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Về hiện tượng phá hủy và kiểm bền cho máy bay không người lái UAV dạng cánh bằng
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Mô tả chi tiết
1 NGHIEN CiAj-TRAOD6l
X/VE HIEN Tl/aNG PHA HUY VA KIEiVl BEN
CHO iVIAY BAY KHONG NGL/O^I LAI UAV DANG CANH BANG
DESTROYED PHENOMENON AND ENDURANCE TEST
FOR UNMANNED AERIAL VEHICLE UAV AIRPLANE TYPE
TS. Tran Dflc Quy, ThS. Nhfl Quy Thd
Trfldng Dai hpc Cdng nghiep Ha Npi
TOM TAT
Trong qud trinh bay thii nghiem hay bay that, cd rat nhieu mdu bay UAV [1] bi phd huy, ddc biet
la phd huy tren be mat cdnh, gdy thiet hai Idn. Bdi bdo ndy trinh bdy cdc nguyin nhdn gdy ra hien tUdng
phd huy bien dang mdy bay UAV dUa tren nguyen ly ddn hoi khi ddng. Ngodi ra, bdi bdo cung trinh bdy
cdc ket qud dat dUdc khi tien hdnh kiem ben cho mdu UAV lam bang sdi composite, trong do phdn cdnh
dUdcgia cdthem bdi thanh thep cacbon cUdng cting loai trung binh (hdm lUdngcacbon 0.25 - 0.6%) [I]
trong dieu kien thdi tiet thay doi vdi gio cap 2, cap 3, cap 4 vd cap 6. Cdc ket qud tinh todn dUdc md phdng
trin Ansys CFX.
Tfl khda: Mdy hay khdng ngUdi ldi, hien tUdngphd huy, kiem ben, md phdng, khi ddng hgc.
ABSTRACT
During the flight, many models UAV [1] have been destroyed. Especially, many UAV were
destroyed on the surface of the wing. This paper, based on aerodynamic elastic principles, presents causes
of the destroyed phenomenon of UAV's profile. Also, the paper presents the results obtained when conducting
durable fiber composite UAV model in which the wings are reinforced by hard steel of average carbon
intensity (carbon 0:25 - 0.6% )[1] in changing weather conditions with 2 level, 3 level, 4 level and 6 level
windy. The calculation results are simulated in Ansys CFX.
Keywords: Unmanned Aerial Vehicle, destroyed phenomenon, endurance test, simulation,
aerodynamic.
TAP CHi CO KHi VI£ T NAM, Sd 12 nam 2013