FIELD: aircraft; rocket engineering.
SUBSTANCE: group of inventions relates to aircraft and rocket engineering. Method of making hypersonic aircraft body from composite materials is characterised by that it is made by winding or volume plaiting of one or more shells of revolution, from which are cut at predetermined coordinates upper and lower aircraft airframe skin panel. Method includes making tip, side edge and bottom cover. All parts are rigidly jointed together to form a given aerodynamic shape of body. Body is characterised by using said method.
EFFECT: group of inventions is aimed at simplifying manufacturing of body.
2 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MODEL OF THE AIRCRAFT AIRFOIL | 2016 |
|
RU2653773C1 |
| AERODYNAMIC STEERING WHEEL OF A HYPERSONIC AIRCRAFT IN THE CONDITIONS OF ITS AERODYNAMIC HEATING | 2017 |
|
RU2680949C2 |
| AERODYNAMIC MODEL OF AIRCRAFT WITH INTEGRATED AIR BREATHING ENGINE | 2008 |
|
RU2370744C1 |
| TIP OF A HYPERSONIC AIRCRAFT | 2016 |
|
RU2651344C1 |
| METHOD OF MANUFACTURE OF HOLLOW BEARING-WALL SKELETON STRUCTURES | 1991 |
|
RU2030336C1 |
| STRUCTURAL MESH SHELL MADE OF COMPOSITE MATERIALS WITH METAL SKIN AND METHOD FOR MANUFACTURE THEREOF | 2020 |
|
RU2765630C1 |
| AIRCRAFT WING FROM POLYMER COMPOSITES | 2012 |
|
RU2531114C2 |
| MANUFACTURING METHOD OF WEDGE-SHAPED RADAR-TRANSPARENT FRONT FAIRING OF SUPERSONIC AIRCRAFT BODY | 2020 |
|
RU2744058C1 |
| HYPERSONIC FLYING VEHICLE | 1999 |
|
RU2172278C2 |
| SKIN PANEL SUFFERING CONSIDERABLE THERMAL LOADS DUE TO AERODYNAMIC HEATING | 1993 |
|
RU2088495C1 |
