I’ve recently been working on getting the six engine gauges for the F-15 put together. Since I’m not going to be using real instruments, I needed to scratch build them. Last year I did a short demo that shows how I’m using a small OLED display to emulate the “odometer” style display that’s used in the Fuel Flow, Temperature and RPM gauges. I finally got around to doing the software integration and did a short video that shows both the air core and the OLED display working together:
Some weeks later, the boards I ordered from Osh Park arrived and I got the first one soldered up.
This is the top of the new interface board. The chip in the center is an LM293DD dual h-bridge chip. This is the surface mount version of the LM293D that I bread-boarded the circuit on. The header on the right goes to the OLED interface.
The bottom of the board has a four pin connector that will go to the air core motor.
This is what the final assembly looks like after the Arduino Nano has been mounted.
The USB connector is at the back end of the board and will be accessed through an opening in the back of the instrument. I’m still working on the design for the instrument core, so I don’t have much else to show yet.
I don’t know if this update qualifies as a “milestone” or not, but I finally finished and installed the wiring harness for the right side console!
The adventure started this morning with the construction of the wiring harness for the recently finished TEWS panel. This consisted of cutting, stripping and adding pins & sockets to the 22 wires that are used by the TEWS panel.
Wow. It’s been a while since I’ve posted an update! Since the last update, I’ve nearly finished the re-wire job for the right side console. I was fortunate enough to get a pile of brand new canon plugs and matching pins. This is allowing me to re-wire the cockpit using the original bulkhead connections, which makes for a much neater build! In order to build the wiring harness, I’ve had to build it out panel by panel. With the completion of the TEWS panel, the wiring harness will be completed. The only thing missing will be the CMD panel that controls how the chaff & flare dispensers behave. I’ve never been able to get a photo of that panel, so I’m going to hold off until I do and can make a new one from scratch.
The navigation control panel is going to be a stand-alone, USB interfaced device due to its complexity. That should be an interesting rebuild.
I started the TEWS panel rebuild nearly 3 years ago, which is kind of embarrassing. In my defense, I DO have a lot going on. There’s good reasons it’s been 15 years since this project started.
When I first wrote about the TEWS panel, I pointed out that I needed to replace the two destroyed Korry “FAIL” indicators that the panel had. I decided to go a different route than the Korry replacement I built for the IFF panel.
First up, here’s what the new SFS interconnect cable looks like:
The end of the cable on the right is bolted to the cockpit floor and the other end winds its way along the pitch axis bearing and up the centerline of the roll axis section. It attaches to the bottom of the SFS box in order to bring the signals from the SFS box & grip to the control interface hardware that’s going to be installed in the left side equipment bay that’s under the cockpit. The clear plastic tube was part of the original SFS interconnect cable. I was able to salvage it for the new cable.
Above is a shot of the SFS end of the cable right before I closed up the outer sleeve.
I’ve been working on getting the inboard throttle grip rebuilt. Having friends in interesting places helped out quite a bit with this part of the project. The F-15C inboard grip contains a “slew” control, which is essentially a tiny little force sensitive joystick. It’s used as the Target Designation Cursor controller. You can see it in the photo below, the “L” shaped object.
The slew control requires an input amplifier because the signal it puts out is very, very tiny. This is where my smart buddies come in. They make an interface board that is specifically designed to turn these slew controllers into joystick axes. The board supports the slew control as the main x/y axis and has a few other goodies on it that make for a complete joystick interface. Below is a pic of that board.
A few people have emailed me asking about more information on the slew control -specifically the pinout. Here you go!
Pin 1 – 5VDC
Pin 2 – X Axis
Pin 3 – Y Axis
Pin 4 – GND
I should also note that one the folks that emailed me was able to successfully get the slew control working by using the analog inputs on an Arduino!
After a very, very long delay, the SFS box is finally finished. There’s literally nothing left that needs to be done for it.
From last weekend’s work, here’s the last two stages of wiring.
First, lace it up!
Then it gets cleaned up and attached to the interior of the SFS box.
I use a LOT of waxed lacing cord. It makes for a very nice looking wiring harness and doesn’t snag on everything like a nylon wire tie will.
The next three photos show the completed SFS box with the grip attached.
And finally, here’s what it looks like installed in the cockpit!
I really, really need to dust.
This past weekend saw some renewed effort on the project. For the last 18 months I’ve been up to my neck in 3D printer things – I’ve been writing the assembly and user guides for SeeMeCNC’s line of excellent 3D printers. http://www.seemecnc.com
One of the things I got done was to finish the missing pawls for the throttle quadrant and get them installed. These pawls act as both an idle gate bar and as a trigger for the engine start switch. In order to pull back past the idle gate, you need to pull up on the finger lift. This prevents you from accidentally cutting fuel off to the selected engine when pulling the throttle fully aft. When starting the engines, you pull up a finger lift and the pawl activates a microswitch that in turn causes the JFS to link the AMAD to the selected engine.
Here’s the new pawls – the originals were sold unfortunately.
Here’s a photo of what the new parts look like installed:
#1 is the idle gate. When the pawl is forward of it, you can’t pull the throttle arm fully aft without lifting the pawl over it.
#2 is the engine start switch. When the pawl is aft of the idle gate, pulling up the finger lift will cause the pawl to engage the switch. The sides of the pawls are 3D printed from ABS plastic. I may replace those printed parts with machined aluminum before installation back in the cockpit.
The other thing I got accomplished was the fitting out of the SFS box! That’s been a long drawn out project for sure! I got the Nosewheel Steering/AP Disconnect paddle & switch installed on Saturday and I completed the wiring & other assembly this evening.
Here’s the start of the process:
The Post-MSIP II grip I have uses 23 wires to cover the six switches on the grip. An additional two wires are needed for the NWS/AP Disc. paddle. The silver connector shown above is the female connector that the grip mates to and was a surplus item a friend scored for me. The very “used” looking connector behind it was the floor-mounted end of the SFS wiring harness that went from the cockpit floor up to the bottom of the SFS box. Since the connectors are insanely expensive (roughly $175 for this one), I decided to re-use existing connectors whenever I could. The other end of the SFS wiring harness will mate to this connector and while the floor connector will be different, it will be nearly impossible to tell it’s not original. This wiring job was a one-way task. I had inadvertently used 22ga wire instead of 24ga and didn’t realize it would be a problem until I’d put all the female crimp-on connectors in place. The pin removal tool I have is too small to fit the 22ga insulation properly, thus making the pin insertion a permanent deal. The pin & socket insertion process took about 20-30 minutes – I did NOT want to make a mistake that would either ruin a connector or cause me to have to cut and splice out a mistake. Fortunately, I got it right. I think.
Here’s what the result looks like:
All that remains is for the bottom connector to be screwed into place and then the wiring needs to be wrapped up in lacing tape and tied to the interior of the SFS box.
The final step will be to install the machined Delrin installation post I made a few years ago and get it properly drilled so I can bolt the SFS box to the lower stick assembly. That should be done this coming Saturday and I’m really, really looking forward to it!
That’s video of the airshow where the accident occurred that resulted in the cockpit section being snapped off the aircraft just aft of Bay 5.
I’ve probably linked to this video before, but I figured someone that had never seen it before might be interested.
Here’s the Radio Call plates:
The font isn’t exactly right, but it’s all I’ve got to work with. All the searches I’ve done for the right font only come up with the one that Derek Higgs did for the Simpits group in 2000.
Landing gear handle panels – I flipped one over so you can kind of see the pocket work done on the back side. A tiny single-sided PCB with warm-white LEDs will light this up nicely (and make it a Type VII edge-lit panel)
Here’s what it looks like on the landing gear handle:
I don’t have the right screws for this – #4-40 are very loose, #6-32 are too tight. I’m not quite sure what the right screw is at this point.
Hopefully tomorrow I’ll post pics of the replacement TEWS panel.
Way back in March, I showed the starting process to how I built new edge-lit panels for the F-15.
I finally was able to get enough time away from doing 3D printer work to get some panel work done!
(The sad thing is, I bought the Rostock MAX to build parts for this and my other projects. Since it arrived I’ve pretty much done nothing but 3D printer oriented stuff…)
Here’s the new Jet Fuel Starter panels.
The new panels are on the left, the old panel is on the right. There’s a few differences between them, but they’re dimensionally identical. The “L” on the far left panel didn’t completely engrave, so I’ll need to touch that up by hand.
The original JFS panel has three 5V lamps that are embedded in the back of the panel. In order to do any repairs to it, you need to use a motorized tool to grind out the “potting” material in order to reach the lamps and their wiring. I suspect that the potting compound is clear, but I’ve never torn apart a panel to find out. Maybe some time I’ll grab an old commercial airliner panel I have and tear it apart. For Science!
Here’s what the new Nav edge-lit panels look like:
This was my first go-round at doing two-color panels. There was some paint bleed and in a few points, masking failure. I’ll touch these up by hand using a magnifying glass and a very fine detail brush. If you didn’t know, the real panel is in the center.
I’ll post pictures of the other panels when I’ve got them completed. I think there’s only one more to finish – it’s a two-color panel as well and fits on the fire suppression panel.
|Parameter Name||Source||Range||Resolution||Samples Per Second|
|Left Aileron Position||Transducer||+/- 20 deg||0.05 deg||53.33|
|Right Aileron Position||Transducer||+/- 20 deg||0.05 deg||53.33|
|Left Stabilator Position||Bus – 16 bit||-30deg to +15 deg||0.006 deg||26.66|
|Right Stabilator Position||Bus – 16 bit||-30deg to +15 deg||0.006 deg||26.66|
|Left Rudder Position||Transducer||+/- 3 0deg||0.04 deg||53.33|
|Right Rudder Position||Transducer||+/- 30 deg||0.04deg||53.33|
|Speed Brake Position||Transducer||0 to 45 deg||0.03 deg||53.33|
|Longitudinal Stick Force||Transducer||+/- 25lbs||0.04lbs||53.33|
|Lateral Stick Force||Transducer||+/- 20lbs||0.05lbs||53.33|
|Longitudinal Stick Position||Transducer||-3 to 6in||0.008in||53.33|
|Lateral Stick Position||Transducer||+/- 4in||0.007in||53.33|
|Right Rudder Pedal Force||Transducer||+/- 200lbs||0.3lbs||53.33|
|Left Rudder Pedal Force||Transducer||+/- 200lbs||0.3lbs||53.33|
|Right Rudder Pedal Position||Transducer||+/- 4in||0.02in||53.33|
|Left Rudder Pedal Position||Transducer||+/- 4in||0.02in||53.33|
|Right Power Lever Angle||Transducer||0deg to 130deg||0.09deg||6.66|
|Left Power Lever Angle||Transducer||0deg to 130deg||0.09deg||6.66|
|Left Fuel Flow||Transducer||0 to 100,000 lbs/hr||0.024 lbs/hr||6.66|
|Right Fuel Flow||Transducer||0 to 100,000 lbs/hr||0.024 lbs/hr||6.66|
|Left Fuel Flow||Transducer||0 to 100,000 lbs/hr||0.024 lbs/hr||6.66|
|Left Engine Nozzle Area||Transducer||2.5 to 65 sqft||0.022 sqft||6.66|
|Right Engine Nozzle Area||Transducer||2.5 to 65 sqft||0.022 sqft||6.66|
|Left Core Speed (N2)||Production System||0 to 110%||0.2%||53.33|
|Right Core Speed (N2)||Production System||0 to 110%||0.2%||53.33|
|Pressure Altitude||Bus – 16 bit||-1,560 to 80,337ft||1.25ft||26.66|