X-Junk-Score: 0 [] X-KAS-Score: 0 [] From: "Stephen Izett stephen.izett@gmail.com" Received: from pmg.Logan.com ([207.170.160.161] verified) by logan.com (CommuniGate Pro SMTP 6.4.0) with ESMTPS id 3774803 for flyrotary@lancaironline.net; Fri, 03 Jan 2025 18:49:29 -0500 Received: from pmg.Logan.com (localhost [127.0.0.1]) by pmg.Logan.com (Proxmox) with ESMTP id BFA1112477 for ; Fri, 3 Jan 2025 18:49:29 -0500 (EST) Received-SPF: pass (gmail.com ... _spf.google.com: Sender is authorized to use 'stephen.izett@gmail.com' in 'mfrom' identity (mechanism 'include:_netblocks.google.com' matched)) receiver=pmg.Logan.com; identity=mailfrom; envelope-from="stephen.izett@gmail.com"; helo=mail-pj1-f51.google.com; client-ip=209.85.216.51 Received: from mail-pj1-f51.google.com (mail-pj1-f51.google.com [209.85.216.51]) by pmg.Logan.com (Proxmox) with ESMTPS for ; Fri, 3 Jan 2025 18:49:29 -0500 (EST) Received: by mail-pj1-f51.google.com with SMTP id 98e67ed59e1d1-2ef28f07dbaso14129808a91.2 for ; Fri, 03 Jan 2025 15:49:29 -0800 (PST) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20230601; t=1735948162; x=1736552962; darn=lancaironline.net; h=message-id:in-reply-to:to:references:date:subject:mime-version:from :from:to:cc:subject:date:message-id:reply-to; bh=hwnK2MoMqwEuj6AMEgl0viJYKZ2s3ptgx6Ah79HNe9M=; b=DO1MKFhfv+uBu+tdrxsf4uQLOjpR+NhR4t3xNriXhcTs/ZXuiKfoII+2rR3Z5Y5r+C NzdesVOBiCfAYOUJi44P9LDQClNZby2F12ebfvPXqRAR3tMZqTmBBzH+csODJMHIbsIe G1t38rCvQRTRfXBZWcbvFqneVLmKp9X/pCVinCQJ3cxstSvDKDHuv2kC0TE2dpsmfs1P bHQ5iSSis9yvUlNA1dJ+jtl2bTLtWDjJDVZ0lq+PlCbRjx4myTAFC5h9tF+yh4HMzkMO NeG//CzYpxom3/n9lTgJAwP/2udfPD4PvO8fLL0tCDXaa2avy4vUOdHXEm9bh65QJvdp 0fNw== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20230601; t=1735948162; x=1736552962; h=message-id:in-reply-to:to:references:date:subject:mime-version:from :x-gm-message-state:from:to:cc:subject:date:message-id:reply-to; bh=hwnK2MoMqwEuj6AMEgl0viJYKZ2s3ptgx6Ah79HNe9M=; b=SPRkxQJj2As1lWgnuNJLg/D3XKAfVjGjLvA5Hz0oJiisdsEkqS3CnOu3M2BiHCqhAl cozbUsPVnuJ9omlmJLs3cqOAinHdVZtzCGauJdsSb/PjP+hoJR/SvW3V4YGxG2abrT5A dbkLgx58MYqH82y44D4WOTV/t+EY5Q+UgptbikEF74iupuRCHdfWkWBSG4D+CKzVu2Vl FSUnJtsYwW7HqCdSQEguqTt1tiZHnZatjzvVxPDxHuE/zZWf/kpMQEtMrHX/L94uLMZ8 XQstE4jCPur/QyP9xyG7hmzGOf3XcJX0yNNaBHMBF0oNKWzHbfsuNepCO0HlSR54/vvf yZBg== X-Gm-Message-State: AOJu0YwOzinvjTHs+zurSOv9+I86FpO9wohw10K+jRMbjBH9zibOuWo4 eXag4LqAUPhc25C6stWOx0Yqg8YZ++WMedK2TlIReuZ0VtsQPxoqT40g4w== X-Gm-Gg: ASbGncugSKyR5diRQG+Le+nDx7N3qWqGBTCyYh3F+eRnk2zQ/tAZR47oZb07VKs9wbO w3zawLcjKC+BaVovV27Zh7b2WX3cEgnkBrjI9ZwUrW22MG/HV1lUJgBlN5TCBINjr5krhd29E7j GdIxQp/6Dwhg8+/PGGU6rgpYk+UBcvpspfeR6e7i9wYmdjUktArew8fUrHdWmBqRHsmFpKTDrCB IiBKpe/7cn00/00Q3E0/LcjP4cvwBX9EDB1ofHaldIrYKzmaqRgO1lca+fFae/1pRBOT416QqL3 X-Google-Smtp-Source: AGHT+IF45QJl3smYHEpmoHXniNn3r/gmD6BUG5MfyOwS9AC3p+E6yYlkH9awmJ5Rn4r9hOd+VpljRw== X-Received: by 2002:a05:6a00:8f07:b0:725:b201:2362 with SMTP id d2e1a72fcca58-72abddb0bd4mr60410562b3a.11.1735948161802; Fri, 03 Jan 2025 15:49:21 -0800 (PST) Received: from smtpclient.apple ([1.127.110.94]) by smtp.gmail.com with ESMTPSA id 41be03b00d2f7-882ec09606csm20175192a12.14.2025.01.03.15.49.20 for (version=TLS1_2 cipher=ECDHE-ECDSA-AES128-GCM-SHA256 bits=128/128); Fri, 03 Jan 2025 15:49:21 -0800 (PST) Content-Type: multipart/alternative; boundary="Apple-Mail=_FF858A12-4408-4155-BADF-F6959B800C30" Mime-Version: 1.0 (Mac OS X Mail 16.0 \(3826.200.121\)) Subject: Re: [FlyRotary] Over-voltage protection/alternator failure Date: Sat, 4 Jan 2025 07:49:07 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <2CF56A1F-C75D-4CEE-B637-3D2C2018638E@gmail.com> X-Mailer: Apple Mail (2.3826.200.121) X-SPAM-LEVEL: Spam detection results: 0 BAYES_00 -1.9 Bayes spam probability is 0 to 1% DKIM_SIGNED 0.1 Message has a DKIM or DK signature, not necessarily valid DKIM_VALID -0.1 Message has at least one valid DKIM or DK signature DKIM_VALID_AU -0.1 Message has a valid DKIM or DK signature from author's domain DKIM_VALID_EF -0.1 Message has a valid DKIM or DK signature from envelope-from domain DMARC_PASS -0.1 DMARC pass policy FREEMAIL_FROM 0.001 Sender email is commonly abused enduser mail provider HTML_MESSAGE 0.001 HTML included in message KAM_MXURI 1.5 URI begins with a mail exchange prefix, i.e. mx.[...] RCVD_IN_MSPIKE_H3 0.001 Good reputation (+3) RCVD_IN_MSPIKE_WL 0.001 Mailspike good senders SPF_HELO_NONE 0.001 SPF: HELO does not publish an SPF Record SPF_PASS -0.001 SPF: sender matches SPF record WEIRD_PORT 0.001 Uses non-standard port number for HTTP --Apple-Mail=_FF858A12-4408-4155-BADF-F6959B800C30 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=utf-8 Hi Finn Really appreciate your reflections and design ideas. I had graded the risk of my smallish ~45amp alternator going HV as low, = and had =E2=80=98assumed' that in such an event the 40Ah battery bank = and ~20amp system load would ballast the system voltage for some time = (minutes) before a critical engine failure was imminent. My engine monitor will let me know =E2=80=98audibly=E2=80=99 as soon as = the system voltage exceeds 15 volts. =E2=80=98Assumptions=E2=80=99 right! I hadn=E2=80=99t got real = confirmation of the real voltage/current over time in such an event. The truth is I have always struggled to get a handle on how a three wire = automotive alternator works electrically. The 'Sense', I thought was simply the feedback for the regulator which I = have from memory via a 5 amp fuse to the engine buss.=20 But what is this =E2=80=98lamp/field=E2=80=99 wire??=20 In mine it=E2=80=99s not connected, and again I =E2=80=98assumed=E2=80=99 = that as my idle is ~1900 rpm this was spinning enough to excite the = system and self sustain the magnetic field at that point. Perhaps I ought diode feed this from the Engine Buss? I understood that because of the above characteristic once these = alternators were generating power you couldn=E2=80=99t turn them off by = de energising a =E2=80=98field=E2=80=99 etc. wire and therefore your = plan to disconnect its output/ B terminal is required. I=E2=80=99m thinking that in your circuit, when your Over Voltage relay = is de-energised by the OVP popping the CB, like disconnecting an = alternator from its battery, (at high RPM, not simply idle) might damage = the alternator diodes/regulator though this is an acceptable outcome if = it keeps the engine running in a critical situation. What I would like to know in order to make an realistic risk assessment = is: 1. How these alternators actually work electrically=20 2. What a High Voltage on the B lead will do over time. A. In the immediate mSec of an event and B Over the next 5 minutes How is your RV4? I hope you can get back in the air soon. Thanks again for the reflections. Steve Izett > On 3 Jan 2025, at 11:35=E2=80=AFam, Finn Lassen = finn.lassen@verizon.net wrote: >=20 > And this is the way I should have done it! >=20 > The error I made (powering the overvoltage relay and alternator field = via the 5A breaker that is pulled to ground when OVP unit triggers) is = what caused total power loss when battery failed open. >=20 > With an internally regulated alternator it needs to power itself after = startup even when disconnected from battery. Because in case of a OVP = nuisance trip, the alternator will continue producing power. The = 33,000uF (or bigger) cap on the B+ terminal should ensure sufficiently = clean (low ripple and noise) to power itself and the engine electronics = is case of no battery (disconnected or failed open). (Size it for your = engine bus current draw, desired alternator RPM range and maximum ripple = you can tolerate. C =3D I / (RPM/60*3*2*Vpp) --- three-phase = bridge-rectified alternator. I my case 10 amps, 3,000 RPM and 1V = peak-peak ripple ~ 0.033 or 33,000uF. >=20 > You should probably have a way to monitor the voltage on the B+ = terminal to ensure the OVP didn't trip on a real alternator runaway, = before trying to reset the 5A breaker. (BTW, a 1A breaker should suffice = -- it's only powering the overvoltage relay). >=20 > Now I'm undecided whether to add a backup battery or not. >=20 > Finn >=20 > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html --Apple-Mail=_FF858A12-4408-4155-BADF-F6959B800C30 Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset=utf-8 Hi = Finn

Really appreciate your reflections and design = ideas.
I had graded the risk of my smallish ~45amp alternator = going HV as low, and had =E2=80=98assumed' that in such an event the = 40Ah battery bank and ~20amp system load would ballast the system = voltage for some time (minutes) before a critical engine failure was = imminent.
My engine monitor will let me know =E2=80=98audibly=E2= =80=99  as soon as the system voltage exceeds 15 = volts.

=E2=80=98Assumptions=E2=80=99 right! I = hadn=E2=80=99t got real confirmation of the real voltage/current over = time in such an event.

The truth is I have = always struggled to get a handle on how a three wire automotive = alternator works electrically.
The 'Sense', I thought was = simply the feedback for the regulator which I have from memory via a 5 = amp fuse to the engine buss. 
But what is this = =E2=80=98lamp/field=E2=80=99 wire?? 
In mine it=E2=80=99s = not connected, and again I =E2=80=98assumed=E2=80=99 that as my idle is = ~1900 rpm this was spinning enough to excite the system and self sustain = the magnetic field at that point.
Perhaps I ought diode feed = this from the Engine Buss?

I understood that = because of the above characteristic once these alternators were = generating power you couldn=E2=80=99t turn them off by de energising a = =E2=80=98field=E2=80=99 etc. wire and therefore your plan to disconnect = its output/ B terminal is required.

I=E2=80=99m = thinking that in your circuit, when your Over Voltage relay is = de-energised by the OVP popping the CB, like disconnecting an alternator = from its battery, (at high RPM, not simply idle) might damage the = alternator diodes/regulator though this is an acceptable outcome if it = keeps the engine running in a critical = situation.

What I would like to know in order = to make an realistic risk assessment is:
1. How these = alternators actually work electrically 
2. What a High = Voltage on the B lead will do over time.
A. In the = immediate mSec of an event and
B Over the next 5 = minutes

How is your RV4?
I hope you = can get back in the air soon.

Thanks again for = the reflections.

Steve = Izett













On 3 Jan 2025, at 11:35=E2=80=AFam, Finn Lassen = finn.lassen@verizon.net <flyrotary@lancaironline.net> = wrote:

=20 =20

And this is the way I should have done it!

The error I = made (powering the overvoltage relay and alternator field via the 5A breaker that is pulled to  ground = when OVP unit triggers) is what caused total power loss when battery failed  open.

With an internally regulated alternator = it needs to power itself after startup even when disconnected from battery. Because in case  of a OVP nuisance trip, the alternator will continue producing power. The 33,000uF (or bigger) cap on the B+ terminal should ensure sufficiently clean (low ripple and noise) to power itself and the engine electronics is case of no battery (disconnected or failed open).  (Size it for your engine bus current draw, desired alternator RPM range and maximum ripple you can tolerate. C =3D I / (RPM/60*3*2*Vpp) --- three-phase bridge-rectified alternator. I my case 10 amps, 3,000 RPM and 1V peak-peak ripple ~ 0.033 or 33,000uF.

You should probably have a way to monitor the voltage on the = B+ terminal to ensure the OVP didn't trip on a real alternator runaway, before trying to reset the 5A breaker. (BTW, a 1A breaker should suffice -- it's only powering the overvoltage = relay).

Now I'm undecided whether to add a backup battery or = not.

Finn

<Battery-AlternatorMin.= png>--
Homepage:  http://www.flyrotary.com/
Archive = and UnSub: =   http://mail.lancaironline.net:81/lists/flyrotary/List.html
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