An airbus with retractable landing gear
A technology of landing gear and air bus, applied in the direction of railway car body parts, etc., can solve the problems of unsatisfactory implementation effect, troublesome implementation, and inability to make turns.
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Embodiment 1
[0027] The reference picture is Figure 1-6 . An air bus with a retractable landing gear, comprising: a compartment 1, a number of retractable landing gear 2, wheels 3, a number of first drive motors 4, a protective layer 5 of an elevating landing gear, auxiliary wheels 6, and a number of second A driving motor 7 and a processing device 8, the processing device 8 is respectively connected to the first driving motor 4 and the second driving motor 7, the first driving motor 4 is connected to the retractable landing gear 2, The retractable landing gear 2 is connected to the wheels 3, the second drive motor 7 is connected to the protective layer 5 of the lifting landing gear, the protective device of the lifting landing gear is connected to the auxiliary wheels 6, The protective layer 5 of the elevating landing gear is divided into several protective areas 9, the number of the protective areas 9 is consistent with the number of the retractable landing gear 2, and the protective a...
Embodiment 2
[0036] The reference picture is Figure 5 . The airbus also includes a storage place 12, which is used to store the retractable landing gear 2 and the wheels 3.
[0037] The storage place 11 also includes a pressure sensor 13, the pressure sensor 13 is connected to the processing device 8, the pressure sensor 13 is located at the top of the storage place 12, and the pressure sensor 13 is used to sense the Whether the wheels 3 exert pressure on the pressure sensor 13 after the landing gear 2 is retracted.
[0038] The retractable landing gear 2 is provided with a folded part, and the pressure sensor 13 does not sense pressure, then the processing device 8 judges that the retractable landing gear 2 has not been recovered, and the processing device 8 Drive the first driving motor 4 to control the folding part to fold the retractable landing gear 2 .
[0039] In the specific implementation process, each pressure sensor also has a corresponding letter number, when the pressure s...
Embodiment 3
[0041] The reference picture is Figure 4 . The retractable landing gear 2 includes a pillar 14, a diagonal brace 15, a beam 16, a sliding bearing 17, a retractable support rod 18, and a retractable action cylinder 19. The pillar 14 and the crossbeam 16 are in a beam frame type. structure, the diagonal brace 15 and the crossbeam 16 are in a truss structure, and the two ends of the diagonal brace 15 are fixed on the pillar 14 and the crossbeam 16, and the crossbeam 16 serves as a rotating shaft at the same time, and the pillar 14 The sliding bearing 17 is connected with the retractable support rod 18 , and the retractable support rod 18 is connected with the bearing frame through the retractable action cylinder 19 .
[0042] Both the front and the rear of the airbus have a fixed portion of 7 meters.
[0043] In the specific implementation process, when the retractable landing gear 2 is retracted, the retractable actuating cylinder 19 releases the retractable support rod 18 to...
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