Fastener for connecting components including a shank having a threaded portion and elongated portion and a fitting portion

• US 6,264,414 B1
• Filed: 01/07/2000
• Issued: 07/24/2001
• Est. Priority Date: 01/12/1999
• Status: Expired due to Fees

• Current Assignee: KAMAX-Werke Rudolf Kellermann GmbH & Co. KG
• Original Assignee: KAMAX-Werke Rudolf Kellermann GmbH & Co. KG
• Inventors: Hartmann, Gunther, Sommer, Wolfgang
• Primary Examiner(s): Saether, Flemming
• Application Number:
  US09/479,540
• Time in Patent Office: 564 Days
• Field of Search: 411/411, 411/412, 411/424, 411/915, 411/916
• US Class Current: 411/411
• CPC Class Codes: F16B 31/00 Screwed connections specially modified in view of tensile load; Break-bolts shape of thread F16B33/02; in couplings F16D9/00
• CPC Class Codes: F16B 35/041 Specially-shaped shafts shape of thread F16B33/02
• CPC Class Codes: Y10S 411/916 Bolt having tension feature

Abstract

A fastener (1) for connecting at least two components includes a shank (4) having an axis. At least one threaded portion (7) is arranged at the shank (4), and it has a stressed cross section. At least one elongation portion (5) is arranged at the shank (4), and it has a stressed cross section. The stressed cross section of the at least one elongation portion (5) is less than the stressed cross section of the at least one threaded portion (7). At least one fitting portion (6) is arranged at the shank (4). It has a stressed cross section, and it includes a plurality of protrusions (9) and channels (10). The at least one elongation portion (5) and the at least one fitting portion (6) are spaced apart along the axis of the shank (4). The channels (10) have a root diameter determining the stressed cross section of the at least one fitting portion (6). The stressed cross section of the at least one fitting portion (6) is at least 20 percent more than the stressed cross section of the at least one elongation portion (5).

Claims

1. A fastener for connecting at least two components, comprising:

a shank having an axis;

at least one threaded portion being arranged at said shank and having a stressed cross section;

at least one elongation portion being arranged at said shank and having a stressed cross section, the stressed cross section of said at least one elongation portion being less than the stressed cross section of said at least one threaded portion up to 30 percent;

at least one fitting portion being arranged at said shank, having a stressed cross section and including a plurality of protrusions and channels, said at least one elongation portion and said at least one fitting portion being spaced apart along the axis of said shank, said channels having a root diameter determining the stressed cross section of said at least one fitting portion, the stressed cross section of said at least one fitting portion being at least 20 percent more than the stressed cross section of said at least one elongation portion.

2. The fastener of claim 1, wherein said elongation portion is designed to be continuously cylindrical without protrusions and channels.

3. The fastener of claim 1, wherein said at least one fitting portion has a surface bearing portion of at least 25 percent with respect to a cylindrical reference portion of the same diameter and the same length.

4. The fastener of claim 1, wherein said at least one threaded portion has an outer diameter, wherein said protrusions of said at least one fitting portion have an outer diameter, and wherein the outer diameter of said protrusions is more than the outer diameter of said at least one threaded portion up to 20 percent.

5. The fastener of claim 1, wherein said protrusions and said channels of said at least one fitting portion are designed and arranged to fully extend about the axis of said shank.

6. The fastener of claim 1, wherein said protrusions and said channels of said at least one fitting portion are designed and arranged to form an inclined spiral profile.

7. The fastener of claim 6, wherein said spiral profile is single-flight.

8. The fastener of claim 6, wherein said spiral profile is double-flight.

9. The fastener of claim 1, wherein said protrusions and said channels of said at least one fitting portion are produced by cold forming and calibrating.

10. The fastener of claim 9, wherein said at least one fitting portion is produced without cutting, and it has a flexibility according to the equation $\begin{array}{c}{\delta }_{}\end{array}$

S=4π

×

lTE×

dt2,(G)

wherein δ

_S represents the flexibility of said elongation portion, l_T represents the length of said elongation portion, E represents the modulus of elasticity of the material of said fastener and d_T represents the diameter of said elongation portion.

11. The fastener of claim 1, wherein said fastener is a fitting elongation screw.

12. The fastener of claim 1, wherein said fastener is a fitting threaded bolt.