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Photos of Kearfott Ring Laser Gyro-Based Inertial Reference Units
[Only about 3 people per decade visit the Laser Equipment Gallery ;-),
the existing format was archaic, and I am lazy. So going forward,
we will use the Windows App "Web Album Generator" for most of the
collections.]
Note: Most links open in a single new tab or window depending on your
browser's settings.
These are photos of Kearfott navigational Inertial Reference Units (IRUs)
or parts of them that use HeNe laser-based Ring Laser Gyroscopes (RLGs).
Only two samples of one model at present.
Note that the terms Inertial Reference Unit (IRU) and Inertial Measurement
Unit (IMU) may be used interchangeably. The Kearfott Website uses IMU; the
label on the actual device has IRU. Go figure. ;-)
Kearfott Inertial Reference Unit K600A374-01
This is a complete system,
probably intended for "Sea Navigation" - e.g., in submarines, larger UAVs, and
the like. For ships, the Z axis would be largely wasted. ;-) Exactly
what the difference is compared to "Land Nav" systems is probably more
in the interfaces and other capabilities than the specific functions.
The primary physical diffference appears to be of the paint color in the
Kearfott brochures: Land Navs are black; Sea Navs are biege. I suppose
that black doesn't show dust and dirt like a light color would. ;-)
Kearfott Inertial Reference Unit: Outside (left), Inside Labeled (center), Inertial Sensor Assembly, Platform (ISAP, right)
For much more information on this IMU, go to
Kearfott K600A374-01 IMU
with Monolithic Block Triple RLG.
Kearfott Inertial Reference Unit K600A374-01 #1
(The photos in the first Web album are courtesy of Ismael Tremblay.)
See Kearfott Inertial
Measurement Unit Assembly K600A374-01 #1 (Web Album, 25 photos).
The RLUs in this IRU are interesting because all three axes are fabricated
in a single block of special low expansion glass or similar material. The
accelerometers are totally separate. At present not much else is known
other than that the RLGs do power up, at least briefly.
The last pic shows an ideal application for this IRU. ;-)
Kearfott Inertial Reference Unit K600A374-01 #2
This one (#2) is mine and is believed to be identical to #1. In fact, their
serial numbers differ by only 5. ;-) However, rather than disassemble the
RLG Block of #2, Ismael Tremblay kindly loaned me his RLG Block for the
photos. So everything up until the clothes come off the RLG Block are of mine
while the naked photos are of his unit.
But first, here are some short videos of what happens with the RLG Block when the IRU is powered. Click on
the small image to see the corresponding video.
Overall Setup for Powered ISAP RLG Block Photos (left) and Closeups
These show the naked RLG Block from IRU #1 tethered to the power supply and electronics from IMU #2. Minor
rearrangement and camera angle variations are used for all the powered photos in the Web Album, below.
The first audible click in the videos occurs when power to the IRU is first switched on, the RLG Block glows
bright three times over approximately three seconds starting around the mid-point, and the second click is
power off. They do get rather boring after almost no time at all. ;-)
And now for the good stuff. ;-)
See Kearfott Inertial
Measurement Unit Assembly K600A374-01 #2 (Web Album, 90 photos so far).
Description of the Web Album photos for #2:
- Overall views (Front, Right, Front_Right, Right, Back_Right, Back,
Back_Left, Left, Front_Left): These are virtually identical in appaerance
to the sample on the Kearfott Website in the year 2025 under "Sea Nav IMUs".
- Closeups of the five military-style circular connectors:
- J1 (66 pins): Control / Signal / Information.
- J2 (15 pins): Power input. 28 VDC nominal, 30 W max. 24 VDC OK.
+Vin: Pins A,B; -Vin: Pins M,N. Case GND: Pin P. No other pins used.
- J3 (13 pins): ????
- J4 (22 pins): ????
- J5 (13 pins): ????
(J3 and J5 have the same pin configuration but are keyed differently.)
- Label: This has both the numbers as described above.
- Indicator: This is also visible in the lower right corner
of the Label photo. Originally I thought it was some sort of fancy optical
sensor because it does NOT look like a photodiode or LED. But the mystery has
been mostly solved after powering the unit multiple times for the photo
shoots and actually paying attention to what it does, which would appear
to simply be a high priced mil-spec LED in a hermetic package no doubt
costing the U.S. Taxpayer BIG BUCKS. It turns on bright green a couple seconds
after power is applied to the IRU. Whether it is simply a fancy Power LED or
something more sophisticated is not known.
- Caution Label: Like we didn't know. ;-)
- Inside Top: This is what greets you after removing the cover. It's
a very clean layout with only 3 or 4 major subassemblies (depending on how
they are counted): Main PCB Assembly (top of photo, mostly hidden),
"Inertial Sensor Assembly, Platform" (ISAP, the round can on elastomer mounts,
lower left) - the heart with the ring laser gyro block and accelerometers;
and the power input, conditioning, and interface modules (lower right).
- Main PCB in Situ: What's visible is the top PCB; a similar size
board is mounted on the other side of the aluminum frame.
- Connector PCB in Situ: At least for some of the connectors.
- Top Main PCB: Some LSI parts but mostly smaller ICs. The
black polka-dot rectangular affair at the right is the high voltage power
supply for the RLG and possibly the PZT.
- Bottom Main PCB: More chips including a Texas Instruments TMS320
DSP. I would guess that the black painted-over 32 pin packages contain the
firmware. ;-)
- Power Connector Module Inside: This is what is behind J2. It
shows the very simple but almost impossible to follow wiring due to the
use of all white insulation. ;-)
- Power Filters: These appear to be RFI-type filters for the
input power. (Look up their Martek part numbers!) Also visible is the Power
Connector Module.
- DC Power Converter: This is another readily identifiable Martek
module. It is a DC-DC converter that takes 28 VDC (nominal) and provides
+5 VDC and ±15 VDC for all the electronics. The spec is actually
14 to 40 V in, so fortunately it will run happily off 24 VDC, which is
a lot more common for powering on the bench with a fixed supply. ;-)
- Interface PCB: Function of this PCB is unknown but it has a bunch
of opto-isolators on it so it must have something to do with interacing in
a nasty electrical environment.
- RLG HV Connector: This is really just a white wire with high
voltage insulation and a female contact secured with a black plastic cap
for the HeNe lasers inside the RLG block and possibly the dither PZT.
- ISAP in Situ: Another view.
- ISAP with Mounts: Front, Right Side, Back, Left Side, Top,
Bottom. The upper cable is for the RLG, the lower cable is
for the accelerometers. The +HV socket for the RLG is also visible.
- ISAP Label: And S/N 670. ;-)
- Inertial Measurement Unit Labeled: And an interior
view with major assemblies annotated. ;-)
- ISAP Housing Mounts Shroud: Exposing the cylinder with the RLG
block and accelerometers
The purpose of the Shroud is not entirely obvious as it is not structural.
But it is made of a thin soft ferrous material which is perhaps
Mu-metal, and thus may be a serving as a magnetic shield. It is
conceivable that even weak magnetic fields could affect the behavior of
the lasers in the RLG at the margins of precision. If that isn't its
function, it must be to make disassembly more annoying. ;( ;-)
- ISAP Shroud Label: The wording of the label on the shroud is strange
(and probably unrelated to the shroud itself): "KEARFOTT
CORPORATION IS THE INITIAL TRANSFERER OF THIS PRODUCT, WHICH CONTAINS
THORIUM LICENSED UNDER 10 CFR 40.13(c)(i)(ii)". It's even stranger looking
up the definition of 10 CFR 40.13. ;-) 10 CFR 40 is part of the
"Code of Federal Regulations" dealing with nuclear
energy. ;-) Part 13 states that the company is
exempt from regulations because there is very little of the stuff present.
Thorium is a weak Alpha emitter so a trace amount may have been placed inside
the RLG block to assist starting of the HeNe lasers. Any Alpha particles
would be totally blocked by the block (no pun intended intentionally)
so forget your Gieger counter. ;-)
- ISAP RLG PCB Top: The RLG monolithic block is below this PCB. The
wires in the 3 ribbon cables (5, 6, 7 wires each) and 3 sets of individual
orange, yellow, and green wires need to be carefully unsoldered to remove the
PCB. That's a total of 27 wires and they are a lot thinner and closer
together than they appear
in the photos. In fact everything in the "can" (which is around 8 cm or
just over 3-1/8 inches in diameter) is actually much smaller than
it appears in the photos. ;( ;-) Detaching (and re-attaching) the wires
requires a steady hand, super fine tip soldering iron, and Mark II upgraded
eyeballs (or a good magnifier or microscope).
- ISAP Accelerometers with PCB: The three accelerometer units are
attached to a metal frame and wired to their respective PCBs.
- ISAP Accelerometer Interface ICs: A fancy part for each one. ;-)
This may be custom as the only hits via a Web search return info on an
older Kearfott IMU.
- ISAP RLG Block in Situ1: The visible portion of the RLG block
exposed when the accelerometer assembly is removed. Three of the six
mirrors are visible with their PZTs for cavity length control.
The purpose of the what appears to be Home Depot Fiberglas foam is not
known. It's very soft and fluffy and not
likely to provide much damping or thermal isolation.
- ISAP_RLG_Block_Insulation1: After removal. I hope the specific
locations of each clump were recorded.
- ISAP_RLG_Block_in_Situ2: And with the foam removed. When the
RLG lasers are powered there is 400-500 VDC on the central pillar as
well as the small test-point at the 1'oclock position. I wanted to
take photos of RLG Block powered in situ but for some reason, neither
the RLG discharges or PZT drive will come on with the cover in place
even if not attached. There is just a brief faint "weep" and it
then apparently aborts. ;( ;-)
- ISAP_RLG_Block_Cover1: Removing this is more than a matter of
three screws. There are 27 teeny wires that need to be carefully unsoldered.
And everything is must smaller and more closely spaced than it appears in
the photos.
- ISAP_RLG_Block_Top1-2: Two views almost straight down.
- ISAP_RLG_Block_Down1-6: Six Views at roughly a 45 degree angle.
- ISAP_RLG_Block_Side1-6: Six views at roughly a 15 degree angle.
- ISAP_RLG_Block_Not_Powered, Powered, and Dark_Powered: Several
sets of photos from various orientations and closeups showing the RLG Block
in room lighting, with the discharge powered, and the same in the dark.
Being tethered to the HV and RLG cables severely limits options for creative
photo composition. ;-)
The first set of three shows the setup for taking these photos with the naked
ISAP RLG Block next to its clothed buddy inside the IMU.
Since this IMU is not connected to anything except power, it does not stay
on for more than a few seconds. This is not thought to be a fault since
unit #1 does the same thing. So it's a feature, not a bug. At least
that is the assumption: Its microbrain expects some sort
of hand-shaking or acknowledgement and quits when this does not occur.
Further, the RLG Block is only powered three (3) times for a second or
so and then shuts off until the next power cycle. So the photos of the
RLG Block with the discharge glowing required applying power to the IMU
with the camera already focused and its shutter mode set to "Repeat". ;-)
- ISAP_RLG_Block_Central_Pillar1: This runs through the entire block
top to bottom and plays some role in powering the HeNe discharges as there
is -400 to -500 V with respect to the IMU case
on both the pillar itself and that little test-point at the 1 o'clock
position when the lasers are lit.
That would be consistent with the expected value of the discharge
voltage and the Central Pillar may indeed be the common cathode for all six of
the discharges. However, there is no direct or indirect DC connection to
it or the anodes or the ballast resistors, but there is a well insulated wire
leading into it from the HV Connector. It may also play a role in the
unlocking PZT.
- ISAP_RLG_Block_Ballast1: The blue resistors standing up
are one of three pairs that provide the main ballast for the HeNe discharges.
They are around 300K ohms each. Their common point is connected
to the other two pairs. The blue resistor laying down along with the
diode are believed to be related but exactly how is not clear.
- ISAP_RLG_Block_Tip-off1: This is where the air gets sucked out
and the HeNe gas mixture gets sucked in. ;-) Unlike some other RLG designs,
it is NOT a cathode. The glob covering it is to protect fragile humans as
the metal is very sharp after it is pinched off with several tons of force
forming a cold weld.
- ISAP_RLG_Block_Mirror+PZT1-3: These are closeups of the three
mirrors that are dithered for cavity length control. They are in no
particular order.
- ISAP_RLG_Block_Mirror+Detector1-3: These are closeups of the
three mirrors which have the interferometers combining the clockwise and
counter-clockwise beams and detectors for each of the three axes. They
are in no particular order.
- ISAP_RLG_Block_Schematic1: This diagram is derived from the
Kearfott patent and shows the arrangement of the mirrors and beam paths
inside the RLG Block. The leg length of the discharge paths in the
RLG Block is between 1.5 and 1.75 inches - it's difficult to measure
precisely or even if the geometry is a precise square. With 4 legs,
the result is a total ring cavity length of between 6 and 7 inches
for an enclosed area of between 2.25 and 3.0625 square inches.
Therefore, the sensitivity is higher than that of the Honeywell GG1320,
which has a two inch leg length but only 3 legs for a 6 inch ring cavity
length with an enclosed area of 1.73 square inches..
- ISAP_RLG_Block_Oriented_Similar_to_Schematic1: The photo was
rotated so that the locations of the mirrors are very approximately
like those in the schematic. More or less. ;-)