US4265688A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for producing sandwich type structural components
Assignee: Airbus Defence and Space GmbH
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Filing: 1978-07-28
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Granted: 1981-05-05
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Expires: 1998-07-28
Abstract
Abstract The present invention relates to a method for producing sandwich type structural components having a honeycomb core interposed between two cover layers. These cover layers are preferably made of fiber reinforced synthetic material. Force introduction points are formed in the structural components by insertion of a core filler mass in the form of a prepolymer which reacts to become a thermoplast. Force introducing connecting elements are connected to the force introducing points by melting these connecting elements into the core filler mass especially by using ultrasonic energy, for example, for an ultrasonic welding operation.
Inventors
- 👤 Ekkehard Gorski
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 02:26
CPC Classifications
B; B32; B32B; B32B3/00; B32B3/10; B29; B29C; B29C65/00; B29C65/02; B29C65/40; B29C65/42; B29C65/56; B29C65/64; B29C65/645; B29C66/00; B29C66/01; B29C66/05; B29C66/10; B29C66/11; B29C66/112; B29C66/1122; B29C66/40; B29C66/47; B29C66/474; B29C66/70; B29C66/72; B29C66/725; B29C66/7252; B29C66/72525; B29C66/7254; B29D; B29D24/00; B29D24/002; B29D24/005; B32B3/12; B32B7/00; B32B7/04; B32B7/12; E; E04; E04C; E04C2/00; E04C2/30; E04C2/34; E04C2/36; B29C66/71; B32B2250/00; B32B2250/40; Y; Y10; Y10T; Y10T156/00; Y10T156/10; Y10T156/1052; Y10T156/1056; Y10T156/1057; Y10T428/00; Y10T428/23; Y10T428/233; Y10T428/234; Y10T428/236; Y10T428/24; Y10T428/24033; Y10T428/24041; Y10T428/24149; Y10T428/24157; Y10T428/24273; Y10T428/24322; Y10T428/24331
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
140 words
A method for manufacturing a sandwich type structural component, comprising the following steps: (a) providing a prefabricated honeycomb core having open pockets therein, (b) bonding a first cover layer to one surface of the honeycomb core, (c) introducing a thermoplastic prepolymer including a foaming agent into said pockets at least at one predetermined location of the structural component, said thermoplastic prepolymer being capable of reacting with said foaming agent to become a thermoplastic foam type material, (d) bonding a second cover layer to the opposite surface of the honeycomb structure, (e) applying ultrasonic energy to said at least one location to melt said thermoplastic foam type material and to sufficiently soften one cover layer for the insertion of a connecting means directly through the cover layer without predrilling, and (f) inserting said connecting means directly into the still soft location.
Claim 2
Independent Claim
140 words
A method for manufacturing a sandwich type structural component, comprising the following steps: (a) providing a prefabricated honeycomb core having open pockets therein, (b) bonding a first cover layer to one surface of the honeycomb core, (c) introducing a thermoplastic prepolymer including a foaming agent into said pockets at least at one predetermined location of the structural component, said thermoplastic prepolymer being capable of reacting with said foaming agent to become a thermoplastic foam type material, (d) bonding a second cover layer to the opposite surface of the honeycomb structure, (e) applying ultrasonic energy to said at least one location to melt said thermoplastic foam type material and to sufficiently soften one cover layer for the insertion of a connecting means directly through the cover layer without predrilling, and (f) inserting said connecting means directly into the still soft location.
Claim 3
Dependent Claim
28 words
The method of claim 1, wherein said thermoplastic prepolymer is a solid block of a thermoplastic mass which is inserted into said honeycomb core at said predetermined location.
Claim 4
Dependent Claim
13 words
The method of claim 1, wherein said thermplastic prepolymer is a granular material.
Claim 5
Dependent Claim
23 words
The method of claim 3, wherein said step of introducing comprises pouring said granular material into said honeycomb core at said predetermined location.
Claim 6
Dependent Claim
23 words
The method of claim 1, further comprising providing said connecting means with a tip to facilitate the insertion through the softened cover layer.
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) | 1984-05-04 | 1984-11-03 | 1985-05-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-05-04 | 1988-11-03 | 1989-05-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-05-04 | 1992-11-03 | 1993-05-05 | $7700.00 | Window Closed / Lapsed |