← Back to Patent Explorer
US4348140A Expired / Lapsed US ⏱️ 0.0 years remaining

Connecting device, preferably for sheet metal components of light metal allows

Assignee: Airbus Defence and Space GmbH
•
Filing: 1981-01-19
•
Granted: 1982-09-07
•
Expires: 2001-01-19
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract The present connecting device for joining sheet metal components has a la of synthetic material at least in the area of the contact surfaces with neighboring components thus effectively preventing contact corrosion.

Inventors

  • 👤 Helmut Bergholz
  • 👤 Walter Tams

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 09:51
CPC Classifications
F; F16; F16B; F16B33/00; F16B33/06; F16B33/004; F16B33/008; F16B5/00; F16B5/02; F16B5/0208; F16B37/00; F16B37/04; F16B37/041; F16B37/06; F16B37/062; F16B37/064; F16B37/065; Y; Y10; Y10T; Y10T403/00; Y10T403/75

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 195 words
An aircraft construction threaded nut assembly for transmitting forces between sheet metal pieces, comprising in combination a piece of sheet metal having first and second holes therein, a nut having a threaded hole, means rigidly securing said nut to said piece of sheet metal, whereby said threaded hole registers with a first hole in the piece of sheet metal, said securing means comprising holding means connected to the nut, at least one rivet hole in said holding means registering with a second hole in said piece of sheet metal, and at least one rivet extending through the rivet hole in the holding means of the nut and through a respective second hole in the piece of sheet metal, said assembly further comprising a coating of synthetic insulating material of sufficient mechanical strength for directly transmitting mechanical stress through the coating covering said holding means substantially on all sides including the wall of the rivet hole in the holding means, whereby the nut is insulated from the piece of sheet metal and from the rivet for releasably securing said piece of sheet metal to a further piece of sheet metal in a rigid, force transmitting manner.
Claim 2
Dependent Claim 195 words
An aircraft construction threaded nut assembly for transmitting forces between sheet metal pieces, comprising in combination a piece of sheet metal having first and second holes therein, a nut having a threaded hole, means rigidly securing said nut to said piece of sheet metal, whereby said threaded hole registers with a first hole in the piece of sheet metal, said securing means comprising holding means connected to the nut, at least one rivet hole in said holding means registering with a second hole in said piece of sheet metal, and at least one rivet extending through the rivet hole in the holding means of the nut and through a respective second hole in the piece of sheet metal, said assembly further comprising a coating of synthetic insulating material of sufficient mechanical strength for directly transmitting mechanical stress through the coating covering said holding means substantially on all sides including the wall of the rivet hole in the holding means, whereby the nut is insulated from the piece of sheet metal and from the rivet for releasably securing said piece of sheet metal to a further piece of sheet metal in a rigid, force transmitting manner.
Claim 3
Dependent Claim 26 words
The assembly of claim 1, wherein said holding means comprise two lugs extending from opposite sides of the nut, each lug having a rivet hole therein.
Claim 4
Dependent Claim 32 words
The assembly of claim 1, wherein said holding means comprise a flange plate (28) with rivet holes therein, said flange plate with its holes being coated with said synthetic material (FIG. 6).
Claim 5
Dependent Claim 16 words
The assembly of claim 3, wherein said nut is a threaded metal sleeve (25) (FIG. 6).

References Cited (Backward Citations)

US715813A Cited
US2336791A Cited
US2726009A Cited
US3176747A Cited
US3118480A Cited
GB889887A Cited
US3252215A Cited
US3620119A Cited
US3916970A Cited
US4074491A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-09-06 1986-03-08 1986-09-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-09-06 1990-03-08 1990-09-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-09-06 1994-03-08 1994-09-07 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag