FIELD: production of composite materials.
SUBSTANCE: group of inventions relates to a method of producing a composite structure, an aircraft part and a stack of layers of a layered composite part. Layered composite structures are obtained using partially cured parts. Partial curing of parts is ensured by applying a catalyst on areas of parts to be completely cured.
EFFECT: said sections are cured at a temperature below normal, while the remaining sections of the part remain uncured, which allows them to undergo joint bonding or joint curing with other structures.
15 cl, 20 dwg
Title |
Year |
Author |
Number |
CONNECTION OF COMPOSITE MATERIALS |
2015 |
- Kohli, Dalip
- Macadams, Leonard
|
RU2708209C2 |
METHODS FOR THE JOINT CONNECTION OF THE FIRST THERMOSETTING COMPOSITE AND THE SECOND THERMOSETTING COMPOSITE WITH THE FORMATION OF A CURED COMPOSITE PART |
2018 |
- Nelson, Karl M.
- Shervud, Trevis Dzhejms
- Dalal, Khardik
- Nguen, Feliks N.
- Li, Dunjon
- Josioka, Keniti
- Koyanagi, Khideo, Endryu
|
RU2758430C2 |
BEARING STRUCTURAL SECTION, METHOD OF ITS APPLICATION AND ITS APPLICATION FOR FABRICATION OF VEHICLE BODY REINFORCED PART |
2011 |
- Bjurkner Shteffen
- Sholler Jokhen
- Khanzen Ehrik
|
RU2576305C2 |
BONDING OF COMPOSITE MATERIALS |
2014 |
- Makadams Leonard
- Kokhli Dalip K.
|
RU2633581C2 |
COMPOSITE MATERIAL WITH IMPROVED PROPERTIES FOR MOULDING AND METHOD OF MAKING SUCH COMPOSITE MATERIAL AND MOULDED PART THEREFROM |
2017 |
- Vedemajer Andreas
- Poller Benyamin
|
RU2729247C1 |
COMPOSITE MATERIALS BONDING |
2013 |
- Makadams Leonard A.
- Kokhli Dalip K.
|
RU2618055C2 |
METHOD OF CONNECTING TWO COMPONENTS |
2008 |
- Mejer Dzhonatan
- Dzhons Dehniehl
- Khehnstridzh Ehndrju
|
RU2477678C2 |
METHOD OF PRODUCING SOLID PART OF FIBROUS COMPOSITE |
2009 |
|
RU2493010C2 |
STRUCTURED THERMOPLASTIC IN INTERSHEET ZONES OF COMPOSITE MATERIALS |
2011 |
|
RU2602159C2 |
THERMOSETTING RESIN CONTAINING EXPOSED THERMOPLASTIC AGENT FOR INCREASING IMPACT STRENGTH |
2008 |
- Koz Dzhon L.
- Mortimer Stefen
- Uehjd Kristofer Dzh.
|
RU2455317C1 |