TY - GEN
T1 - Differential pressure measurement of an insect wing using a MEMS sensor
AU - Takahashi, Hidetoshi
AU - Matsumoto, Kiyoshi
AU - Shimoyama, Isao
PY - 2012
Y1 - 2012
N2 - An insect can perform flight maneuvers such as hovering and snap turns. There have been many methods such as digital particle image velocimetry (DPIV) or kinematic analysis using robotic wings modeled on insects to investigate the aerodynamic force. The aerodynamic force is derived from the differential pressure between the upper and lower surfaces of its wings. The actual aerodynamic force on real insect wings has never been measured directly during free flight. Here we show direct measurement of differential pressure acting on the wing surface of a real insect during free flight. A micro differential pressure sensor was fabricated by utilizing micro electro mechanical systems (MEMS) and fixed to a butterfly (Papilio protenor) wing. The size and weight of the sensor chip are 1.0 mm x 1.0 mm x 0.3 mm and 0.7 mg, respectively. The differential pressures were measured during takeoff. From the measured differential pressure distribution, aerodynamic force was calculated. The maximum aerodynamic force generated on the wings was 3 times larger than the gravity acting on the body.
AB - An insect can perform flight maneuvers such as hovering and snap turns. There have been many methods such as digital particle image velocimetry (DPIV) or kinematic analysis using robotic wings modeled on insects to investigate the aerodynamic force. The aerodynamic force is derived from the differential pressure between the upper and lower surfaces of its wings. The actual aerodynamic force on real insect wings has never been measured directly during free flight. Here we show direct measurement of differential pressure acting on the wing surface of a real insect during free flight. A micro differential pressure sensor was fabricated by utilizing micro electro mechanical systems (MEMS) and fixed to a butterfly (Papilio protenor) wing. The size and weight of the sensor chip are 1.0 mm x 1.0 mm x 0.3 mm and 0.7 mg, respectively. The differential pressures were measured during takeoff. From the measured differential pressure distribution, aerodynamic force was calculated. The maximum aerodynamic force generated on the wings was 3 times larger than the gravity acting on the body.
KW - Aerodynamic force
KW - Butterfly
KW - Differential pressure
KW - Insect flapping flight
KW - MEMS sensor
UR - http://www.scopus.com/inward/record.url?scp=84867638818&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84867638818&partnerID=8YFLogxK
U2 - 10.1109/ICCME.2012.6275673
DO - 10.1109/ICCME.2012.6275673
M3 - Conference contribution
AN - SCOPUS:84867638818
SN - 9781467316163
T3 - 2012 ICME International Conference on Complex Medical Engineering, CME 2012 Proceedings
SP - 349
EP - 352
BT - 2012 ICME International Conference on Complex Medical Engineering, CME 2012 Proceedings
T2 - 6th International Conference on Complex Medical Engineering, CME 2012
Y2 - 1 July 2012 through 4 July 2012
ER -