US5616887A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Electrical and mechanical cable connector permitting relative rotation between connector components
Assignee: Airbus Operations GmbH
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Filing: 1995-07-21
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Granted: 1997-04-01
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Expires: 2015-07-21
Abstract
Abstract An electrical and mechanical cable connector is constructed for maintaining an electrical grounding circuit in electrical installations on board of an aircraft. For this purpose the connector has two bodies positioned coaxially to each other and rotatable to each other but restrained against relative axial movement by a spring ring. One of the two bodies has a plurality of contact springs formed by cutting axial slots integrally into a portion of the one body. The body with the contact springs rests at least partly in or on the respective support body. Both bodies have a common central axis and contact pressures are effective radially inwardly or radially outwardly relative to the common central axis and are axially distributed along the central axis, whereby both bodies are electrically interconnected to maintain the grounding circuit.
Inventors
- 👤 Safa Kirma
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 08:57
CPC Classifications
H; H01; H01R; H01R35/00; H01R13/00; H01R13/648; H01R13/658; H01R13/6581; H01R13/6582; H01R13/6583; H01R13/6591; H01R13/6592; H01R13/6593
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
153 words
An electrical and mechanical cable connector for protecting electrical installations in an aircraft against electromagnetic overloads, comprising a cylindrical hollow contact first body (1) of electrically conducting material having a circumferentially closed section (1.1) and an axially slotted section (1.2) forming electrical contact springs (1.3), a cylindrical hollow support second body (2) coaxially supporting said contact first body (1) in a manner permitting relative rotation between said first body and said second body, and an axial displacement preventing member (4) engaging said contact first body and said support second body (2) while permitting said relative rotation, and wherein said electrical contact springs (1.3) exert a biasing pressure against said support second body for conducting said electromagnetic overloads through said electrical contact springs, said pressure being distributed in a substantially radial direction relative to a central longitudinal axis (6) of said cable connector (18) and axially distributed in parallel to said central longitudinal axis.
Claim 2
Dependent Claim
153 words
An electrical and mechanical cable connector for protecting electrical installations in an aircraft against electromagnetic overloads, comprising a cylindrical hollow contact first body (1) of electrically conducting material having a circumferentially closed section (1.1) and an axially slotted section (1.2) forming electrical contact springs (1.3), a cylindrical hollow support second body (2) coaxially supporting said contact first body (1) in a manner permitting relative rotation between said first body and said second body, and an axial displacement preventing member (4) engaging said contact first body and said support second body (2) while permitting said relative rotation, and wherein said electrical contact springs (1.3) exert a biasing pressure against said support second body for conducting said electromagnetic overloads through said electrical contact springs, said pressure being distributed in a substantially radial direction relative to a central longitudinal axis (6) of said cable connector (18) and axially distributed in parallel to said central longitudinal axis.
Claim 3
Dependent Claim
57 words
The cable connector of claim 1, wherein said contact first body (1) surrounds said support second body (2) in contact with an outer circumferential surface of said support second body (2), and wherein said electrical contact springs (1.3) are biased radially inwardly into contact with said support second body (2) to which spring biasing forces are distributed.
Claim 4
Dependent Claim
58 words
The cable connector of claim 1, wherein said contact first body (1) is supported inside said support second body (2) by contacting an inner circumferential surface of said support second body (2), and wherein said electrical contact springs (1.3) are biased radially outwardly into contact with said support second body (2) to which spring biasing forces are distributed.
Claim 5
Dependent Claim
52 words
The cable connector of claim 1, wherein said support second body (2) has a large diameter section (2.1), a small diameter section (2.2), and a shoulder (2.3) connection said sections (2.1, 2.2) to each other, said contact first body (1) contracting said small diameter section (2.2) of said support second body (2).
Claim 6
Dependent Claim
48 words
The cable connector of claim 4, further comprising a coupling nut (16) rotatably supported on said large diameter section (2.1), and a further axial displacement preventing member engaging said coupling nut (16) and said support second body (2) to permit relative rotation therebetween but prevent an axial displacement.
Claim 7
Dependent Claim
53 words
The cable connector of claim 2, further comprising a contact pressure increasing spring clasp (8) surrounding said electrical contact springs (1.3) thereby increasing a contact pressure between said electrical contact springs and said support second body (2) while substantially eliminating any bending moments between said springs (1.3) and said circumferentially closed section (1.1).
Claim 8
Dependent Claim
38 words
The cable connector of claim 6, wherein said pressure increasing spring clasp (8) is a circular split spring, and wherein said electrical contact springs (1.3) comprise a groove in which said pressure increasing spring clasp (8) is received.
Claim 9
Dependent Claim
68 words
The cable connector of claim 1, wherein said contact first body (1) comprises a flange (5) connected radially outwardly to said contact first body (1) and an axially extending rim (15) connected to said flange, said rim (15) being spaced radially outwardly from an outer circumference of said support second body (2) to form an axially facing groove (3) for holding an end of a protective cable hose.
Claim 10
Dependent Claim
138 words
An electrical and mechanical cable connector for protecting electrical installations in an aircraft, comprising a coupling nut (16), a hollow cylindrical support body (2A) made of electrically conducting material supporting said coupling nut (16) in a manner permitting relative rotation between said coupling nut (16) and said support body (2A), an axial displacement preventing member (4.1) engaging said coupling nut (16) and said support body (2A) while permitting said relative rotation, said support body (2A) comprising a large diameter section (2.1A), a small diameter section (2.3A) and a shoulder (2.4A) between said sections (2.1A, 2.3A), said large diameter section (2.1A) comprising a circumferentially closed portion (2.1A) and an axially slotted portion forming electrical contact springs (2.2A) biased radially relative to a central longitudinal axis (6) of said cable connector and in parallel to said central longitudinal axis (6).
Claim 11
Dependent Claim
138 words
An electrical and mechanical cable connector for protecting electrical installations in an aircraft, comprising a coupling nut (16), a hollow cylindrical support body (2A) made of electrically conducting material supporting said coupling nut (16) in a manner permitting relative rotation between said coupling nut (16) and said support body (2A), an axial displacement preventing member (4.1) engaging said coupling nut (16) and said support body (2A) while permitting said relative rotation, said support body (2A) comprising a large diameter section (2.1A), a small diameter section (2.3A) and a shoulder (2.4A) between said sections (2.1A, 2.3A), said large diameter section (2.1A) comprising a circumferentially closed portion (2.1A) and an axially slotted portion forming electrical contact springs (2.2A) biased radially relative to a central longitudinal axis (6) of said cable connector and in parallel to said central longitudinal axis (6).
Claim 12
Dependent Claim
56 words
The cable connector of claim 9, wherein said coupling nut (16) surrounds said support body (2A) in contact with an outer circumferential surface of said electrical contact springs (2.2A) which are biased radially outwardly into contact with said coupling nut (16), whereby a biasing force of all contact springs is distributed into said coupling nut (16).
Claim 13
Dependent Claim
56 words
The cable connector of claim 9, wherein said support body (2A) surrounds said coupling nut (16) in contact with an inner circumferential surface of said electrical contact springs (2.2A), which are biased radially inwardly into contact with said coupling nut (16), whereby a biasing force of all contact springs is distributed into said coupling nut (16).
Claim 14
Dependent Claim
60 words
The cable connector of claim 11, further comprising a contact pressure increasing spring clasp (8.1) surrounding said electrical contact springs (2.2A) thereby increasing a contact pressure between said electrical contact springs and said coupling nut (16) radially inwardly onto said coupling nut (16), while substantially eliminating any bending moments between said contact springs (2.2A) and said circumferentially closed portion (2.1A).
Claim 15
Dependent Claim
39 words
The cable connector of claim 12, wherein said pressure increasing spring clasp (8.1) is a circular split spring (8.1) and wherein said electrical contact springs (2.2A) comprise a groove in which said pressure increasing split spring (8.1) is received.
Claim 16
Dependent Claim
24 words
The cable connector of claim 9, wherein said electrical contact springs (2.2A) and said support body (2A) are constructed as a single-piece integral component.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2000-03-31 | 2000-09-30 | 2001-04-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2004-03-31 | 2004-09-30 | 2005-04-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2008-03-31 | 2008-09-30 | 2009-04-01 | $7700.00 | Window Closed / Lapsed |