TILTING STRUCTURE AND AIRCRAFT - GUANGDONG HUITIAN AEROSPACETECHNOLOGY CO LTD

Title:

TILTING STRUCTURE AND AIRCRAFT

Document Type and Number:

WIPO Patent Application WO/2022/241974

Kind Code:

A1

Abstract:

A tilting structure and an aircraft comprising the tilting structure. The tilting structure comprises a machine arm (100), a tilting electric motor (200) arranged on the machine arm (100), and a power electric motor assembly (300) in transmission connection with a driving shaft of the tilting electric motor (200). The tilting structure further comprises a shaft connection rotation member (400), the shaft connection rotation member (400) being provided with a first connecting member (410) and a second connecting member (420), wherein the driving shaft of the tilting electric motor (200) is connected to the shaft connection rotation member (400) by means of the first connecting member (410); and the shaft connection rotation member (400) is rotationally connected to the machine arm (100) by means of the second connecting member (420). The machine arm (100), the shaft connection rotation member (400), the first connecting member (410) and the second connecting member (420) are coaxially arranged. By means of the tilting structure, the radial force borne by the driving shaft of the tilting electric motor can be reduced, such that the flight safety of the aircraft is improved.

More Like This:

WO/2023/146965	INTEGRATED PROPELLER-BOOM FAIRING
JP2006021733	VERTICAL TAKING-OFF AND LANDING MACHINE INSTALLING RAPID WIND QUANTITY GENERATION WIND DIRECTION CHANGING DEVICE OF DOUBLE INVERSION TWO-AXIS TILT AS DEVICE FOR LIFT AND PROPULSION OF MACHINE BODY AND USING IT AS STEERING MEANS
WO/2021/109311	GROUND EFFECT BASED ROTORCRAFT AND FLIGHT MODE SWITCHING CONTROL METHOD

Inventors:

ZHAO DELI (CN)
ZHOU SHUANGJIU (CN)
LI JIE (CN)

Application Number:

PCT/CN2021/117096

Publication Date:

November 24, 2022

Filing Date:

September 08, 2021

Export Citation:

Click for automatic bibliography generation Help

Assignee:

GUANGDONG HUITIAN AEROSPACETECHNOLOGY CO LTD (CN)

International Classes:

B64C27/52; B64C1/06

Foreign References:

CN113086182A	2021-07-09
CN206087334U	2017-04-12
CN108945395A	2018-12-07
CN209776795U	2019-12-13
GB957314A	1964-05-06
US5620305A	1997-04-15

Attorney, Agent or Firm:

BEIJING ZHOZHIJUNDA ATTORNEYS AT LAW (CN)

Download PDF:

View/Download PDF PDF Help

Previous Patent: TROPOLONE-CHITOSAN DERIVATIVE, AND PREPARATION METHOD THEREFOR AND USE THEREOF

Next Patent: METHODS FOR TREATING CANCERS ASSOCIATED WITH EGFR MUTATION