A combined material frame roof beam casing integral structure for wing body fuses unmanned aerial vehicle
The utility model relates to a combined material frame roof beam casing integral structure for wing body fuses unmanned aerial vehicle belongs to aircraft technical field. This kind of combined material frame roof beam casing integral structure that is used for wing body fusion unmanned aerial vehic...
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| Main Authors | , , , , |
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| Format | Patent |
| Language | Chinese English |
| Published |
09.01.2018
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| Subjects | |
| Online Access | Get full text |
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| Summary: | The utility model relates to a combined material frame roof beam casing integral structure for wing body fuses unmanned aerial vehicle belongs to aircraft technical field. This kind of combined material frame roof beam casing integral structure that is used for wing body fusion unmanned aerial vehicle, including fuselage casing, fuselage long purlin, first frame roof beam and second frame roof beam, fuselage casing middle part both sides system has the wing, and fuselage length purlin sets up in the fuselage casing along fuselage casing axis direction, and first frame roof beam sets up at theinside front end of the wing of fuselage casing, and first frame roof beam includes preceding mast of wing and first fuselage deckle board, second frame roof beam includes wing back beam and second fuselage deckle board. The utility model discloses a be assembled between/be connected between, simple structure not only, constitutional detail quantity reduces, and because the frame roof beam is integrative, it is direct tha |
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| Bibliography: | Application Number: CN20172740501U |