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Re: [ULF-1] Ulf-1 Digest, Vol 69, Issue 1
- From
- Member 111
- Date
- 2018-05-02 19:54 UTC-06:00
- Message
- #0574
Member 67,
Thank you for giving us some insight into your very interesting build. I watched your Destructive Test on YouTube several times.
Did you deviate from the drawings with respect to the spar cap dimensions as well or just in the attachment fittings as described?
I was wondering if the added the weight of the power system and motor pylons needed some beefing.
Thanks again for pioneering,
Austin in UT
> On May 2, 2018, at 3:03 PM, [email] wrote:
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> 1. ULF-1 spar destructive test (Member 117)
> 2. Re: ULF-1 spar destructive test (Member 72)
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> ----------------------------------------------------------------------
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> Message: 1
> Date: Wed, 2 May 2018 14:54:25 +0100
> From: Member 117 <[email]>
> To: [email]
> Subject: [ULF-1] ULF-1 spar destructive test
> Message-ID: <[email]>
> Content-Type: text/plain; charset="us-ascii"
>
> Good afternoon
>
> I am preparing all the materials to begin the construction of a ULF-1 in Portugal, and I saw on the web, that the EAA Chapter 309 in North Carolina performed a ULF-1 Spar destructive test, it is possible to have access to these data? and if the construction of the spar was carried out according to the instructions in the manual ?
>
> thank you
>
> Best regards,
>
> Member 117
>
>
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> Message: 2
> Date: Wed, 2 May 2018 17:00:29 -0400
> From: Member 72 <[email]>
> To: [email]
> Subject: Re: [ULF-1] ULF-1 spar destructive test
> Message-ID: <[email]>
> Content-Type: text/plain; charset="utf-8"
>
> Hi Nuno,
>
> Good luck with your
> Build! We deviated from the plans with the attachment fittings at the wing roots. The plans call for tubular rivets to be used to attach the steel fittings to the spar caps. We did not have the tooling to fabricate these large rivets. So, at each station that required a rivet, we drilled a 1/2? hole and epoxied a nylon lug or bushing into the hole. The nylon lugs have a 1/4? hole drilled down the center to accept an AN-4 aviation bolt. We epoxied the steel spar fittings on, with their 1/4? holes pre-drilled to match the holes on the nylon lugs. Then, we added the bolts, washers and nuts. We were in contact with Member 9, the designer, at Aero in Germany. Because of our deviation to his plans on the most heavily loaded part of the airframe, he asked us to perform a destruction test and gave us a minimum breaking strength. Fortunately we were well over his minimum figure, and he blessed our design deviation! If we were to do it again, we would consider using 1/2? phenoli
> c rod rather than the nylon. But, the nylon lug material worked OK.
>
> Best regards,
> Member 72
>
>
>
> Sent from my iPhone
>
>> On May 2, 2018, at 9:54 AM, Member 117 <[email]> wrote:
>>
>> Good afternoon
>>
>> I am preparing all the materials to begin the construction of a ULF-1 in Portugal, and I saw on the web, that the EAA Chapter 309 in North Carolina performed a ULF-1 Spar destructive test, it is possible to have access to these data? and if the construction of the spar was carried out according to the instructions in the manual ?
>>
>> thank you
>>
>> Best regards,
>>
>> Member 117
>>
>>
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> End of Ulf-1 Digest, Vol 69, Issue 1
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