Desert Aircraft DA35 Скачать руководство пользователя страница 4

Ignition System 

 

Introduction 

The 

V2 Desert Aircraft Ignition

 module is a microprocessor controlled auto advance/retard system.  

The unique timing curve has been developed by Desert Aircraft to provide optimum performance and reliability for your 
DA35. This unique curve will provide easy starting, smooth running throughout the rev range and rapid response to 
acceleration and deceleration.   
With the combination of multiple magnets on the engine hub and a bipolar hall sensor, the microprocessor can measure 
the shaft speed and position accurately. The V2 ignition provides consistent safe starting because the module won’t spark 
unless the propeller is deliberately “flipped” at starting speed. The module will also not allow the engine to start or run 
backwards.  
 
Warning! This programmed ignition system may not be compatible with other Desert Aircraft engines. 
 

Mounting  

The module is supplied with mounting grommets and eyelets to be used in a similar way they are used to mount servos. 
Alternatively the module can be mounted with Velcro straps on a foam/rubber bed. Cable ties (Zip ties) should be avoided 
as the hard plastic can damage the ignition module case over time. 
Choose a location where the module can sit flat away from heat sources and well away from any receivers or connected 
servos. The module will produce a small amount of heat so do not completely enclose it in foam. (The top surface with the 
embossed logo is where most of the heat will be radiated from.) 
Choose a location that will allow you to route the cables in such a way they will not be damaged.  
The sensor cable is provided in a rubber braided sleeve that is resistant to high temperatures and abrasion. There is no 
need to provide any additional protection (e.g. spiral wrap) as that will just add mass to the sensor lead putting more strain 
on the connections. 
The HT cable has an outer silicon jacket to give protection from both high temperatures and mechanical abrasion. Please 
take care that the cable is protected from sharp edges (e.g. fiberglass cowl edges) as this will cut through the protective 
sleeve and can result in unreliable engine performance. Route and support the cable so that it minimizes the amount of 
movement of the cable. 
 

Connection 

Three simple connections are all that is required.  

1.  Push the spark plug cap onto the CM6 spark plug until the hex of the spark plug is covered by the cap outer shell. 

The cap is secured by both the outer housing around the plug hex as well as the internal silicon moulding fitting 
over the plug top. 

2.  Plug the sensor lead into the module in the slot marked “SENSOR.” A Futaba style lead is used so that it will only 

plug in one way. YOU MUST USE A DA TYPE HALL SENSOR FOR CORRECT OPERATION. 

3. 

Connect the battery via your preferred switch (either mechanical or Tx controlled kill switch) to the slot marked 
“POWER.” Check the alignment so that the polarity is correct.  

IT IS IMPORTANT NOT TO CONNECT POWER 

TO A MODULE WITHOUT A SPARK PLUG FITTED TO THE CAP. 

Note about mechanical switches.

 We have found that toggle switches are un-reliable when subjected to the vibration 

typical of a model aircraft. Heavy duty slide style switches typically supplied by the radio manufacturers are better suited.  
 

Battery Considerations 

The V2 ignition module is nominally rated for 4.8 to 8.4V dc supply. This means you can use either a 4 or 5 cell nickel 
cadmium (NiCad), nickel metal hydride (NiMH) battery, or a 2 cell lithium ion (Li-ion), Lithium polymer (LiPo) or Lithium ion 
phosphate (LiFePO4) battery. The module features a constant power convertor to charge the high voltage capacitor. This 
will mean the higher the supply voltage used, the lower the current draw from the battery. On the V2 single ignition 
module, a 4cell NiCad 1100mAHr battery will give a couple of hours of typical flying with plenty of reserve.  A 2 cell Lion 
600mAHr will give approx the same running time.  
Soft pack LiPo batteries while electrically compatible are not ideal for use in gas aircraft because of their mechanical 
construction. Over a period of time, the tab connection to the LiPo cells will not tolerate the vibration experienced by a 
typical gas aircraft. We have seen these connections become intermittent resulting in unreliable engine performance. 
 
A reverse connected battery will not damage the module but it won’t run and the LED will not turn on. On the other hand if 
you allow the battery positive (or an internal cell connection) to come into contact with the engine or the ignition module 
enclosure, 

it will damage the module

. We have seen this happen with poor mounting of the battery pack which has worn 

through the insulation of the cell letting it touch the engine or module case. 
                          

                                                                                3                                                                   (Continued) 

 

Modellmarkt24.ch

Содержание DA35

Страница 1: ...TM DA35 Owner s Manual 4 14 Modellmarkt24 ch ...

Страница 2: ... damage Always operate the motor in an open area Do not operate indoors This motor can develop tremendous thrust Make sure the aircraft is properly secured when starting or operating the motor Inspect motor mount bolts and firewall integrity before operating the motor Anyone in the immediate area of the motor should use eye protection during operation of the motor Keep spectators at least 30 feet ...

Страница 3: ...ar the inlet to allow an unobstructed airflow into the carburetor If the carburetor is located in front of the firewall be sure there is at least 3 8 10mm of clearance from the carburetor inlet If there is less than this make a hole larger than the carburetor inlet diameter in the firewall to insure the carburetor s intake is un restricted The throttle arm is tapped for a 4 40 SAE ball link The re...

Страница 4: ...are all that is required 1 Push the spark plug cap onto the CM6 spark plug until the hex of the spark plug is covered by the cap outer shell The cap is secured by both the outer housing around the plug hex as well as the internal silicon moulding fitting over the plug top 2 Plug the sensor lead into the module in the slot marked SENSOR A Futaba style lead is used so that it will only plug in one w...

Страница 5: ...sert Aircraft if you have any questions regarding timing Only use NGK CM 6 spark plugs Other plugs may not fit the plug caps firmly Plug gap is 018 to 020 38 to 50 mm Never operate the ignition without a spark plug in the plug caps This can permanently damage the ignition coil Desert Aircraft V2 Ignition Specifications Note Specifications subject to change Parameter Minimum Typical Maximum Operati...

Страница 6: ...5 Modellmarkt24 ch ...

Страница 7: ...ays check and tighten prop bolts before each flight Loose prop bolts allow prop movement which will shear the bolts Always use the correct length prop bolts If a spinner back plate is not used the prop bolts may be too long and can bottom out in the hub before they fully tighten against the prop washer The exhaust system weight of the airplane field elevation etc will have an effect on what prop l...

Страница 8: ...ndard and optical Wires can break from vibration near connectors Check and or swap out regulators isolators or optical switches if using one Check tank venting clunk position and fuel flow Fuel doesn t move in the line when the prop is flipped or carb doesn t prime Is the choke plate closed completely Make sure tank is vented Make sure there are no air fuel links on the engine case or carb mount a...

Страница 9: ...bon deposits to avoid damaging the parts Once an attempt to remove carbon has been made the task must be completed as any remaining carbon may be loosened and can dislodge while the engine is running This can damage the engine and or bridge the spark plug Manuals may be updated with additional tips and trouble shooting info from time to time Please check our web site www desertaircraft com or cont...

Страница 10: ...___ Other Items __________ REASON FOR ENGINE AND OR IGNITION RETURN Crash Yes____ No____ Other_________________________________________ ________________________________________________________________________________ ________ ________________________________________________________________________________ ________________________________________________________________________________ ____________...

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