tillergirl
Well-Known Member
Views on the following would be appreciated please.
I have a couple of cracked frames on either side at the tuck of the stern. They are relatively stable in the sense that some epoxy putty put in the cracks last winter shows no sign of movement and the seams adjacent are tight. However, this year is the time to do something about them. And here is the subject of choice.
I do not really want to take the cockpit apart as that would be major reconstruction so the issue is what can I achieve with the access I've got. That is access through the cockpit floor and through the cockpit lockers, the floors of which are removable. Against this is a very substantial bilge stringer under which the replacement frame would have to be wiggled.
This photo taken 16 years ago on re-engining shows the extent of the curve into the bilge. Obviously there is a reverse curve for the topsides. The stringer is just out of sight. The cracked frames are level with the stuffing box.
Choices seem to be:
1. Steam complete new frames - but the frames will each be nearly 2 metres in length and 25mm x 32mm section. The restricted access and the bilge stringer is going to make it really difficult - if not doubtful - to get the frame in. Best option but also the most difficult?
2. Laminate complete new frames - but with that tuck at the turn of the bilge, steaming is still going to be necessary and then there is the problem of gluing wet timber
3. Steam new frames in two pieces with a long scarf about mid section either above or below the bilge stringer - this would enable each half to be bent in the available space. There might be an issue in keeping the half that does not tuck under the stringer in place during the fitting and the scarf would have to accomodate some of the curve.
4. Cut out the cracked part of the frames (the bottom bits) and steam the replacement and scarf this to the part of the old frame left in situ.
5. Is there another alternative?
Any comments or suggestions. I would really like to do option 1 but I fear there is just not enough access.
I have a couple of cracked frames on either side at the tuck of the stern. They are relatively stable in the sense that some epoxy putty put in the cracks last winter shows no sign of movement and the seams adjacent are tight. However, this year is the time to do something about them. And here is the subject of choice.
I do not really want to take the cockpit apart as that would be major reconstruction so the issue is what can I achieve with the access I've got. That is access through the cockpit floor and through the cockpit lockers, the floors of which are removable. Against this is a very substantial bilge stringer under which the replacement frame would have to be wiggled.
This photo taken 16 years ago on re-engining shows the extent of the curve into the bilge. Obviously there is a reverse curve for the topsides. The stringer is just out of sight. The cracked frames are level with the stuffing box.
Choices seem to be:
1. Steam complete new frames - but the frames will each be nearly 2 metres in length and 25mm x 32mm section. The restricted access and the bilge stringer is going to make it really difficult - if not doubtful - to get the frame in. Best option but also the most difficult?
2. Laminate complete new frames - but with that tuck at the turn of the bilge, steaming is still going to be necessary and then there is the problem of gluing wet timber
3. Steam new frames in two pieces with a long scarf about mid section either above or below the bilge stringer - this would enable each half to be bent in the available space. There might be an issue in keeping the half that does not tuck under the stringer in place during the fitting and the scarf would have to accomodate some of the curve.
4. Cut out the cracked part of the frames (the bottom bits) and steam the replacement and scarf this to the part of the old frame left in situ.
5. Is there another alternative?
Any comments or suggestions. I would really like to do option 1 but I fear there is just not enough access.