Showing posts with label Wiring. Show all posts
Showing posts with label Wiring. Show all posts

Friday, 20 December 2019

Wiring Washup

This blog is a wash up on the electrics and what when right and wrong for this builder.


It's a lot of wire regardless of what choices made
with component selection with tandem aircraft 
having just half the space to place that stuff in

Overview
Wiring, according to "Kitplanes" wiring has finished many a builder off. Having reached that stage of this project, this builder has come close many times. This blog will cover some of the good, most of the stupid that the builder created to reach the point where connections to the Circuit Breaker Panel could be manufactured.

Comments
Estimated runs determined and installed, this was covered in very early blogs and at this end, I would do the same. It went wrong with the final mix of wires, this was a function of the "guesstimate" of the requirements for the central cores but did not allow for the inter-connections.  This was due to a complete lack of any detailed design of the wiring, especially areas like the flap drive, controller, radios and stick. 

The factory used a Flybox controller, and all those connections are completed at the RS232 port located at the rear of the instrument. 

My choice of a separate module was a function of the panel being space poor and/or just the builder stuffing in stuff, and that has ramifications most that do not appear to later.

One choice that did work was the use of coloured wire. Still, it did create an issue in that many time the correct gauge was not on the shelf and supply was weeks away, white wire is readily available, and if doing it again, I would examine the use of 18/20 gauge white and a felt tip Sharpie pen to add a coloured stripe. 

This was used when exchanging 16 gauge for two 18 gauge for the flap power,  white as active and a black stripe was added to indicate earth by running the wire thru the tip of the pen. Black, black/white would be used for earth solely with red used for all actives.

The builder would try to use 18 gauge [10 amps] and 20 gauge [5 amps]  and forget wire smaller than 22 gauge except for specialized installations, and larger sizes would use red/black and red/white striped to indicate an active and earth.

A series of terminal strips were used to allowing wire from various equipment to be connected to their relevant power supply being either a circuit breaker of gang strip for active/earth. This enables the looms to behind the panel to be linked with the looms from the airframe at any point of assembly. 




The T shaped mount that the factory developed is a good idea as it allows a reasonable amount of area to mount the necessary hardware. On this install, the terminal strips were mounted vertically on 12 od x 20 mm high nylon spacers. These spacers are really good at creating more space by freeing up the deck of the main spine.







The negative is weight as the builder is sure that there are a few kilos of unneeded wire, terminals, brackets, and crimps. The cleanest method is to directly go-between the hardware and instruments, but diagnostics can be more challenging to undertake. 

One of the few good ideas was looming the cables in the PPS sleeve, while a little time consuming it created a series of defined cables to connect to the various points on the aircraft and for 95% of the time they just drop in.


Finally, they just look right and to burn this much effort, aka time, there must be something at the end as a justification.

Even though the panel is analog, all the instruments use a DB port of 9 or 15 pins allowing ease of connection and facilitating panel removal. 

Flying Legend has created as much maintenance access at the rear of the panel that would be practical and being able to put a panel of the bench in under 15 minutes just makes it all better. 

To do this, every connection has to be a plug and preferably a  DB - Why? - I have the tools. All the interconnections are then installed into the terminals strips creating ease of reorganization when required.

Another error was to use solder DB in the junction they made the work in the stick junction box a neverending nightmare. The use of the crimp pin type was considered but rejected initially because of the cost of the crimping tool, no change out of $US400. 

In the end, desperate people will try anything, and the pin crimper appears to work well for 20/22 guage in the crimps, but everyone has to be checked as about 10% fail. The real benefit is being able to swap pins to fix those stupid errors, this was covered in a Facebook post. 

Can a builder justify the cost of the correct crimper that a choice but so far so good?

All wires entering screw terminal block were fitted with pin sleeve that is crimped onto the end of the wire. The purpose is to protect the wire from the cutting action of the screw crimp.


This crimper is used with the sleeve crimps but has
seen duty with the DB pin crimps shown above

Adding the wiring to a DB15, four systems meet at this plug - this interaction has been the single biggest issue for the builder.

Initially, I used solder plugs because they were available BUT wasted a bucket of time in just trying to sort out the interconnections. In the end, the junction box for all the switches on the stock was removed then a terminal strip added. The plugs used on the external connections changed to the pin type, again for ease of attachment and correction.


Checking the junction box for all the control sticks
The addition of controls to the rear seat created more
work than the simple "yes" agreeing do it took.

Interconnections in the junction box

Would I use a junction box again, not if I could come up with a better idea, but at the time it seemed like a good idea? 


The terminal strips were mounted vertically to increase the available space, initially, these were fitted directly to the central member, but it was found that mounting these on 20 mm long nylon spacers allows the wires to be installed freely at the base. 

This frees the top enabling installation of the jumpers, which in turn allowed the looms to be tied to them with cable ties. The excess wire could be tucked under or run between rows freely.

A number of connectors were used in the assembly to allow various areas to be connected/ typically the wings to the fuselage, and circuit breaker panel to the main panel. For the smaller connections, Molex 2/3/4 pin were selected for their size and availability.

Most connections internally in the aircraft were AMP connectors to connect the circuit breaker panel and the wings with the Seal-All connectors. 

These were used in external areas like the wheel wells and for the rudder tail light.








Comments
Where was the most significant error and loss of time - well, several places stand out?

1 - Continuity, this is the biggest issue for this builder, while basic schematics existed; they were necessary, and to create the physical world, it was at best "stick and cane design." Simply put, it means you know where you have to go, but as you are half-blind, you are going to trip up on every logistical on the way, with the lost time not worth talking about.

"The more paper, the better - a wiring diagram would be a lifesaver."

2 - Wire tracing, while the coloured wire was used it in places, became disjointed, defeating the purpose and in an area like the joystick/junction box created a total black hole for time with red to green, etc. Another area was the interface between the intercom, radio, and mike switches, just too many wire colours on the same circuit, creating a complex matrix even to record on the schematics.

"Keep the colour consistent as possible even if you have to ditch the wire supplied with the switches to colours at your disposal."

3- Labeling, here, the numbering system works well but was not used from the start, and when used, it may have been a little thin. Doing it again, I would be more verbose mainly were a lot of circuits mix. In the case of the stick, an "ELEV UP" at the plugs would have saved a lot of time. This does not replace the id numbers but should be at the start and end of every wire as far as practical.

"Start with a labeler from day one - these can be changed later, but anything that removes the guesswork with saving 10 x the time taken to install it."


The wiring exposed every personal fault I possess, and being raw at this type of work, the builder had no tools to stop time evaporating.

Put simply, I stuffed up and paid in time in hundreds of hours and frustration. The only key is to plan and to steal ideas. This was the one reason the wiring diagrams attached to this site will be updated as soon as practical to "As-built" in the hope that one or two may be of value to at least one person.

Define "as-built": Fewer stuff-ups

Monday, 23 September 2019

Trig 21 Transponder

This blog covers the installation of the Trig Model 21 Mode S transponder

Overview
While not mandatory for this aircraft to be fitted with a mode S transponder one became available from an aircraft upgrading at a good price - sold!

While complete it did not include the installation kit, so a Trig installation kit was purchased and placed in the cupboard until needed. 

At this point, it was noted that the plugs used push in crimp pins and the crimper was to cost $US100 plus delivered to Australia. My local radio guy advised me to just solder them with a very fine iron, not the first choice but my only one if I did not want to spend the money for 20 crimps plus a 2-week wait.

In a previous blog on wiring tools used on the project, the ferrules with crimper are shown but more importantly, it appeared to have the same action. A piece of 22 guage wire was inserted and a crimp applied, after a check, it was re-crimped providing adequate clamping force.





The other issue was all the builder had was a stock of 20 guage wire at this time - a little heavy but there. While as large as the pins allow, it did provide a solid crimp, while leaving some minor marks on the cable insulation.

Time to loom up.

Installation.
Followed the factory wiring diagram and installed the required cables, theses were labelled and the transponder clipped into its cradle located on the top side of the wheel well toward the panel.


The PPS sleeve is creating cool looking looms
The transponder clips into a lockable cradle


Comment
Get out of jail card played

Tuesday, 20 August 2019

Wiring Tools

This blog covers the tools used in the wiring process.

Overview
To wire the aircraft a number of tools are required to achieve a good standard of assembly and regardless of what instruments are selected the problem will be the same with the only scale being a variable.



Support bracket for the panel - replace rivet in the bow with an M4 rivet nut.
Fabricated a bracket as shown that uses the top mounting bolts of the panel.

Tools

This tool crimps ferrules onto bare ends of wires when inserted into screw terminals of electronics. 
The most useful were red/yellow/white/green to be found on the Bay



Crimper for AMP aircraft rings and spades.




This is used to install brass pins onto the ends of the wire. The modified pliers fold the brass
tabs over and the crimper places that nice V you see in all the factory-installed ends.
It is critical for a secure connection and was purchased from Spruce
The pliers were a cheap spring-loaded set just trimmed for the task

A temperature-controlled soldering unit is a must.
Always use a 1.0 mm resin core 60/40 solder where possible



The blue handled tools are strippers, both have their strengths but the
builder favours the pliers. The orange handled tool is a flush shear cutter
not a pair of side cutters. Both these tools are supplied by Xuron and the
flush cutters provide the cleanest of all cuts  




Comment




The wiring goes on and if of any interest, a blow by blow is on my facebook page under Gary Spencer Salt.

Tuesday, 10 October 2017

Master Circuit

This blog cover the master circuit and hardware used.

Overview
To save weight an alternative solenoid was sourced based on a recommendations found on the Matronics site.

Each of the three [3] circuits has a separate bus supplied to a switch/breakers rated to meet the total demand of each circuit they supply.

Installation
To facilitate maintenance and installation it was decided to install a series off AMP plugat the circuit breaker panel and the airframe. The plugs were terminated behind the panel on the starboard side into plugs on a dedicated bracket. 

This allows the manufacture of the circuit breaker/switch panel as one assembly on the workbench and then installed into the air-frame.

Note: AMP plugs feature gold plated pins for increased reliability. The 14 guage were a push and required a little more care to achieve a satisfactory connection.

The input from the manual isolator switch was run in 6 gauge wire to the master relay with the panel 15 amp switch/breaker feed with individual 14 gauge wires and the 10 amp switch/breaker supplied with a 16 gauge feeder. 

Each run was terminated onto their respective breakers using the screw connections supplied.

The main feed to the through the breaker was run in 6 gauge aluminum / copper clad cable for increased margin. The cable ends were fitted with nipples behind the panel to prevent accidental shorts when servicing that area.

Note: Battery fuse is 50 amps / Generator 30 amps


Load check wire selection
Schematic - Master-20 

Batteries
Two [2] LifePo4 each with 20 amp hour [lead equivalent] and 230 CCA were installed into the rear compartment to achieve a 18%MAC - it not moving again that is a guarantee. 

The MAC is at 18.5% empty with the relocated pump. The current battery's combined with relocating the hydraulic pump saved me 4kg [8.8 lbs] compared to the current battery. Since the original selection of batteries, EarthX in the USA have release a superior battery and the existing batteries may be replace by these at some point. 

At the positive terminal a 125 amp lo-Blo® fuse was installed to eliminate nuisance blowing during temporary, short duration overloads. These are commonly used for battery and alternator connections and other heavy gauge cables requiring high current protection in automobiles. 

The connection to the positive stud was made using a rigid bus to save space and weight.

The existing cables were then run to the underside of the folded channel and terminated with the same studs used at the firewall as the  aluminium cable used is light but stiff.

From the studs colour coded battery cables were manufactured from flexible battery cable connecting the battery to the aluminium cable allowing ease off battery removal and preventing any chance confusion at reinstallation.

Circuit Fuses
Two holders that accept automotive maxi fuses were installed on the firewall to protect the supply to the breaker panel and the generator rated at 50 / 20 amps respectively. 

The holders were fitted into a folded 0.030'' aluminium channel as it proved impractical to mount with the single bolt mount provided. Both channels were riveted to the firewall and then the holder bolted with a cap hd screw into a M4 rivet nut.



The lug at the rear was designed to engage into a guide on the
original application requiring a custom bracket mount
However they were light/compact when installed



Isolator
It was originally intended to use a manual switch as a isolator without a master solenoid but this has proved impractical. The manual isolator is now a TRUE isolator in the automotive sence - pull cord - ALL power is removed. 

In any track car the crews must have a means to shut the whole car down and that task is performed by these mechanical isolators.

In my aircraft in a rapid emergency where there is no time to clean up all the separate panels created - Pull the red ring. 

Comment
Worked as planned.  

The isolator will require a mechanical pump to work 100% as planned - watch this space - the motor is going to the shop to be upgraded and the final configuration will be decided once were verify a few items on a test stand.


This blog was not intended to give a running description of the day by day work - refer to Facebook Gary Spencer Salt for more frequent general updates.

Breaker Panel

This blog covers the construction of the switch and breaker panel.

Overview
The panel is located on the starboard side of the pilot's seat screwed to the bulkhead. Its was decided that the panel was to be removable to allow construction and maintenance to be undertaken on a bench.

To achieve this the panel has to be equipped with a number of plugs to allow the connection of the panel into the airframe wiring.

Installation.
The panel was folded from 0.030'' 2024-T3 sheet and fixed to the fuselage former's using M4 rivet nuts three [3] per side and fixed using M4 aluminium screws. The removable panels were manufactured from the same material and fixed using M3 x 10 cap HD S/S screws and rivet nuts.

With the final layout decided for the switches and breakers the removal panels were primed and drilled using a step drill to suit either the switches / breakers as required.

It was decided to connect the panel to the fuselage wiring using AMP plugs as outlined in the blog on the master circuit. The three [3] circuits were connected via switched circuit breakers using 14 and 16 gauge wire terminated onto the master bus behind the firewall. 

Use of the three separate feeds allowed reduced the wire sizes so they could be handled using the AMP pins.


Switch - Breaker Panel


One of the really big problems converting schematics into the physical without drawing the whole exercise requires a lot of imagination to be used, this saves time but leads to more work and things not happening the way you imagined.

The circuit logic was visualized as shown below with switched breakers providing power to a circuit breaker panel and to fuses behind the main panel but during installation a simpler system evolved making the use of the switched breakers of less importance - Streaker's defence is invoked.




Switched breakers will allow grouped shutdown of the selected electrical load in the event of an alternator failure but adds to the overall complexity. 

Klixon 2TC2 breakers were selected for their light weight and small size especially in depth as the panel as constructed is shallow. The breakers are organized into three [3] buses - Essential/Avionics/General paralleled with terminal strips [bus's] located behind the panel.



Breaker panel

The largest single load is the lighting especially the strobes even with all lights beign lightweight / low current LED types followed by the avionics. The other loads are mostly intermittent high current so battery storage is important as the load analysis shows the alternator lacks the reserve's to power theses.
Current Load Analysis

Comment
The question could be posed - Why all this effort? - Well the builder could try and give lots of reasons but in the end its all about the vibe and a good replica creates a vibe - does it not?

This blog was not intended to give a running description of the day by day work - refer to Facebook Gary Spencer Salt for more frequent general updates.

Tuesday, 30 May 2017

Wiring Panel

This blog covers the wiring behind the panel

Overview
The work to convert all the wiring schematics into the physical world has now to be undertaken. Without detailed design work and drawings a lot has to be left to the imagination, while living in the hope of finishing with a product that appears to have a small amount of intelligence applied.

The primary goals set for the installation : -

1 - The panel must be removable by disconnecting plugs. 

2 - Weight to be kept to a minimum.

3 - Wiring to be in a orderly  and logical 

The channel was secured at the firewall and the lower panel using four [4] M3 rivet nuts at both ends. The lower rail that the panel is mounted on had a series of holes drilled to align with the front mounting screws of the channel.

The side Z panels for mounting other hardware were now installed and secured with self tapping screws. These should have been installed much earlier as access for the fixings was a real issue requiring the removal of the mounting angles for the panel cover.


T panel installed - undercarriage terminal strips on left with
first of the AMP plugs installed for the intercom. Additional plugs will be
installed to connect to the breaker / switch panel 

RS 232 connectors mounted in channel for tacho,manifold pressures and AOA [LHS]
Cables for engine instruments shown on RHS connected to power bus

Note: The mounting panels are screwed only to allow removal / replacement in the event of a major change at some future date. The T mounting was necessary to provide adequate mounting points for the electrical hardware



Component assembly center support
Master terminal strip would have been better at six studs
with the shunt relocated

RS232 Connections
While the UMA instruments selected had a RS232 plug, a number of other instruments did not namely the AOA indicator, trim indicators and assorted lights.


Punch openings and RS232 connectors
Note the flattening of the ferals after installation


As supplied - LHS
Center support punched to allow the mounting of the RS232 connector with incorporated terminal strip. Each wire was fitted with a ferrule to protect the wire when clamped into the strips. The hex mounting nuts supplied with the terminals were removed and replaced with longer one to allow fixing onto the center channel.

The LED indicators has a RS232 socket soldered onto the factory wires and supported with a 0.040'' 2024-T3 brackets fixed to the panel using 3M automotive trim tape.


RS232 plugs LED / AOA indicator

These brackets carry the load and provide strain relief for the solder connections with a short cable connecting the instrument to the channel connectors as outline above.

Firewall Penetrations
IP68 Glands
Many of the cables from the engine instruments are required to penetrate the firewall. Though there are many systems around these are large, expensive and not available in Australia. With our main enemy being fumes, brass IP68 glands were sourced from JayCar and then installed with the seals located on the inside face placing the open base at the firewall side. The glands are tightened around the cable with the open face to be sealed with high temperature red silicone. 

Each cable is tagged with its cable ID at the exit. This is to assist troubleshooting and locating to correct cable to hook to the sensors.


Firewall penetrations IP68 glands
All labels printed with the Dymo printer on heat shrink tube

Note: The pitch chosen was a little tight and this builder would recommend spacing to suit your ring spanners. 

Starter Solenoid
The starter solenoid was mounted adjacent to the master positive stud located in the firewall and connected with a brass bus. This will have a insulated coating applied at final installation with a insulated coating applied to the brass bus.


Starter solenoid connected to positive battery stud
connected with 20 x 1.5 mm brass bus

Comment
Kaos appearing to ease as each wire is terminated with the largest issue just converting the schematics into real world wire and seeing how to have them interact with each other.