TW201613800A - Booster propulsion device of multi-axis helicopter - Google Patents

Booster propulsion device of multi-axis helicopter

Info

Publication number
TW201613800A
TW201613800A TW103134614A TW103134614A TW201613800A TW 201613800 A TW201613800 A TW 201613800A TW 103134614 A TW103134614 A TW 103134614A TW 103134614 A TW103134614 A TW 103134614A TW 201613800 A TW201613800 A TW 201613800A
Authority
TW
Taiwan
Prior art keywords
driving unit
axis helicopter
propulsion device
horizontal propeller
helicopter
Prior art date
Application number
TW103134614A
Other languages
Chinese (zh)
Inventor
Max Yu-Fu Su
Original Assignee
Max Yu-Fu Su
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Max Yu-Fu Su filed Critical Max Yu-Fu Su
Priority to TW103134614A priority Critical patent/TW201613800A/en
Publication of TW201613800A publication Critical patent/TW201613800A/en

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Abstract

The invention refers to a booster propulsion device of multi-axis helicopter. The booster propulsion device is mounted beneath the body of the multi-axis helicopter and comprises a driving unit and a horizontal propeller. The driving unit electrically connecting with the throttle controller of the multi-axis helicopter so that the driving unit can link mechanically with the horizontal propeller and adjust the included angle between the horizontal propeller and the body. Accordingly, by means of controlling the speed of the multi-axis helicopter via the throttle controller, the throttle controller can provide the feedback of sensing signal to the driving unit. In such a case, the driving unit can link up with the horizontal propeller and adjust the included angle so that the multi-axis helicopter can keep balance stably in high-speed conditions.
TW103134614A 2014-10-03 2014-10-03 Booster propulsion device of multi-axis helicopter TW201613800A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW103134614A TW201613800A (en) 2014-10-03 2014-10-03 Booster propulsion device of multi-axis helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW103134614A TW201613800A (en) 2014-10-03 2014-10-03 Booster propulsion device of multi-axis helicopter

Publications (1)

Publication Number Publication Date
TW201613800A true TW201613800A (en) 2016-04-16

Family

ID=56361126

Family Applications (1)

Application Number Title Priority Date Filing Date
TW103134614A TW201613800A (en) 2014-10-03 2014-10-03 Booster propulsion device of multi-axis helicopter

Country Status (1)

Country Link
TW (1) TW201613800A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI610851B (en) * 2016-03-31 2018-01-11 英華達股份有限公司 A multi-axes unmanned aerial vehicle and the flying method thereof
TWI625270B (en) * 2017-04-19 2018-06-01 威拓動力有限公司 Triaxial helicopter

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI610851B (en) * 2016-03-31 2018-01-11 英華達股份有限公司 A multi-axes unmanned aerial vehicle and the flying method thereof
TWI625270B (en) * 2017-04-19 2018-06-01 威拓動力有限公司 Triaxial helicopter
US10526082B2 (en) 2017-04-19 2020-01-07 Max Su Triaxial helicopter

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