A Conceptual Design for Deflection Device in VTDP System
The effectiveness of the Vectored Thrust Ducted Propeller (VTDP) system is not high currently, especially the lateral force is not large enough. Thus, a conceptual design for a deflection device of a VTDP system was proposed to achieve effective hovering control. The magnitude of the lateral force that was applied to maintain balance while hovering was examined. A comparison between the experimental and numerical results for the 16H-1 was made to verify the numerical simulation approach. The deflection devices of the X-49 and the proposed design were analyzed using numerical simulations. The results indicated that a larger lateral force and lower power consumption were presented in the proposed design. The results of this article provide a new idea for the design of the VTDP system.
Figure 1
Figure 2
Figure 3
Figure 4
Figure 5
Figure 6
Figure 7
Figure 8
Figure 9
Figure 10
Figure 11
Figure 12
Figure 13
Figure 14
Figure 15
Figure 16
Figure 17
Figure 18
Figure 19
Figure 20
Figure 21
Figure 22
Figure 23
Figure 24
Figure 25
Figure 26
Figure 27
Figure 28
Figure 29
Figure 30
Posted 15 Oct, 2020
Received 13 Oct, 2020
Invitations sent on 08 Oct, 2020
On 08 Oct, 2020
On 06 Oct, 2020
On 05 Oct, 2020
On 05 Oct, 2020
On 16 Sep, 2020
Received 15 Sep, 2020
On 05 Sep, 2020
Received 02 Sep, 2020
On 29 Aug, 2020
Invitations sent on 25 Aug, 2020
On 24 Aug, 2020
On 24 Aug, 2020
On 23 Aug, 2020
On 23 Aug, 2020
A Conceptual Design for Deflection Device in VTDP System
Posted 15 Oct, 2020
Received 13 Oct, 2020
Invitations sent on 08 Oct, 2020
On 08 Oct, 2020
On 06 Oct, 2020
On 05 Oct, 2020
On 05 Oct, 2020
On 16 Sep, 2020
Received 15 Sep, 2020
On 05 Sep, 2020
Received 02 Sep, 2020
On 29 Aug, 2020
Invitations sent on 25 Aug, 2020
On 24 Aug, 2020
On 24 Aug, 2020
On 23 Aug, 2020
On 23 Aug, 2020
The effectiveness of the Vectored Thrust Ducted Propeller (VTDP) system is not high currently, especially the lateral force is not large enough. Thus, a conceptual design for a deflection device of a VTDP system was proposed to achieve effective hovering control. The magnitude of the lateral force that was applied to maintain balance while hovering was examined. A comparison between the experimental and numerical results for the 16H-1 was made to verify the numerical simulation approach. The deflection devices of the X-49 and the proposed design were analyzed using numerical simulations. The results indicated that a larger lateral force and lower power consumption were presented in the proposed design. The results of this article provide a new idea for the design of the VTDP system.
Figure 1
Figure 2
Figure 3
Figure 4
Figure 5
Figure 6
Figure 7
Figure 8
Figure 9
Figure 10
Figure 11
Figure 12
Figure 13
Figure 14
Figure 15
Figure 16
Figure 17
Figure 18
Figure 19
Figure 20
Figure 21
Figure 22
Figure 23
Figure 24
Figure 25
Figure 26
Figure 27
Figure 28
Figure 29
Figure 30