PERKINELMER HY-3003

Imaging
D A T A S H E E T
Lighting
Telecom
High Energy Switches
Thyratrons
Description
Features
Thyratrons are fast acting high
voltage switches suitable for a
variety of applications including
radar, laser and scientific use.
• Wide operating voltage range
PerkinElmer’s thyratrons are
constructed of ceramic and
metal for strength and long life.
Over 300 thyratron types are
available from PerkinElmer. The
types listed in this guide are a
cross section of the broad line
available. We encourage
inquiries for thyratrons to suit
your particular application.
• High pulse rate capability
• Ceramic-metal construction
• High current capability
• Long life
.
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How a Thyratron works
The operation of the device can
be divided into three phases: triggering and commutation (closure),
steady-state conduction, and
recovery (opening), each of which
is discussed below.
ANODE
CONTROL GRID (G2)
AUXILIARY GRID (G1)
CATHODE
Figure 1. Thyratron with auxiliary grid
(heater detail not shown)
Triggering and Commutation
When a suitable positive triggering pulse of energy is applied to
the grid, a plasma forms in the
grid-cathode region from electrons. This plasma passes through
the apertures of the grid structure
and causes electrical breakdown
in the high-voltage region
between the grid and the anode.
This begins the process of thyratron switching (also called commutation). The plasma that is
formed between the grid and the
anode diffuses back through the
grid into the grid-cathode space.
"Connection" of the plasma in the
anode-grid space with the plasma
in the cathode-grid space completes the commutation process.
The commutation process is simply modeled as shown in Figure 2.
The time interval between trigger
breakdown of the grid-cathode
region and complete closure of
the thyratron is called the anode
delay time. It is typically 100-200
nanoseconds for most tube types.
During commutation, a high voltage spike appears at the grid of
the thyratron. This spike happens
in the time it takes for the plasma
in the grid-anode space to "connect" to the plasma in the gridcathode space. During this time,
the anode is momentarily "connected" to the grid thereby causing the grid to assume a voltage
nearly that of the anode’s.
Although the grid spike voltage is
brief in duration, usually less than
100 nS, it can damage the grid
driver circuit unless measures
are taken to suppress the spike
before it enters the grid driver circuit. The location of the grid spike
suppression circuit is shown in
Figure 3, Grid Circuit.
Figure 4, Typical Grid Spike
Suppression Circuits, shows the
more common methods used to
protect the grid driver circuit. In
using any of these types of circuits, care must be exercised to
assure that the Grid Driver Circuit
pulse is not attenuated in an unacceptable manner. The values for
the circuit components are
dependent on the characteristics
of the thyratron being driven, the
e
e
1. Trigger pulse applied
to control grid.
2. Grid-cathode breakdown.
Propagating
Plasma Front
3. Electrons from grid-cathode
region create a dense plasma
in the grid-anode region. The
plasma front propagates toward the cathode via breakdown of gas.
Figure 2. Thyratron commutation
4. Closure
grid driver circuit design, and the
performance required from the
thyratron itself. Contact the applications engineering department at
PerkinElmer to discuss the specific details of your requirement.
Conduction
Once the commutation interval
has ended, a typical hydrogen
thyratron will conduct with nearly constant voltage drop on the
order of 100 volts regardless of
the current through the tube.
Recovery
Thyratrons open (recover) via
diffusion of ions to the tube inner
walls and electrode surfaces,
where the ions can recombine
with electrons. This process takes
from 30 to 150 microseconds,
depending on the tube type, fill
pressure, and gas (hydrogen or
deuterium). The theoretical maximum pulse repetition rate is the
inverse of the recovery time.
Recovery can be promoted by
arranging to have a small negative DC bias voltage on the control grid when forward conduction has ceased. A bias voltage of
50 to 100 volts is usually sufficient.
Recovery can also be improved
by arranging to have small negative voltage on the anode after
forward conduction has ceased.
In many radar circuits, a few-percent negative mismatch between
a pulse-forming network and the
load ensures a residual negative
anode voltage. In laser circuits,
classical pulse-forming networks
are seldom used, so inverse
anode voltage may not be easily
generated. Recovery then strongly depends on the characteristics
of the anode charging circuit. In
general, charging schemes
involving gently rising voltages
(i.e., resonant charging and ramp
charging) favor thyratron recovery, and therefore allow higher
pulse repetition rates. Fast ramping and resistive charging put
large voltages on the anode
quickly, thus making recovery
more difficult. The ideal charging
scheme from the viewpoint of
thyratron recovery is command
charging, wherein voltage is
applied to the thyratron only an
instant before firing.
CURRENT LIMITING AND/OR
MATCHING RESISTOR
GRID SPIKE
SUPPRESSION CIRCUIT
GRID DRIVER
CIRCUIT
Figure 3. Grid Circuit
(a)
Filter
(b)
Zener
(c)
MOV
(d)
Spark Gap
Figure 4. Typical Grid Spike Suppression Circuits
Thyratrons
RMS
Anode
Current
lp (Aac)
Plate
Dissipation
Factor
Pb
(x 109)
Cathode
Heater
V/A
Reservoir
Heater
V/A
Peak
Forward
Grid
Voltage
egy
(Min)
Impedence
of Grid
Circuits
g (Max)
EIA Type & Comments
Notes
Seated
Height x
Tube Width
(Inches)
1
2.35 x 1.0
Peak
Anode
Voltage
epy (kV)
Peak
Anode
Current
ib (a)
Average
Anode
Current
lb (Adc)
HY-2
8
100
0.1
2
2.7
6.3/3.5
Note 1
175
1200
JAN 7621
HY-6
16
350
0.5
6.5
5
6.3/7
6.3/2.5
150
1500
JAN 7782
2 x 1.4
HY-60
16
350
0.5
6.5
5
6.3/7
6.3/7
150
1500
JAN 7665A
2.4 x 1.4
HY-61
16
350
0.5
6.5
5
6.3/8.5
Note 1
150
1500
HY-10
20
500
0.5
8
10
6.3/7.5
6.3/4
200
500
HY-11
18
1600
0.5
8
10
6.3/7.5
6.3/4
200
500
HY-1A
18
500
0.5
8
10
6.3/11
Note 1
175
500
1
5x2
HY-1102
18
1000
0.5
16
10
6.3/7.5
6.3/8
20
500
2
2x2
HY-3192
32
1000
2.2
47.5
50
6.3/12.5
6.3/5.5
1500
250
3
3.75 x 3.25
HY-32
32
1500
2.2
47.5
50
6.3/18
6.3/5.5
450
400
4
4 x 3.25
HY-3204
32
1500
1
25
40
6.3/18
6.3/6
450
400
ib to 10kA @ <1usec
4
3x6
1802
25
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
400
JAN 7322
4
4 x 3.25
HY-3002
25
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
400
HY-3003
35
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
400
4 x 3.25
HY-3004
25
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
400
4.75 x 3.25
HY-3005
35
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
400
HY-3025
28
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
250
HY-3189
32
5000
2.2
47.5
50
6.3/12.5
6.3/5.5
500
250
HY-5
40
5000
8
125
160
6.3/30
4.5/11
1300
100
HY-53
40
5000
4
90
100
6.3/30
4.5/11
1300
100
LS-3101S
35
5000
2
45
50
6.3/18
6.3/6
500
LS-4101
40
12000
3
55
50
6.3/28
6.3/6
500
LS-4111
40
12000
3
55
100
6.3/28
6.3/6
HY-3246
45
15000
2
45
50
6.3/16
LS-3229
70
15000
2
45
50
HY-3202
32
20000
0.5
47.5
50
LS-5001
40
20000
4
90
LS-5002
50
20000
4
70
Type
1
3.6 x 1.4
3.4 x 2
JAN 7620
2.2 x 2.25
JAN8613
4 x 3.25
3
4.75 x 3.25
4.25 x 3.25
3.75 x 3
5 x 4.5
8614
3
5 x 4.5
250
6
5.25 x 3
250
3,6
8 x 3.5
500
250
3.5,6
8.25 x 3.5
6.3/6
500
250
6.3/16
6.3/6
450
400
3,6
6.3/18
6.3/13
500
250
2,6
6.4 x 3
100
6.3/29
4.5/10
2500
50
3
6.75 x 4.5
100
6.3/35
4.5/15
2500
100
5.75 x 3
Two gap tetrode
Two gap tetrode
6.4 x 3
3
9.5 x 4.5
LS-5101
40
20000
4
90
100
6.3/29
4.5/10
2500
50
3,6
6.75 x 4.5
LS-5111
40
20000
4
90
200
6.3/29
4.5/10
2500
50
3,5,6
7.2 x 4.5
Notes
1.
2.
3.
4.
5.
6.
Cathode and reservoir heater internally connected
Grounded grid design
Auxiliary grid design
MT-4 mount required
Liquid cooling design
Hollow anode design for reverse current
PerkinElmer thyratron control grid driver TM-27 recommended for use with all thyratrons up to 3 inch diameter. TM-29 recommended for thyratrons greater than 3 inch diameter.
The selections above are a representative sample of hundreds of design variations available. Contact PerkinElmer for support for any specific application.
Definition of Terms
TERMS USED TO CHARACTERIZE INDIVIDUAL PULSES
Peak Anode Voltage (epy): maximum positive anode voltage, with respect to the cathode.
Peak Inverse Anode Voltage (epx): maximum negative anode voltage, with respect to the cathode.
Peak Forward Anode Current (ib): maximum instantaneous positive anode current.
Peak Inverse Current (Ibx): maximum instantaneous negative anode current.
Pulse Width (tp): current pulse full-width at half-maximum.
Pulse Repetition Rate (prr): average number of pulses/second.
Current Rise Time (tr): time for the forward current to rise from 10% to 90% of its peak value.
Anode Fall Time: time for the forward anode voltage to collapse from 90% to 10% of its maximum value.
Anode Delay Time (tad): time interval between triggering and commutation (commutation is defined below). The precise
reference points for this interval vary with the application.
Anode Delay Time Drift (∆tad): gradual decrease in anode delay time that occurs as the thyratron warms up.
Jitter (tj): pulse-to-pulse variation in anode delay time.
TIME AVERAGED QUANTITIES
DC Average Current (Ib): forward current averaged over one second.
RMS Average Current (Ip): root-mean-square current averaged over one second.
Plate Breakdown Factor (Pb): numerical factor proportional to the power dissipated at the anode, averaged over one
second. Pb = epy x ib x prr.
STRUCTURAL PARTS OF THE THYRATRON
Auxiliary Grid: grid placed between the control grid and cathode in some thyratrons. A small DC current (or a larger pulsed
current) applied between Auxiliary Grid and cathode can be used to control the anode delay time. (Anode delay time is
defined above). Thyratrons with auxiliary girds are called Tetrode Thyratrons.
Reservoir: maintains the gas pressure in the tube at a level which depends on the reservoir heater voltage.
GENERAL TERMINOLOGY
Static (Self) Breakdown Voltage (SBV): applied voltage at which a thyratron will break down spontaneously, without
being triggered.
Commutation: transition from trigger breakdown to full closure of the thyratron.
Recovery Time: time which must elapse after decay of the circuit current before anode voltage can be reapplied to the
thyratron without causing self-breakdown. The maximum possible pulse repetition rate is the inverse of the recovery time.
Grid Bias: negative DC voltage which may be applied to the control grid to speed up recovery.
Marking
PerkinElmer’s trademark, part designation, and date code.
PerkinElmer welcomes inquiries about special types. We would be pleased to discuss the requirements
of your application and the feasibility of designing a type specifically suited to your needs.
For more information email us at [email protected] or visit our web site at www.perkinelmer.com/opto
Note: All specifications subject to change without notice.
USA:
PerkinElmer Optoelectronics
35 Congress Street
Salem, MA 01970
Toll Free: (800) 950-3441 (USA)
Phone: (978) 745-3200
Fax: (978) 745-0894
.
DS-247 Rev A 0901
© 2001 PerkinElmer, Inc. All rights reserved.
www.perkinelmer.com/opto