|
| |
 |
|
This test report presents the
data and describes the procedures
for testing the current-carrying
capacity for QA's test probes.
This information is useful for
test and design engineers when
calculating probe requirements
for high current and temperature
applications.
Measure the current capacity
of test probes. Two types of tests
were performed; both were simulations
of common applications for probes.
The first tested a solitary probe
mounted in a G10 fixture plate,
while the second tested a group
of probes (3x3 grid pattern).
|
|
|
Probe Series |
Center Spacing |
Plunger Travel |
|
025-16 |
.025 [0.63] |
.160 [4.06] |
|
039-16 |
.039 [1.00] |
.160 [4.06] |
|
050-05 |
.050 [1.27] |
.050 [1.27] |
|
050-16 |
.050 [1.27] |
.160 [4.06] |
|
050-25 |
.050 [1.27] |
.250 [6.35] |
|
075-25 |
.075 [1.91] |
.250 [6.35] |
|
075-40 |
.075 [1.91] |
.400 [10.16] |
|
100-05 |
.100 [2.54] |
.050 [1.27] |
|
100-16 |
.100 [2.54] |
.160 [4.06] |
|
100-25 |
.100 [2.54] |
.250 [6.35] |
|
100-40 |
.100 [2.54] |
.400 [10.16] |
|
125-25 |
.125 [3.18] |
.250 [6.35] |
Dimensions
are in in. [mm] |
|
The current-carrying ability
of a probe is measured with respect
to probe temperature. The upper
temperature limit of a spring
probe is determined by the spring
material. Springs which are made
of music wire can be used without
adverse effects up to 250° Fahrenheit
[120° C]. Although stainless steel
springs are also used in QA probes
and can withstand temperatures
up to 400° F [204° C], 250° F
[120° C] is used for the upper
temperature limit since the probe
user may not always be certain
of the spring material.
A controllable
DC current source was used to
provide a constant current through
the probe and socket assembly
being tested, while a thermocouple
was used to track the temperature
of the probe. The current was
increased in one Ampere intervals
(one-half intervals for the 039-16
and 025-16 Series), and sufficient
time was allowed between increases
for the temperature to stabilize.
As current increased, probe temperature
increased, and testing continued
until the 250° [120°C] Fahrenheit
threshold was reached.
For the first test, a solitary
probe was oriented as shown in
the sketch below. A probe from
each series was mounted in a 5/16"
block made of G10. The block stood
horizontally on four legs, and
airflow was blocked by baffles
arranged around the test block.
| |
| Setup
for measuring current
versus temperature
for a single probe/socket
assembly. |
A type K thermocouple was used,
with 40 AWG (.003 [.08] diameter
conductor) Chromel/ Aluminel wire
connected to the socket just below
the bottom surface of the mounting
plate. The .003 [.08] wire diameter
minimized heat transfer from the
socket and reduced response time.
Wires for supplying current to
the probe were 20 AWG or greater.
One current supply wire was connected
directly to the tail of the socket.
The other was connected to a solder-coated
plate which was in contact with
the probe tip. This contact plate
was mounted such that the probe
was compressed to its rated 2/3
stroke. The test set up was intended
to closely simulate typical applications
for test probes.
The second test (probe groups,
3x3 Grid), nine probes and sockets
were mounted on a three-by-three
grid of the appropriate center
spacing. All nine probes were
wired in series by connecting
the appropriate socket tails,
and by selectively jumping the
tips in succession with a solder-coated
plate simulating a typical printed
circuit board. In this way, the
same current was assured to run
through all nine probes. The thermocouple
was connected to the center socket
at the same location as in the
previous test. |
| |
|
|
|
The plotted graphs compare the
temperature versus current for
all of the probe series. The sockets
used for each series are listed
in the table, the 100-25 Series
were all tested in 100-SDN250S
sockets with exception to the
100-PRH2509S probes which were
tested in 100-SDH250W sockets
and plotted on the 100-25 Series
graphs. Additional tests included
the testing of the various spring
forces and varying the stroke
lengths for the 100-25 Series.
Complete numeric test results
are available. |
|
|
|
| 025-SBP160C-3 |
Flush |
| 039-SDC165J |
.150
[3.81] |
| 050-SBB050C-6 |
Flush |
| 050-SBB160C-6 |
.150
[3.81] |
| 050-STB255C-6 |
.150
[3.81] |
| 050-SRB255C-6 |
.150
[3.81] |
| 075-SDN250W* |
.150
[3.81] |
| 100-SDN050W |
Flush |
| 100-SDN160W |
.150
[3.81] |
| 100-SDN250S* |
.150
[3.81] |
| 100-SDH250W |
.150
[3.81] |
| 125-SDN250S |
.150
[3.81] |
| * Both the .250" and .400" stroke probes
use the same socket. |
|
| |
|
|
-
As the group data shows,
higher probe densities decrease
the probes current carrying
ability. This is due to the
combined heat generated by
the probes and the decrease
of air circulation via natural
convection. Because each application
is unique, it is recommended
that appropriate tests be
conducted before probes are
put into service in applications
with high currents, high probe
densities or limited airflow.
-
These temperature measurements
were made in the absence of
any forced convection. Providing
airflow (by means of a fan,
for example) around the sockets
will reduce the temperature
for a given current. Also,
tests have shown that the
airflow present due to leaks
in a typical vacuum fixture
will reduce temperature.
-
For conditions where the
ambient temperature differs
from the 75° F [24° C] ambient
of these tests; shift the
data by the same amount that
the ambients differ to determine
whether the 250° F [120° C]
limit is exceeded. For example,
a 100-25 series probe with
a P tube operating in an environment
with an ambient temperature
of 120° F [49° C] will exceed
250° F [120° C] at 7 Amps
(instead of 14 Amps at 75°
F [24° C] ambient).
-
Differences in current carrying
capacity for various springs
are not significant.
-
Differences in current carrying
capacity for various strokes
are not significant.
-
Note that although the probe
will not be damaged from operation
at temperatures up to 250°
F [120° C], some types of
plastics used as mounting
plates will not withstand
this temperature. Also, the
operator must be protected
against contacting probes
at high temperatures.
-
This data reflects performance
at 100% duty cycle. Higher
currents can be carried for
pulses of short duration.
For simplicity, apply higher
currents for no longer than
one second (longer pulses
may be carried, but require
that thermal inertia and rate
of temperature gain be known).
For example, the electrical
resistance of 100-PRH2509S
in 100-SDH250W averages 7
milliohms and carries a maximum
current of 20A; it is able
to continuously dissipate
a maximum of 2.8W (P=I2R).
At 50A, it would dissipate
about 17.5W, which means the
duty cycle must be reduced
to 16%. So, to avoid overheating
this probe at 50A, power must
be applied for no more than
160 milliseconds (1 second
x 16%).
- For comparison, note that
a Kynar-insulated solid copper
wire the same diameter as a
100-25 Series probe tube (.054
[1.371]) reaches 250° F [120°
C] at 29A.

025-PRP1641S |

039-PRP1614S-S |

050-PLP0513S
|

050-PLP1609S
|

050-PTP2509S
|

050-PRP2509S |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe |

Multiple Probes
3x3 Grid |

Single Probe
100-PRP2509
L, S, H, Y & X Springs
|

Multiple Probes
3x3 Grid
100-PRP2509
L, S, H, Y & X Springs
|

Single Probe
Variable Stroke Lengths
100-PRP2509S |

Multiple Probes
3x3 Grid
Variable Stroke Lengths
100-PRP2509S
|
|
|
|
| |
|
|
| |
|