[0001] The present invention refers to a method and system for the compensation of wave
guide resonant cavites, more particularly to a system for the compensation of the
thermal effects on the cavity characteristics and for the conservation of the band-width
at varying tuning frequencies.
[0002] The invention comprises the microwave resonant cavities so obtained, with compensation
of the resonance frequency and also of the magnetic coupling and of the band-width.
PRIOR ART
[0003] The wave guide cavities are largely used as resonators and filters when the microwave
signal powers are high and cannot therefore involve dielectric containing cavities.
[0004] It is known that thermal excursions can cause deleterious effects on the working
and on the characteristics of resonant cavities and affect the resonant frequency
in an prohibitive measure. The problem is so important that the manufacturers have
to use special materials with very low thermal coefficients, which are however very
expensive and often are very difficult to be machined and/or formed. The well known
alloys INVAR and SUPER-INVAR are to be recalled among the various precious materials.
To restrict the use of such expensive materials, compensation systems have been suggested
which can be adopted in combination with poor materials so to maintain the excursions
of the resonant frequency and of the band-width within acceptable (even if not entirely
satisfactory) limits.
[0005] For instance, one of these systems foresees the use (especially in the dielectric
cavities) of several materials with different thermal expansion coefficients, located
however in such a way to cause a compensation of the expansions.
[0006] Just to fix the ideas, one of the most immediate solutions of the prior art is represented
in fig. 1 which is a schematic and partial cross-section showing a wave guide cavity
CAR (10) delimited by major longitudinal upper PAS (3) and lower PAI (4) walls at
a distance H from each other, and by minor transversal and walls PE (1) and PE (2)
at a distance L.
[0007] The resonant cavity CAR is tuned wilh the help of a variable capacity Cv formed of
a rod AS which can assume a variable penetration. At increasing penetration P and
therefore capacity Cv, decreases the cavity tuning frequency Fs.
[0008] The rod penetration P is regulated by means of a screw VI which is fixed through
a bolt D to a cylinder CI soldered to the cavity CAR (10). The thermal compensation
is based on the difference between the expansion linear coefficient of the rod AS
and of the support cylinder CI. At increasing temperature, as the cylinder undergoes
an expansion higher than that of the rod AS, the end of this rod reduces its penetration
into the cavity causing a decrease of the capacity of Cv and therefore a tuning frequency
increase which compensates the natural decrease caused by the cavity linear dimension
increase.
[0009] The above frequency compensation can be perfect at one frequency but can be maintained
with acceptable characteristic only in one frequency restricted band because of the
strong non-linearity between the tuning frequencies Fs and the rod penetrations P
into the cavity. Indeed when the frequency decreases, at a parity of frequency variations
ΔF, correspond always minor introductions P of the rod; all this causes an over compensation
at the lower frequencies and a subcompensation at the higher frequencies.
[0010] An other inconvenience of the above described system resides in the big encumbrance
of the cylinder/rod device which has a body outside the wave guide cavity. Moreover
said tuning system is not able to develop a frequency variable action on the cavity
coupling elements because the mutual distance does not vary at the different frequencies.
This concept will be better clarified in the course of the invention description .
[0011] First object of the present invention is to provide a method and system which do
not show the above mentioned drawbacks and allow the obtainement of an optimal and
easy tuning and of a contemporaneous compensation concerning not only the resonant
frequency but also the band width and the coupling.
[0012] An other object is to provide wave guide resonant cavities with a compensation device
having a body moving along the longitudinal axis and substantially within protuberances
projecting from the cavity major walls, and an organ of support and control of the
translation and position of said body over said protuberances, said organ extending
on substantially the whole internal length of the cavity and imparting displacements
to said body only on the basis of its thermal variations.
[0013] These and other objects are reached with a variable capacity obtained trough longitudinal
displacements. In a simple advantageous and therefore preferred embodiment, the system
according to the invention comprises:
a) stationary means provided on and projecting from at least one of the cavity major
walls, said means having a longitudinal extension "l" which is small over the length
"L" of said major walls;
b) means movable over said means a) projecting from said walls;
c) means which extend on the whole length L within the cavity and carry said movable
means b) imparting them displacements proportional to their thermal excursion; and
d) means to form a fixed stationary constraint at one end of said means c) -
In one embodiment of the invention, the means a) projecting from the two major
faces towards the cavity internal space have a thickness variable from Smx to So over
a length "l", and the means b) have a major base in correspondence to the minimal
thickness So and a minor base in correspondence to the maximal thickness (Smx), the
distance between said major and minor bases being equal to "l".
[0014] In a preferred embodiment of the invention, the means a) have the form of a pole
shoe and the means b) nave the form of a cylinder showing therefore a constant diameter
on the length "l".
[0015] The various features and advantages of the invention will better appear from the
following description of the non-limitative embodiments shown in the accompanying
drawings, in which:
- figures 2 and 10 are schematic frontal views of the wave guide cavity embodying the
compensator according to the invention;
- fig. 3 is a top view of the cavity of fig. 2;
- figures 4, 7 and 7A are equivalent schemes of the cavity incorporating the compensator;
- fig. 4A is a diagram;
- fig. 5 is a front view similar to that of fig. 2 but restricted to a compensation
system portion shown on an enlarged scale;
- fig. 6 is an equivalent scheme of the prior art solution;
- figures 8 and 8A are plan respectively cross section views of a compensator formed
of rectangular elements, and
- fig. 11 is a lateral view of a double cavity with two compensators of the type of
fig. 10.
[0016] In the drawings the reference CAR (10) indicates a resonant cavity in the form of
a wave guide, schematically defined by two minor end walls PE(1), PE(2) and two major
upper PAS(3) and lower PAI(4) walls; to one of the two end walls, f.i. to PE(2) are
associated the input and output connectors CON I (6) respect. CON U (5) with the relevant
loops LO I(7), LO U (8).
[0017] In the central zone of the cavity CAR (10) is located the compensation system according
to the invention COMP(11) (figures 2,3,8A, 10 and 11), which generally comprises:
a) at least one, preferably two (as shown in the figures 2,8A, 10 and 11) protuberancies,
thickenings or projections SPO₁, SPO₂ provided on the two major faces PA(3) and PAS
(2) and having a longitudinal extension "l" small over the length L of said major
faces or walls;
b) a wedge Cu, CUC and CUC' respectively in the figures 2, 10 and 11 which is movably
inserted between said protuberances and has a length "l'" equal or different from
"l";
c) a rod AS extending on the whole length L and carrying fixedly the wedge Cu, and
d) a constraint V at one end of road AS which cannot move at this end whereas at the
other end EL it is free to undergo dimensional excursions under the effect of thermal
variations.
[0018] In fig. 2 the wedge Cu and the projections SPOi are trapezoidal but they can be parallelepiped
f.i. rectangular as in figures 8 and 8A or cylindrical as in the figures 10 and 11.
In fig. 2 said wedge Cu has a terminal minor face 20 f.i. in correspondence to the
maximal projection Smx and a terminal major face 21 in correspondence to the terminal
protrusion So; the wedge has its two major surfaces 22 and 23 extending parallel to
the major faces 25 and 26 of projections SPO₁ and SPO₂ over a length "l". In figures
8 and 8A wedge Cu is parallelepiped wilh equal faces 20 and 21; accordingly also the
SPO₁ and SPO₂ have an equal height. In fig 10 the wedge CUC is a cylinder body; the
SPO₁ and SPO₂ have the shape of a pole shoe.
[0019] A rod AS carries Cu, said rod being free at the end EL (passing thus through the
wall PE(1)) but being blocked at the end 28 where it can be activated manually or
wilh the help of a motor for tuning purposes. An air gap I exists between walls 22
and 23 of wedge Cu and the facing walls 25 and 26 of the projections SPO₁ and SPO₂.
[0020] Referring to the equivalent scheme of fig. 4, cavity CAR (10) has a resonant frequency
which, in a resonator of the λ/2 type and in the absence of compensator COMP, occurs
at L = λ/2 where L is the length of CAR.
[0021] The compensator COMP corresponds to an additional capacity Cv which is clearly variable
with the displacement of wedge Cu between protruberances SPO₁ and SPO₂, i.e. with
the variation of the gap I (fig.5). If this gap I is Io in the position 1) of fig
5, it will assume values Ii > Io as Cu is displaced by rod AS rightwards f.i. to the
position 2 in said fig.5.
[0022] By varying gap I, vary the capacity Cv of compensator COMP and the capacity equivalent
length "Le" in the sense that at increasing I (desplacement of Cu to the right) decreases
Le because of the capacity Cv decrease. Let us consider the situation in the absence
of compensator COMP: with increasing temperatures the resonant cavity CAR would expand
by itself, i.e. its length L = λ/2 would increase and its resonant frequency Fr would
decrease. By adopting compensator COMP and setting it, according to the invention,
in such a way that to a natural increase ΔL of the length L and thus to a capacity
reduction -ΔC caused by a temperature increase ΔT, corresponds a displacement of Cu
rightwards and thus a gap increase ΔI and consequently a reduction - ΔCv of the additional
capacity such as to compensate the cavity thermal and dimensional variations wilh
simple and effective means.
[0023] In the diagram of fig. 4A, curve 1 shows the natural behaviour of cavity CAR in the
absence of compensation: at increasing temperature T (on the abscissa) L increases
and accordingly the resonant frequency FR decreases (curve 2).
[0024] If now at increasing temperatures the rod AS desplaces the wedge Cu rightwards, i.e.
gap I increases and decreases the capacity Cv added by compensator COMP with consequent
frequency increase (curve 1), one succeeds in compensating substantially constantly
the resonance frequency FR (curve 3) on which the wave guide cavity had been tuned.
[0025] Moreover the compensator according to the invention produces further surprising advantages.
As known in the devices with movable elements it is important that the magnetc coupling
between loops LOI, LOU and cavity be not altered. However in the compensation absence,
when the resonant frequency decreases, the loop magnetic coupling and the resonator
band-width decreases. One of the drawbacks of the prior art f.i. of the type of fig.
1, is that even if a compensator having a rod AS with variable penetration is able
to increase or decrease capacity Cv and therefore decrease or increase the tuning
frequency, it is however not able to produce any influence on the coupling degree.
[0026] This is due to the fact that rod AS is and remains always in a fixed position f.i.
over the walls PE(1) and PE (2); i.e. the rod can move upwards or downwards along
its axis Z-Z (fig. 6) but can not move perpendicularly to Z-Z. This limitation is
schematically shown in fig. 6 where capacity Cv is indicated as a variable capacity
but it cannot change its longitudinal position f.i. it cannot move in the position
P indicated with dotted line.
[0027] According to an important feature of the invention, the value of the variable capacity
is maximal (and thus the resonant frequency is minimal) just when the loop coupling
must be increased and thus the distance of said capacity Cv from the loops LO is to
be minimized so to have a coupling increased proportionally to the frequency decrease.
[0028] In fig. 7A the maximal capacity Cmx is shown just at a minimum distance Dmin from
loop LO whereby the natural coupling decrease due to the frequency decrease is compensated
by this. In fig. 7 also the other limit case is shown in which the minimal capacity
Cmin is obtained at the maximal distance Dmax of wedge Cu from the end wall PE(2)
carrying the loops. As to this minimal capacity Cmin corresponds a resonance maximal
frequency and thus a high natural coupling, the compensator wedge Cu is moved rightwards
so to decrease its coupling with the loops and to compensate the coupling increase.
[0029] Consequently also the band-width is compensated and maintained substantially constant
at varying frequency. Moreover these two beneficial surprising effects of the tuning
frequency thermal compensation and of the coupling and band-widh compensation at varying
resonant frequency do not have negative consequences on the insertion loss: indeed
the whole compensator has big dimensions (especially over the conventional screws
of fig. 1) and is flown by low density currents to which corresponds a negligible
loss.
[0030] Besides the critical feature of the compensation of the coupling and of the band-width
due to the approaching/departing of the compensator wedge from the loops, the invention
has also involved the overcoming of a technical prejudice. Fig 9 schows the curve
of the electric field between the walls of the cavity resonant in the most used mode
TE 101. It is a half sinusoidal curve with a central maximum. This central position
corresponds therefore to the maximal efficiency of the capacity inserted in the cavity
and is thus normally adopted when it is desired to vary the frequency with a variable
capacity placed in a fixed position.
[0031] If on the contrary the tuning is to be varied with a constant capacity placed in
a position variable along the major length , the most convenient position is that
nearest to the end walls because there occurs the major variation of the frequency.
[0032] Further in this position the maximal linearity in the correspondence between the
capacity position and the tuning frequency occurs because the electric field sinusoidal
characteristic is nearly linear in the proximity of zero. If the capacity is placed
in the cavity center, no cavity tuning frequency variations correspond to the position
variations because the electric field varies there too slowly. A frequency variation
is obtainable also in this position if on the cavity walls are provided projections
as in fig. 2 or wedges as in fig 8 or pole shoes as in figures 10 and 11. The corresponding
nucleus to be moved must have the form of a prism, a wedge or a cylinder in said three
cases to have a sufficiently linear tuning at varying position.
[0033] From the above it appears clearly that it is possible to tune the cavity with good
linearity by placing the mobile wedge in any position. Consequently, at a substantial
parity of linearity on the whole length it is possible and advantageous to choose
the critical position to which corresponds the minor band-width variation at varying
frequency.
[0034] By appropriately selecting the linear thermal expansion coefficient (s) of the control
rod (f.i. by making the rod with material gradients e.g. in INVAR on a length portion
and in brass on an other length portion as in figures 2,3 and 10), it is possible
to obtain a thermal compensation with a very wide frequency band thanks to the linearity
made possible by the criterion chosen to vary the tuning.
[0035] To the advantage of the tunability band increase togheter with good thermal compensation
must be added the other advantage of the minor encumbrance f.i. over fig. 1 because
of the absolute absence of outer organs as the whole compensation system namely the
rod and the relevant wedge are inside the cavity. As anticipated, in figures 10 and
11 a diplexer is shown with two compensators in which the protuberances SPO₁, SPO₂,
resp. SPO
1', and SPO
2', have the shape of pole shoes and the wedges CUC are cylinders.
[0036] The important advantage is that, for small as for big rotations (generally casually
occurrring during transportation after setting in the manufacture facilites) of rod
AS around its longitudinal axis X-X (arrow F) the air gap between CUC and the polar
shoe remains constant and therefore also the electric characteristics of the cavity
are independent from the angular position of CUC over the pole shoe.
1. Method for the thermal compensation of resonant cavities in form of wave guides, closed
and defined by at least six walls, on at least one PE(2) of which are provided connectors
(CON) and relevant coupling loops (LOI, LOU), characterized in that along the whole
major longitudinal extension (L) of the cavity (CAR) a rodshaped element (AS) is placed
which is fre of constraints at one (EL) of its ends and shows on its minor extension
(l') gradients of thickness, composition and capacitative coupling with at least one
of said cavity forming walls.
2. Method according to claim 1, characterized in that further analogous gradients are
generated also on the cavity longitudinal walls, substantially in correspondence of
said minor extension (l').
3. System of the thermal compensation of resonant cavities in form of wave guides, comprising
at least:
i) two walls (PAS₃, PAI₄) which are parallel and symmetrical over the longitudinal
axis of the cavity and have a length L and a transversal distance H;
ii) two end walls (PE₁. PE₂);
iii) input and output connectors (CON I, CON U) with relevant loops LOI, LOU of coupling
with the cavity, charaterized in that on an extension "l" lower than L, a variable
capacity is created by moving longitudinally a nucleus or wedge over portions of said
walls, said wedge undergoing longitudinal translations under the action of the thermal
variations of a support element extending on the whole length L, the maximum value
of said capacity being obtained with the maximum displacement of said nucleus towards
the wall carrying the coupling loops associated to said connectors.
4. System according to claim 3, characterized in that the nucleus is parallelepiped and
the longitudinal walls are provided with protuberances projecting inside the cavity.
5. System according to claim 3, characterized in that the wedge is cylindrical and the
protuberances projecting from the walls have the shape of a pole shoe.
6. System according to claim 3, characterized by:
a) means provided on and projecting from two major, each other facing, cavity forming
walls which protrude inside the cavity with a thickness variable from a maximum Smx
to a minimum So thickness value on a length portion "l" generally small over the length
L of the major walls;
b) means inserted between said projecting means having a trapezoidal form with a major
base corresponding to said protuberance minimal thickness (So) and a minor base corresponding
to the maximal protuberance (Smx) of means a), the distance between said major and
minor bases being substantially equal to "l";
c) means to carry and guide longitudinally means b) between means a) so to vary the
gap (I) between said means a), and
d) means to form a fixed stationary constraint at one end of means c) which are free,
i.e. not constrained at the other end.
7. System according to claim 6, charaterized in that the means a) are ribs with variable
projection to the cavity inside, and the means b) have the form of a trapezoidal wedge
with minor base in correspondence to the maximum projection points of a) and with
major base in correspondence to the minimal projections, and means c) have the form
of a rod.
8. System according to claim 3,4,5 or 6, characterized by additional means ( manual or
motor) placed at the terminal d).
9. System according to at least one of claims 3 to 8, wherein the cavity is substantially
made of not precious material of thermal expansion low coefficient.
10. System according to claims 3, 4, 5 or 6, wherein the projecting ribs, the wedge and/or
the rod are also made of not precious materials having equal or different thermal
expansion coefficients.
11. System according to at least one of the claims from 3 to 10, characterized in that
the displacement of the nucleus or wedge is carried out in such a way that said wedge
is brought near the wall carrying connectors and loops when said additional capacity
is high ( the temperature is low) increasing thereby the coupling between loops and
cavity, and is taken away from said wall when said additional capacity is minimal.