Title:
AIRCRAFT AND BLI PROPULSION UNIT
Document Type and Number:
WIPO Patent Application WO/2023/074368
Kind Code:
A1
Abstract:
[Problem] To provide a technology capable of increasing a propulsion efficiency in a BLI propulsion technology. [Solution] An aircraft according to the present technology comprises a fuselage and a BLI propulsion unit. The fuselage is cylindrical, long in the axial direction and short in the width direction and the vertical direction and has a rear end on the rear side in the axial direction. The BLI propulsion unit is located on the rear side of the fuselage and has an air intake, in which the center position of the air intake is offset from the center position of the rear end in one or both of the vertical direction and the width direction.
Inventors:
KOBAYASHI HIROSHI (JP)
YOKOKAWA YUZURU (JP)
SUZUKI MASAYUKI (JP)
NISHIZAWA AKIRA (JP)
IIJIMA RYUJI (JP)
SHIMA EIJI (JP)
YOKOKAWA YUZURU (JP)
SUZUKI MASAYUKI (JP)
NISHIZAWA AKIRA (JP)
IIJIMA RYUJI (JP)
SHIMA EIJI (JP)
Application Number:
PCT/JP2022/038038
Publication Date:
May 04, 2023
Filing Date:
October 12, 2022
Export Citation:
Assignee:
JAPAN AEROSPACE EXPLORATION (JP)
International Classes:
B64D33/02; B64C11/48; B64C21/06; B64D27/14; F01D17/20
Foreign References:
| JP2020040649A | 2020-03-19 | |||
| JP2019039420A | 2019-03-14 | |||
| US20150000252A1 | 2015-01-01 |
Attorney, Agent or Firm:
MINAMI AOYAMA PATENT AND TRADEMARK ATTORNEYS (JP)
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