High-speed aircraft and cartridge
A high-speed aircraft and channel technology, applied in the field of flight structures, can solve problems such as large resistance of flyable structures, and achieve the effect of energy saving in flight
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Embodiment 1
[0041] Please refer to figure 1 and figure 2, Embodiment 1 of the present invention is:
[0042] An aircraft, the fuselage shell 1 is respectively provided with an inner fluid passage 2 and an outer fluid passage 3 surrounding the fuselage, and the inner fluid passage 2 and the outer fluid passage 3 are respectively provided with a plurality of openings and the fuselage shell 1 The inner fluid channel 2 communicates with the port 6 through the conduit 602, the outer fluid channel 3 communicates with the port 601, the engine 4 is located at the tail of the fuselage shell 1, and its suction port communicates with the outer fluid channel 3, and the exhaust port 3 communicates with the port 6. The gas port communicates with the outside world, and the air intake area of the port 601 is larger than that of the port 6 .
[0043] When the aircraft is flying, the fluid enters the inner and outer fluid passages through the ports 6 and 601 respectively. At this time, the engine 4 ge...
Embodiment 2
[0051] Please refer to figure 1 and figure 2 , the second embodiment of the present invention is:
[0052] A kind of aircraft, different from Embodiment 1 is to remove conduit 602 and port 6, and evenly distribute a plurality of small aperture ports 603 with smaller apertures on the inner shell 102, so that the inner fluid passage 2 and the outer fluid passage 3 connected.
[0053] When the aircraft is running, the engine produces a strong suction force, which naturally makes it easier to suck the fluid on the shell at a high speed through the larger port 601, forming two layers of high-speed fluid layers 301 with approximately equal flow velocities on the channel and the surface of the shell, and at the same time The engine also sucks a small amount of fluid in the inner fluid passage 2 through the less small aperture opening 603 of the evenly distributed aperture in the outer fluid passage 3, because the intake area of the opening 601 is much larger than the small apert...
Embodiment 3
[0055] Please refer to Figure 1 to Figure 3 , Embodiment three of the present invention is:
[0056] An aircraft is provided with an inner fluid channel 2 and an outer fluid channel 3 around the upper and lower surfaces of the wing shell 5, wherein the inner fluid channel 2 in the fuselage shell 1 communicates with the outer fluid channel 3 in the wing shell.
[0057] When the aircraft is flying, the powerful suction of the engine 4 passes through the fuselage, and the evenly distributed openings 601 on the fuselage shell 1 suck the fluid into the outer fluid channel at a high speed, so that a high-speed fluid layer 301 is formed around the fuselage and the wing, and the fuselage Between the housing 1 and the inner fluid channel 2 in the wing housing 5, there is a huge pressure difference due to the difference in flow velocity, and the inner fluid channel 2 passes through the conduit 602 and the evenly distributed orifices 6 to release the high pressure generated by the low f...
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