Method of installing a structural blind fastener

1. A method of installing a two-piece, one-sided-installation fastener system, comprising:

inserting a core bolt and a sleeve into a hole of a structure having a front side and a back side, the core bolt having a frangible driving provision coupled to a core bolt head;

translating the core bolt backward away from the front side of the hole without rotating the core bolt relative to the sleeve;

buckling a softened portion of the sleeve to form a single buckled sleeve portion;

flattening the buckled sleeve portion against the back side of the hole; and

rotating the core bolt relative to the sleeve to apply tension in the fastener system independent of translating the core bolt backward away from the front side of the hole.

2. The method of claim 1 , further comprising the step of:

separating the frangible driving provision from the core bolt head at a pre-defined fastener preload.

3. The method of claim 2 , wherein the step of separating the frangible driving provision from the core bolt head includes at least one of:

exceeding a torsional capability of an interface between the frangible driving provision and the core bolt head;

axially pulling on the frangible driving provision until exceeding a tension capability at the interface; and

bending the frangible driving provision until exceeding a bending capability of the interface.

4. The method of claim 3 , wherein the step of separating the frangible driving provision from the core bolt head comprises:

separating the frangible driving provision from the core bolt head at a break groove formed at the interface.

5. The method of claim 1 , wherein:

the softened portion comprises a localized annealed portion extending along a portion of a sleeve length.

6. The method of claim 1 , wherein the step of buckling the softened portion of the sleeve includes:

buckling the softened portion of the sleeve radially outwardly into an annular sleeve bulb.

7. The method of claim 6 , wherein the step of buckling the softened portion of the sleeve includes:

buckling the softened portion until the buckled sleeve portion has a minimum diameter of approximately 1.2 times a sleeve outside diameter when the buckled sleeve portion is buckled against the structure.

8. The method of claim 1 , wherein the step of translating the core bolt further comprises:

engaging an axial translation feature formed on the frangible driving provision.

9. The method of claim 1 , wherein the step of translating the core bolt further comprises:

maintaining a sleeve head against the structure in a manner preventing axial translation of the sleeve relative to the hole.

10. The method of claim 1 , wherein the step of translating the core bolt further includes:

translating the core bolt without translating or rotating the sleeve relative to the hole.

11. The method of claim 1 , wherein the step of rotating the core bolt comprises:

engaging a rotation feature formed on the frangible driving provision.

12. The method of claim 1 , wherein the step of rotating the core bolt includes:

engaging core bolt threads with a locking feature formed in the sleeve; and

restricting rotation of the core bolt relative to the sleeve in response to engaging the locking feature.

13. The method of claim 1 , wherein the step of rotating the core bolt relative to the sleeve includes:

preventing rotation of the sleeve relative to the hole.

14. The method of claim 13 , wherein the step of preventing rotation of the sleeve relative to the hole includes:

engaging an anti-rotation feature on a sleeve head of the sleeve.

15. The method of claim 14 , wherein the step of engaging the anti-rotation feature on the sleeve head includes:

engaging at least one of indentations and protrusions on the sleeve head.

16. The method of claim 1 , wherein the step of rotating the core bolt relative to the sleeve includes:

nesting the core bolt head in a core bolt pocket in a sleeve head of the sleeve.

17. The method of claim 1 , wherein the step of inserting a core bolt and a sleeve into a hole of a structure comprises:

inserting the core bolt and the sleeve into a hole of an aircraft structure.

18. A method of installing a two-piece, one-sided-installation fastener system, comprising:

inserting a core bolt and a sleeve into a hole of a structure having a front side and a back side, the core bolt having a frangible driving provision coupled to a core bolt head, the sleeve having a sleeve head;

axially pulling on the frangible driving provision;

translating the core bolt backward away from the front side of the hole without rotating the core bolt relative to the sleeve and while maintaining the sleeve head against the structure;

buckling a softened portion of the sleeve against the back side of the structure to form a single buckled sleeve portion;

flattening the single buckled sleeve portion against the back side of the hole; and

rotating the core bolt relative to the sleeve to apply tension to the fastener system without axially translating the core bolt relative to the sleeve.