
Parallel and contra-flow arrangements are also possible and it can be advantageous to have reduced intersection angles between adjacent plates in this case also. In these cases both hot and cold sides see the same angles of intersection so a further reduction to between 30 and 60 degrees is beneficial. Several examples are shown in FIG. 10 which shows isometric views of unit cells of two stacked cross-corrugated heat exchanger plates 1010 a-d, 1012 a-d for various intersection angles, namely 90degrees—FIG. 10 a, 45 degrees—FIG. 10 b, 30 degrees—FIGS. 10 c and 15 degrees—FIG. 10 d.
Other alternative embodiments of the invention are shown in FIGS. 11 to 13.
In the embodiment shown in FIG. 11, the corrugated plate 1110 includes main corrugations having peak and trough ridges 1112 a, 1112 b in which only the alternate ridges have undulations. The remaining, non-undulating ridges 1114 are substantially straight. A possible function for defining such a profile is given in equation 2 below in which the function ƒ_hcorresponds to equation 1 above and ƒ_sis defined in equation 3 below. The remaining parameters are defined above for equation 1.
$\begin{matrix} f_{01} (x, y) = {\begin{matrix} f_{h} (x, y), & 0 \leq y \leq P \\ (1 - \frac{y - P}{P / 2}) f_{h} (x, y) + (\frac{y - P}{P / 2}) f_{s} (x, y), & P \leq y \leq 1.5 P \\ f_{s} (x, y), & 1.5 P \leq y \leq 2 P \end{matrix} & Eq . 2 \\ f_{s} (x, y) = \frac{H}{2} \cos (\frac{2 π y}{P}) & Eq . 3 \end{matrix}$
This is advantageous as the extent to which the airflow crossing the plates 1110 is disrupted which can act to increase the heat exchange between the plates 1110. More specifically, the applicants have discovered that increased thermal performance can be achieved with a configuration which continually excites and relaxes the airflows, with particular benefit being taken from the relaxation flow. In this embodiment, this is achieved with the introduction of the straight ridges 1114. It will be appreciated that the distribution of undulating and straight ridges may be determined to achieve a desired thermal performance. Specifically, there may be one undulating ridge to two straight ridges in a given plate.
FIG. 12 shows a heat exchanger plate 1210 in which the main corrugations as defined by the ridges 1212 are tortuous in that they are sinusoidal waves in the longitudinal direction. Such a profile can be defined by the function shown in equation 4 below, where ƒ_hcorresponds to the function given in equation 1 above, a_wis the amplitude of the sinusoidal wave and P_wis the pitch of the sinusoidal wave.
$\begin{matrix} f_{02} (x, y) = f_{h} (x, y - a_{w} \cos (\frac{2 π x}{P_{w}})) & Eq . 4 \end{matrix}$
Again, with this embodiment, the inclusion of a sinusoidal (or otherwise curved or meandering) main corrugation increases the turbulence within the channels formed by the corrugations which can act to increase the thermal transfer between airflows. In the embodiment shown, the pitch of the wave is half that of the pitch of the main corrugation, and the amplitude of the wave is approximately twice the amplitude of the main corrugations. However, it will be appreciated that other configurations and functions will provide the desired increased thermal response which will be application specific.
FIG. 13 shows yet another embodiment in which the curvature of the main corrugation is wave-like in that it includes an asymmetrical profile. The asymmetrical profile includes an upstream slope 1312 and a downstream slope 1314 in which the upstream slope 1312 has a sharper angle of incidence relative to the plane of the plate 1310 when compared to the downstream slope 1314. Hence, air travelling downstream 1316 is disrupted and accelerated by the more vertical face of the upstream slope 1312 and before gradually decelerating on the less steep downstream portion of the main corrugation profile.
In the embodiment of FIG. 13, the wave-like profile can generally be thought of as a skewed sinusoid which is be defined by the function given in equation 5. It will be appreciated that the chosen profile and function may be varied whilst retaining the advantageous acceleration and deceleration behaviour. For, example, the profile may be more saw toothed with sharper ridge peaks, or shallower,
$\begin{matrix} f_{03} (x, y) = {\begin{matrix} f_{m 1} (x, y), & 0 \leq y \leq 0.5 P \\ f_{m 2} (x, y - 0.5 P), & 0.5 P \leq y \leq P - 0.5 β P \\ f_{m 1} (x, y - 1.0 P), & P - 0.5 β P \leq y \leq 1.5 P \\ f_{m 2} (x, y - 1.5 P), & 1.5 P \leq y \leq 2 P - 0.5 β P \\ f_{m 1} (x, y - 2.0 P), & 2 P - 0.5 β P \leq y \leq 2 P \end{matrix} & Eq . 5 \end{matrix}$
in which:
$shift = β \frac{P}{2}, 0 \leq β \leq 1$ ${\begin{matrix} P_{1} = (1 + β) P \\ P_{2} = (1 - β) P \end{matrix} {\begin{matrix} m_{1} (x, y) = H \cos (\frac{2 π (y + shift)}{P_{1}}) \\ m_{2} (x, y) = - H \cos (\frac{2 π y}{P_{2}}) \end{matrix} {\begin{matrix} f_{m 1} (x, y) = \frac{H}{2} (a_{h} \cos (\frac{2 π x}{P}) m_{1} (x, y) + (1 - a_{h}) m_{1} (x, y)) \\ f_{m 2} (x, y) = \frac{H}{2} (a_{h} \cos (\frac{2 π x}{P}) m_{2} (x, y) + (1 - a_{h}) m_{2} (x, y)) \end{matrix}$
H, P and P_hare defined above for equation 1.
Another way to describe the configuration would be to say that the profile forms a fluidic diode in which the lateral flow across the main corrugations is greater in a first direction than from a second direction. It will be appreciated that in normal use the flow is directed in the first, higher resistance direction.
The embodiments described above are not to be taken as a limitation of the broader inventive concept defined by the claims.
For example, it will be appreciated that the geometric configuration of the heat exchanger plates may be altered to provide a desired thermal response. Further, the various features relating to the main corrugations and undulations are envisaged as having application in more than one embodiment. For example, the wave-like profile of shown in FIG. 12 may be combined with the alternating ridge profiles shown in FIG. 11.
Additionally, it is envisaged that although the summits shown are described as providing contact points for adjoining adjacent plates together, this is not a limitation of the invention, and some of the summits may not abut summits of an adjacent plate.
Further still, the pitch of the undulations may be different to the pitch of the main corrugations. It is envisaged that in some embodiments, the pitch of the undulations may be between 0.2 to 5 of the pitch of the main corrugations.
It is also envisaged that the distribution of the corrugations across the surface of a heat exchanger plate may be varied to account for variations in the air flow and temperature distribution within the heat exchanger matrix. For example, the undulations may be more densely spaced towards an inlet of the matrix than towards the outlet, or vice versa.

Claims

1. A heat exchanger, comprising:

a plurality of stacked corrugated plates, each plate having a plurality of parallel main corrugations each having longitudinal peak ridges and trough ridges, wherein either or both of the peak ridges and trough ridges have an undulating profile so as to define a plurality of summits in a common plane.

2. A heat exchanger as claimed in claim 1 wherein either or both of the main corrugations and undulations are periodic.

3. A heat exchanger as claimed in claim 2 wherein either or both of the main corrugations and undulations are substantially sinusoidal, Bezier curves or line and arcuate segments in profile.

4. A heat exchanger as claimed in claim 1 wherein the pitch of the undulations is equal to the pitch of the main corrugations in an adjacent plate.

5. A heat exchanger as claimed in claim 1 wherein the longitudinal axes of the main corrugations of adjacent plates are angled relative to each other.

6. A heat exchanger as claimed in claim 5 wherein the angle is 90 degrees.

7. A heat exchanger as claimed in claim 5 wherein the angle is between 0 and 180 degrees.

8. A heat exchanger as claimed in claim 1 wherein the depth between adjacent ridges is greater than the depth of the undulations.

9. A heat exchanger as claimed in claim 1 wherein one or more of the summits provides a seat portion for abutting a corresponding summit of an adjacent plate.

10. A heat exchanger as claimed in claim 1 wherein the undulations of adjacent peak ridges and trough ridges in a plate are in phase relative to the longitudinal axis of the main corrugations.

11. A heat exchanger as claimed in claim 1 wherein substantially the entirety of each plate has undulating ridges.

12. A heat exchanger as claimed in claim 1 in which at least one of the corrugated plates includes straight ridges.

13. A heat exchanger as claimed in claim 1 in which the main corrugations are asymmetric.

14. A heat exchanger as claimed in claim 13 in which the main corrugations have a saw toothed profile.

15. A heat exchanger as claimed in claim 1 wherein the main corrugations are tortuous along the longitudinal axis of the main corrugation.