US4389340A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Flexible, electrically conductive jointing material, particularly suitable for aircraft
Assignee: Dassault Aviation SA
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Filing: 1980-08-06
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Granted: 1983-06-21
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Expires: 2000-08-06
Abstract
Abstract A flexible, electrically conductive jointing material consists of an elastomer containing metal in a divided state distributed in its mass. The metal is in the form of laminae or paillettes of aluminium or of aluminium alloy, the length of which is greater than their width or thickness. The elastomer, which may be the product known under the name "Thiokol", exhibits a pasty consistency when applied enabling it to be spread with a spatula and mixed in situ. The jointing material may be used for connecting together the structural parts of aircraft.
Inventors
- 👤 Fernand J. Levy
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 07:24
CPC Classifications
H; H01; H01R; H01R13/00; H01R13/02; H01R13/22; H01R13/24; H01R13/2407; H01R13/2414; H01B; H01B1/00; H01B1/20; H01B1/22; H05; H05K; H05K3/00; H05K3/30; H05K3/32; H05K3/321
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
114 words
A composition of matter, for application to aircraft structural parts made of aluminum or aluminum alloy, comprising a flexible electrically-conductive jointing material consisting of a resilient electrically-insulating matrix formed of an elastomer selected as being, upon application at the desired site of the aircraft, of pasty consistency adapted for spreading and molding in situ, and of generally rectangular particles of aluminum or aluminum alloy distributed throughout said matrix and formed of scales having on average a length of approximately 2 to 4 millimeters, a width of approximately 100 to 150 microns and a thickness of approximately 30 to 60 microns, the proportion of scales in the elastomer being approximately of 1:4 parts by weight.
Claim 2
Dependent Claim
114 words
A composition of matter, for application to aircraft structural parts made of aluminum or aluminum alloy, comprising a flexible electrically-conductive jointing material consisting of a resilient electrically-insulating matrix formed of an elastomer selected as being, upon application at the desired site of the aircraft, of pasty consistency adapted for spreading and molding in situ, and of generally rectangular particles of aluminum or aluminum alloy distributed throughout said matrix and formed of scales having on average a length of approximately 2 to 4 millimeters, a width of approximately 100 to 150 microns and a thickness of approximately 30 to 60 microns, the proportion of scales in the elastomer being approximately of 1:4 parts by weight.
Claim 3
Dependent Claim
26 words
Composition as claimed in claim 1, wherein the elastomer has a liquid polysulphide polymer base which vulcanizes at ambient temperature under the action of an accelerator.
Claim 4
Dependent Claim
145 words
A jointing material for use as an electrically-conductive flexible seal to bond electrically-conductive metal surface portions of a structure, consisting of an electrically-insulating elastomer loaded with electrically-conductive metal particles distributed throughout its mass, wherein the metal of said particles is electrochemically compatible with the metal of said surface portions in that said metals do not form a galvanic couple, and said particles are in the form of generally rectangular scales having on average a length of approximately 2 to 4 millimeters, a width of approximately 100 to 150 microns and a thickness of approximately 30 to 60 microns, the proportion of said scales in said elastomer being approximately of 1:4 parts by weight, and wherein said elastomer, when applied at the desired site, exhibits a pasty consistency enabling it to be spread with a spatula for molding in situ upon setting into final flexible condition.
Claim 5
Dependent Claim
145 words
A jointing material for use as an electrically-conductive flexible seal to bond electrically-conductive metal surface portions of a structure, consisting of an electrically-insulating elastomer loaded with electrically-conductive metal particles distributed throughout its mass, wherein the metal of said particles is electrochemically compatible with the metal of said surface portions in that said metals do not form a galvanic couple, and said particles are in the form of generally rectangular scales having on average a length of approximately 2 to 4 millimeters, a width of approximately 100 to 150 microns and a thickness of approximately 30 to 60 microns, the proportion of said scales in said elastomer being approximately of 1:4 parts by weight, and wherein said elastomer, when applied at the desired site, exhibits a pasty consistency enabling it to be spread with a spatula for molding in situ upon setting into final flexible condition.
Claim 6
Dependent Claim
26 words
Material as claimed in claim 3, wherein said elastomer has a liquid polysulphide polymer base which vulcanizes at ambient temperature under the action of an accelerator.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-06-20 | 1986-12-20 | 1987-06-21 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-06-20 | 1990-12-20 | 1991-06-21 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-06-20 | 1994-12-20 | 1995-06-21 | $7700.00 | Window Closed / Lapsed |