![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
|
Thread Tools | Display Modes |
#11
|
|||
|
|||
![]()
Forget PW5's, let's do the aerotow on CG hooks again!
|
#12
|
|||
|
|||
![]()
Brian wrote:
I really can't see any drawback to the make before break switch other than cost and availablity. As long as you have appropiate fuses or circut breakers in the system fire should not be an issue and 99.99% of the time you will only be switching from a low battery to a good battery. and the two batterys are only connected for a few milliseconds which may not be such a bad thing as it will slightly slow the voltage transition to your instruments. Based on my experiments with two 18 amphour batteries, one freshly charged and the other discharged below 10 volts, the "surge" current will be less than 10 amps. For the more typical case (two 7 amphour batteries, one fresh and one discharged to 11 volts or so), the surge current will be only a few amps. This is well within the capacity of switches, wires, and fuses commonly used, especially given the short duration. -- Change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
#13
|
|||
|
|||
![]()
(if the circuit does not show up aligned,
view the message with Courier New Font) I have in my ASW27 three batteries and two solar panels on the fuselage for recharging. Batteries need a certain time to adjust their chemical process for delivering current and for receiving current from the panels. The racers for the solar challenge overcome this problem by using two batteries: One for driving and the second for receiving the energy delivered by the panels or from the motors while braking. Is the second one full the batteries are exchanged in the circuit: the second for driving and the first for recharging. I did the wiring of the rotary main switch the same way for my ASW27 (example for 2 batteries) __________________________________________________ _ BATTERIES 7.2Ah 0 A 0 B ¦ ¦ +-----¦------¦---+--- LOGGERS ¦ ¦ DIODES ¦ ¦ +------¦---+ ¦ ¦ ROTARYSWITCH + +-+ + +-+ ROTARYSWITCH --¦-----¦ 0 A B ROTARYSWITCH + + + + ¦ ¦ ¦ ¦ +-------+------------- AVIONICS ¦ ¦ ¦ SOLAR-CHARGER -------+---+ = 10000uF ¦ GROUND ------------------+------------------- __________________________________________________ __ The Cambridge Logger takes the power from the battery with the highest Voltage. The capacitor bridges switch over time up to 1sec if radio is in receiving mode. I fly with this layout for more than 10 years and never had a problem with instruments, loggers or palms failing. I normally fly a complete week until I recharge the batteries externally. Additionally I have an override switch which connects the Solar panels directly to the Avionics, but I never saw need to use it up to now. Chris CH __________________________________________________ ___ |
#14
|
|||
|
|||
![]()
(if the circuit does not show up aligned,
view the message with Courier New Font) I have in my ASW27 three batteries and two solar panels on the fuselage for recharging. Batteries need a certain time to adjust their chemical process for delivering current and for receiving current from the panels. The racers for the solar challenge overcome this problem by using two batteries: One for driving and the second for receiving the energy delivered by the panels or from the motors while braking. Is the second one full the batteries are exchanged in the circuit: the second for driving and the first for recharging. I did the wiring of the rotary main switch the same way for my ASW27 (example for 2 batteries) __________________________________________________ _ BATTERIES 7.2Ah 0 A 0 B ¦ ¦ +-----¦------¦---+--- LOGGERS ¦ ¦ DIODES ¦ ¦ +------¦---+ ¦ ¦ ROTARYSWITCH + +-+ + +-+ ROTARYSWITCH --¦-----¦ 0 A B ROTARYSWITCH + + + + ¦ ¦ ¦ ¦ +-------+------------- AVIONICS ¦ ¦ ¦ SOLAR-CHARGER -------+---+ = 10000uF ¦ GROUND ------------------+------------------- __________________________________________________ __ The Cambridge Logger takes the power from the battery with the highest Voltage. The capacitor bridges switch over time up to 1sec if radio is in receiving mode. I fly with this layout for more than 10 years and never had a problem with instruments, loggers or palms failing. I normally fly a complete week until I recharge the batteries externally. Additionally I have an override switch which connects the Solar panels directly to the Avionics, but I never saw need to use it up to now. Chris CH __________________________________________________ ___ "ContestID67" wrote in message oups.com... I would like to ask the rec.aviation.soaring community for comments about their experiences switching between batteries while in flight. It seems to be common practice to carry two batteries. There is usually a master switch and then an A/B switch to toggle between the batteries. The issue is what will a momentary interruption in power, when you toggle the A/B switch, do to your flight recorder/computer? Most important is the integrity of your flight log, less importantly is your task and other flight data. PDAs are not suseptible to this issue as they come with their own internal ("backup") battery. Also, let's not discuss "well I have this-and-that device as a backup" (handheld GPS, machanical vario, etc). The issue at hand is competition, record or badge flying and quarantee that all important flight log by maintaining power to your flight recorder. I have not seen a ship yet that had two redundant flight recorders (but I will bet they exist). A simple double throw A/B switch is commonly used. My measurements show that this type of switch is completely open (no power) for 10-15ms but this depends greatly on the quality of the switch. There are make-before-break switches in which for a brief period of time both batteries are connected to each other and there is no loss of power. However even briefly connecting two heafty batteries together, with one possibly completely failed, has its own drawbacks (like an onboard fire). This of course all depends on the pilot knowing when to switch. If (s)he first waits until a failure is noticed, then all may be lost. Another approach is having two ship's batteries connected to one another via a "device" which allows each to (safely) supply current and to automatically switch between the two if one fails. A pair of heafty diodes is an obvious and simple choice as one battery cannot "charge" the other but both can supply power. However, you will typically loose 0.6v-0.8v across a silicon power diode. Ultimately it seems to depend on the manufacturer of the recorder and how their electronics handle a temporary loss of power. Some manufacturers support permanent backup batteries which charge from the ship's main battery. This may be the best overall solution. Any of your ideas and solutions are very welcome. Thanks, John |
#15
|
|||
|
|||
![]()
(if the circuit does not show up aligned,
view the message with Courier New Font) I have in my ASW27 three batteries and two solar panels on the fuselage for recharging. Batteries need a certain time to adjust their chemical process for delivering current and for receiving current from the panels. The racers for the solar challenge overcome this problem by using two batteries: One for driving and the second for receiving the energy delivered by the panels or from the motors while braking. Is the second one full the batteries are exchanged in the circuit: the second for driving and the first for recharging. I did the wiring of the rotary main switch the same way for my ASW27 (example for 2 batteries) __________________________________________________ _ BATTERIES 7.2Ah 0 A 0 B ¦ ¦ +-----¦------¦---+--- LOGGERS ¦ ¦ DIODES ¦ ¦ +------¦---+ ¦ ¦ ROTARYSWITCH + +-+ + +-+ ROTARYSWITCH --¦-----¦ 0 A B ROTARYSWITCH + + + + ¦ ¦ ¦ ¦ +-------+------------- AVIONICS ¦ ¦ ¦ SOLAR-CHARGER -------+---+ = 10000uF ¦ GROUND ------------------+------------------- __________________________________________________ __ The Cambridge Logger takes the power from the battery with the highest Voltage. The capacitor bridges switch over time up to 1sec if radio is in receiving mode. I fly with this layout for more than 10 years and never had a problem with instruments, loggers or palms failing. I normally fly a complete week until I recharge the batteries externally. Additionally I have an override switch which connects the Solar panels directly to the Avionics, but I never saw need to use it up to now. Chris CH __________________________________________________ ___ |
#16
|
|||
|
|||
![]()
(if the circuit does not show up aligned,
view the message with Courier New Font) I have in my ASW27 three batteries and two solar panels on the fuselage for recharging. Batteries need a certain time to adjust their chemical process for delivering current and for receiving current from the panels. The racers for the solar challenge overcome this problem by using two batteries: One for driving and the second for receiving the energy delivered by the panels or from the motors while braking. Is the second one full the batteries are exchanged in the circuit: the second for driving and the first for recharging. I did the wiring of the rotary main switch the same way for my ASW27 (example for 2 batteries) __________________________________________________ _ BATTERIES 7.2Ah 0 A 0 B ¦ ¦ +-----¦------¦---+--- LOGGERS ¦ ¦ DIODES ¦ ¦ +------¦---+ ¦ ¦ ROTARYSWITCH + +-+ + +-+ ROTARYSWITCH --¦-----¦ 0 A B ROTARYSWITCH + + + + ¦ ¦ ¦ ¦ +-------+------------- AVIONICS ¦ ¦ ¦ SOLAR-CHARGER -------+---+ = 10000uF ¦ GROUND ------------------+------------------- __________________________________________________ __ The Cambridge Logger takes the power from the battery with the highest Voltage. The capacitor bridges switch over time up to 1sec if radio is in receiving mode. I fly with this layout for more than 10 years and never had a problem with instruments, loggers or palms failing. I normally fly a complete week until I recharge the batteries externally. Additionally I have an override switch which connects the Solar panels directly to the Avionics, but I never saw need to use it up to now. Chris CH __________________________________________________ ___ |
#17
|
|||
|
|||
![]()
CHo wrote:
(if the circuit does not show up aligned, view the message with Courier New Font) I have in my ASW27 three batteries and two solar panels on the fuselage for recharging. Batteries need a certain time to adjust their chemical process for delivering current and for receiving current from the panels. How much time are you talking about for glider batteries? I've not seen any mention of this in the data sheets for our batteries. -- Change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
#18
|
|||
|
|||
![]()
I have received communications from several manufacturers about this
issue and am awaiting information from others. I plan on presenting this during my speech at the 2006 SSA convention. Interestingly, I picked up the following from the Volkslogger manual.... ================= "The VOLKSLOGGER has no internal buffer against momentary power interruptions. This has the advantage that there is no part, which deteriorates and would have to be replaced every 2-3 years by the manufacturer. Therefore, the power supply of the instrument has to be protected against momentary drops below the minimum voltage. In particular during switching of batteries such voltage drops can take place, which will lead to a separated flight record during readout. This means that the recording of the flight consists of several files, which is accepted reluctantly or not at all by the evaluator. The circuit shown is meant as an example for a buffered and fused installation. Alternately it is recommended to use a separate logger battery (Gel-Cell, 12V, 1.8 Ah), to which no other power consuming devices are connected." ======================= Basically the diagram shows the battery connected to the Volkslogger via a series 0.5A fuse, a series Shottky diode 1N5817 and a parallel 22,000uF capacitor. You can see the diagram in the manaul available at the web site http://www.volkslogger.de/en/html/volkslogger.html. The manual states that the logger can be run as low as 9.5vdc (up to 24vdc). However, Mr Johannes Garrecht (designer) stated in his letter to me that the Volkslogger will run at 7vdc. Impressive. After I compile all the information and present it at the convention I will make it available here. Stay tuned. |
|
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Battery Source | Mike the Strike | Soaring | 81 | October 28th 05 12:46 AM |
Advice and experts with 400 series Cessnas (414 and 421), purchase and training | [email protected] | Owning | 36 | January 9th 05 02:32 AM |
Batteries, charger for Yaesu handheld - NiCad or NiMH? | David Herman | Owning | 10 | November 7th 04 04:30 PM |
boot camp advice | jameson | Military Aviation | 17 | July 22nd 04 05:12 AM |
Rechargable AA batteries and chargers | TripFarmer | General Aviation | 2 | October 17th 03 06:34 PM |