Patent US5128192A successfully refreshed from Google Patents.
US5128192A
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US
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Braided preform process for thermoplastic honeycomb cores
Assignee: Northrop Grumman Corp
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Filing: 1990-02-02
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Granted: 1992-07-07
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Expires: 2010-02-02
Abstract
Abstract For producing ultra strong lightweight core material for composite structure such as aircraft wings, fairings and stabilizers, preimpregnated thermoplastic fiber yarn is processed according to this invention into blocks of ducted core material having a balanced honeycomb pattern. A tubular thermoplastic fabric sheath is braided along shaped mandrels, positioned end to end, as they pass through a braiding machine. The sheath is cut apart at the mandrel ends and the sheathed mandrels are stacked uniformly into a press, where the stack is compressed to contact all interfacial facets. Then heat is applied to fusion bond the stack together at the interfacial facets. Then after cooling to a setting temperature, the pressure is removed and the stack is removed from the press for mandrel extraction. In an embodiment utilizing metal mandrels treated with a release agent, the mandrels are extracted by pressing them out of the bonded block individually with a special long stroke pneumatic press having a long thin pin supported by fixed and floating bushings. In a preferred method, which eliminates extraction pressing, the mandrels are cast from a washable, high temperature eutectic salt so that the mandrels may be removed from the bonded stack by a hot water wash.
Inventors
- 👤 John R. Narasaki
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 21:32
CPC Classifications
B; B32; B32B; B32B3/00; B32B3/10; B32B3/12; B29; B29C; B29C33/00; B29C33/44; B29C33/52; B29C70/00; B29C70/04; B29C70/06; B29C70/10; B29C70/16; B29C70/22; B29C70/222; B29C70/28; B29C70/30; B29C70/34; B29C70/345; B29D; B29D99/00; B29D99/0089; B32B27/00; B32B27/06; B32B27/12; B32B2260/00; B32B2260/02; B32B2260/021; B32B2262/00; B32B2262/02; B32B2262/0207; B32B2262/0215; B32B2305/00; B32B2305/02; B32B2305/024; B32B2398/00; B32B2398/20; B32B2603/00; Y; Y10; Y10T; Y10T428/00; Y10T428/24; Y10T428/24149; Y10T428/24165
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
85 words
A method of producing a ducted core structure from preimpregnated thermoplastic fiber yarn comprising the steps of: (a) braiding preimpreganted thermoplastic fiber yarn lengthwise along hexagon shaped mandrels so as to form a braided sheath surrounding each mandrel; (b) stacking said mandrels, each thusly sheathed, in a lattice patterned stack; (c) bonding said sheaths together at interfacial facets thereof by application of heat to said stack; and (d) removing said mandrels from said stack to provide a ducted core structure having a hexagon shaped cells.
Claim 2
Independent Claim
85 words
A method of producing a ducted core structure from preimpregnated thermoplastic fiber yarn comprising the steps of: (a) braiding preimpreganted thermoplastic fiber yarn lengthwise along hexagon shaped mandrels so as to form a braided sheath surrounding each mandrel; (b) stacking said mandrels, each thusly sheathed, in a lattice patterned stack; (c) bonding said sheaths together at interfacial facets thereof by application of heat to said stack; and (d) removing said mandrels from said stack to provide a ducted core structure having a hexagon shaped cells.
Claim 3
Dependent Claim
50 words
The method according to claim 1 wherein said mandrels are formed prior to said step (a) by casting shaped mandrels with a washable, high temperature eutectic salt, and wherein, after said bonding step (c), said mandrels are removed from said stack in said step (d) with a hot water wash.
Claim 4
Dependent Claim
33 words
The method according to claim 1 wherein said mandrels in said step (a) are positioned end to end, and wherein step (a) further comprises cutting said sheath apart at ends of said mandrels.
Claim 5
Dependent Claim
50 words
The method according to claim 1 wherein said step (c) further comprises applying pressure to said stack to as to contact interfacial facets of said sheath, and wherein step (d) further comprises removing said heat and then, when said stack has cooled to below a setting temperature, removing said pressure.
Claim 6
Independent Claim
179 words
A method for making a block of hexagonal honeycomb ducted core structure from a length of preimpregnated braided reinforced thermoplastic yarn having a softening temperature above which thermoplastic fusion between adjacent sections of yarn can take place; providing a plurality of elongate mandrels having a hexagon shape in cross section; braiding the yarn into a hollow core sheath surrounding each mandrel; stacking the sheathed mandrels in a close packed 3-dimensional hexagonal array in which each face of each sheath is in contact with the face of an adjacent sheath throughout the interior volume of the array to form a honeycomb structure of open cells of hexagonal shape each side of each cell being bounded by double walls from two adjacent sheaths; mechanically pressing the array so formed while heating the array to a thermoplastic fusion temperature; subsequent cooling the array to below thermoplastic fusion temperature so that said sheaths are intimately bonded together throughout the array by fusion of the thermoplastic material impregnated into said yarn; removing said pressure and removing said mandrels to leave a block of honeycomb.
Claim 7
Independent Claim
179 words
A method for making a block of hexagonal honeycomb ducted core structure from a length of preimpregnated braided reinforced thermoplastic yarn having a softening temperature above which thermoplastic fusion between adjacent sections of yarn can take place; providing a plurality of elongate mandrels having a hexagon shape in cross section; braiding the yarn into a hollow core sheath surrounding each mandrel; stacking the sheathed mandrels in a close packed 3-dimensional hexagonal array in which each face of each sheath is in contact with the face of an adjacent sheath throughout the interior volume of the array to form a honeycomb structure of open cells of hexagonal shape each side of each cell being bounded by double walls from two adjacent sheaths; mechanically pressing the array so formed while heating the array to a thermoplastic fusion temperature; subsequent cooling the array to below thermoplastic fusion temperature so that said sheaths are intimately bonded together throughout the array by fusion of the thermoplastic material impregnated into said yarn; removing said pressure and removing said mandrels to leave a block of honeycomb.
Claim 8
Dependent Claim
29 words
A ducted core structure formed from preimpregnated thermoplastic fiber yarn comprising a plurality of ducts with mutually joining walls, said walls being formed of braided preimpreganted thermoplastic fiber yarn.
Claim 9
Dependent Claim
29 words
A ducted core structure formed from preimpregnated thermoplastic fiber yarn comprising a plurality of ducts with mutually joining walls, said walls being formed of braided preimpreganted thermoplastic fiber yarn.
Claim 10
Dependent Claim
24 words
A ducted core structure according to claim 6 wherein said adjoining walls are formed of a double layer of said braided preimpregnated thermoplastic yarn.
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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) | 1995-07-07 | 1996-01-06 | 1996-07-07 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-07-07 | 2000-01-06 | 2000-07-07 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-07-07 | 2004-01-06 | 2004-07-07 | $7700.00 | Window Closed / Lapsed |