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US4416349A Expired / Lapsed US ⏱️ 0.0 years remaining

Viscoelastically damped reinforced skin structures

Assignee: Boeing Co
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Filing: 1981-09-30
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Granted: 1983-11-22
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Expires: 2001-09-30
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Abstract

Abstract Viscoelastically damped reinforced skin structures wherein a sandwich skin having a relatively thick core is supported by structural elements, such as stringers and frames, are disclosed. In one form (FIG. 1), a main skin (15) is supported by stringers (13) that are in turn supported by frames (11). The skin, stringers and frames are securely attached to one another by any suitable means, such as a bonding adhesive, rivets, bolts, etc. Located between the stringers are core layers (17) formed of honeycomb or foam materials. A first plate (21) overlies each core layer and extends to the flanges of the adjacent stringer. A second plate (25) overlies each adjacent pair of first plates. The core layer is viscoelastically attached (19 and 23a) to the skin and the first plate; and, the first plate is viscoelastically attached (23b, c and 27a, b) to the stringer flanges and to the second plate. Alternatively, a single plate (49, FIG. 3) can overlie the core layers (47) and the stringers (43). In an alternative form of the invention (FIG. 4), the main skin (63) is located between the stringers (65) and the frames (61); and, is securely attached thereto. An outer skin (67) is viscoelastically attached (68a, b and 73) to the stringers (65) and to core layers (69). The core layers (69) are located between the main (63) and outer skin (67, and pairs of adjacent stringers (65). The core layers are also viscoelastically attached (71) to the main skin (63).

Inventors

  • 👤 Loyd D. Jacobs

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 19:26
CPC Classifications
G; G10; G10K; G10K11/00; G10K11/16; B; B64; B64C; B64C1/00; B64C1/06; B64C1/12; B64C1/40; B64C3/00; B64C3/18; B64C2001/0054; B64C2001/0072; Y; Y02; Y02T; Y02T50/00; Y02T50/40; Y10; Y10T; Y10T428/00; Y10T428/24; Y10T428/24149; Y10T428/31504; Y10T428/31551; Y10T428/31605

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 259 words
In a reinforced skin structure including a plurality of frames, a plurality of spaced-apart stringers and a skin, said plurality of stringers being affixed to and supported by said plurality of frames, said skin being affixed to and supported by said plurality of stringers, said plurality of stringers having a U-shape with outwardly projecting flanges oriented such that said skin is affixed to the crossmembers of said U-shaped stringers and the flanges of said U-shaped stringers are affixed to said plurality of frames, the improvement comprising an integral damping mechanism, said integral damping mechanism comprising: (A) core layers attached to said skin and located between adjacent pairs of spaced-apart stingers; and, (B) viscoelastic coupling means for selectively attaching said core layers to said stringers, said viscoelastic coupling means comprising: (1) a relatively stiff coupling comprising: (a) a first panel comprising a plurality of sections, each of said first panel sections extending from the flange of one of said stringers to the flange of the next adjacent stringer so as to overlie the core layer lying between said adjacent stringers; and, (b) a second panel comprising a plurality of sections, each of said second panel sections overlying an adjacent pair of first panel sections so as to span the area between the flanges of a U-shaped stringer; (2) stringer/coupling viscoelastic layers for attaching said first panel sections to said stringers; (3) core/coupling viscoelastic layers for attaching said first panel sections to said core layers; and (4) panel/panel viscoelastic layers for attaching said second panel sections to said first panel sections.
Claim 2
Dependent Claim 259 words
In a reinforced skin structure including a plurality of frames, a plurality of spaced-apart stringers and a skin, said plurality of stringers being affixed to and supported by said plurality of frames, said skin being affixed to and supported by said plurality of stringers, said plurality of stringers having a U-shape with outwardly projecting flanges oriented such that said skin is affixed to the crossmembers of said U-shaped stringers and the flanges of said U-shaped stringers are affixed to said plurality of frames, the improvement comprising an integral damping mechanism, said integral damping mechanism comprising: (A) core layers attached to said skin and located between adjacent pairs of spaced-apart stingers; and, (B) viscoelastic coupling means for selectively attaching said core layers to said stringers, said viscoelastic coupling means comprising: (1) a relatively stiff coupling comprising: (a) a first panel comprising a plurality of sections, each of said first panel sections extending from the flange of one of said stringers to the flange of the next adjacent stringer so as to overlie the core layer lying between said adjacent stringers; and, (b) a second panel comprising a plurality of sections, each of said second panel sections overlying an adjacent pair of first panel sections so as to span the area between the flanges of a U-shaped stringer; (2) stringer/coupling viscoelastic layers for attaching said first panel sections to said stringers; (3) core/coupling viscoelastic layers for attaching said first panel sections to said core layers; and (4) panel/panel viscoelastic layers for attaching said second panel sections to said first panel sections.
Claim 3
Dependent Claim 21 words
The improvement claimed in claim 1 wherein said core layers are attached to said skin by skin/core layers of viscoelastic material.
Claim 4
Dependent Claim 17 words
The improvement claimed in claim 2 wherein said core layers are formed of a honeycomb core material.
Claim 5
Dependent Claim 16 words
The improvement claimed in claim 2 wherein said core layers are formed of a foam material.
Claim 6
Dependent Claim 17 words
The improvement claimed in claim 1 wherein said core layers are formed of a honeycomb core material.
Claim 7
Dependent Claim 16 words
The improvement claimed in claim 1 wherein said core layers are formed of a foam material.

References Cited (Backward Citations)

US3020986A Cited
US3087574A Cited
US3976269A Cited
US4313524A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-11-21 1987-05-23 1987-11-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-11-21 1991-05-23 1991-11-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-11-21 1995-05-23 1995-11-22 $7700.00 Window Closed / Lapsed

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