JP7049234B2 - ハイブリッド飛行体 - Google Patents
ハイブリッド飛行体 Download PDFInfo
- Publication number
- JP7049234B2 JP7049234B2 JP2018214791A JP2018214791A JP7049234B2 JP 7049234 B2 JP7049234 B2 JP 7049234B2 JP 2018214791 A JP2018214791 A JP 2018214791A JP 2018214791 A JP2018214791 A JP 2018214791A JP 7049234 B2 JP7049234 B2 JP 7049234B2
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- Prior art keywords
- turbine
- rotor
- turbine engine
- gas turbine
- nacelle
- Prior art date
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- 230000001141 propulsive effect Effects 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 8
- 238000002485 combustion reaction Methods 0.000 description 7
- 239000000446 fuel Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 239000003381 stabilizer Substances 0.000 description 6
- 230000003247 decreasing effect Effects 0.000 description 3
- 101100393881 Arabidopsis thaliana GT16 gene Proteins 0.000 description 2
- 230000000740 bleeding effect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000012447 hatching Effects 0.000 description 1
- 230000015654 memory Effects 0.000 description 1
- 238000010992 reflux Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0083—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by several motors of different type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- B64D31/16—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants
- B64D31/18—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants for hybrid-electric power plants
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Description
図1はこの発明の第1実施形態に係るハイブリッド飛行体を全体的に示す斜視図、図2は図1のハイブリッド飛行体の機体に収容されるガスタービン・エンジンなどの説明断面図、図3は図2のハイブリッド飛行体のガスタービン・エンジンを含む構成要素を全体的に示すブロック図である。
図13はこの発明の第2実施形態に係るハイブリッド飛行体を模式的に示す、図2と同様のGT16などの説明断面図である。
抽気路、26b タービン、36 電子制御ユニット(ECU。制御部)、40 回転数センサ、42,44,46 温度センサ、50,52 圧力センサ、54 高度計(ALT)、56 ジャイロセンサ、60 GPS受信機、62 回転数センサ、80 熱交換器
Claims (4)
- 複数の翼を有する機体と、
前記複数の翼のそれぞれに設けられた環状のナセルと、
前記ナセルに収容され、前記機体のヨー軸と平行な回転軸を有し、前記機体を推進させる推進力を生じるロータと、
前記機体に取り付けられると共に、圧縮機と前記圧縮機と一体に回転する第1タービンとからなるガスタービン・エンジンと、
前記ガスタービン・エンジンの出力軸に接続されて電力を発電する発電機と、
前記発電機で発電された電力を蓄電するバッテリと、
前記バッテリと前記ロータの回転軸に接続され、前記バッテリから電力の供給を受けるとき前記ロータを駆動する一方、前記ロータで駆動されるとき電力を発電するモータ・ジェネレータと、
前記ガスタービン・エンジンと独立に、前記ナセルの内部に設けられ、前記ガスタービン・エンジンから出力される高圧ガスを供給されるとき前記ロータを駆動する第2タービンと、を備え、
前記第2タービンは、前記ナセルの内壁に形成された複数の静翼と、前記複数の静翼に対向して配置された複数の動翼と、を有するチップタービンからなり、
前記ナセルの内部には、前記第2タービンより上方に環状のダクトが形成され、
前記ダクトには、前記高圧ガスを抽気する抽気路と、前記複数の静翼に向けて下方に開口する複数の噴出口と、が設けられることを特徴とするハイブリッド飛行体。 - 前記ガスタービン・エンジンと前記第2タービンの間に熱交換器を配置したことを特徴とする請求項1に記載のハイブリッド飛行体。
- 前記ガスタービン・エンジンとモータ・ジェネレータの動作を検出する検出手段と、前記検出手段の出力に基づいて前記ガスタービン・エンジンとモータ・ジェネレータの動作を調整して飛行を制御する制御部とを備えたことを特徴とする請求項1または2に記載のハイブリッド飛行体。
- 前記制御部は、前記飛行が離着陸であるとき、前記モータ・ジェネレータを動作させることを特徴とする請求項3に記載のハイブリッド飛行体。
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2018214791A JP7049234B2 (ja) | 2018-11-15 | 2018-11-15 | ハイブリッド飛行体 |
US16/660,593 US11174035B2 (en) | 2018-11-15 | 2019-10-22 | Hybrid flight vehicle |
CN201911047276.4A CN111186584B (zh) | 2018-11-15 | 2019-10-30 | 混合动力飞行器 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2018214791A JP7049234B2 (ja) | 2018-11-15 | 2018-11-15 | ハイブリッド飛行体 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2020082755A JP2020082755A (ja) | 2020-06-04 |
JP7049234B2 true JP7049234B2 (ja) | 2022-04-06 |
Family
ID=70704502
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2018214791A Active JP7049234B2 (ja) | 2018-11-15 | 2018-11-15 | ハイブリッド飛行体 |
Country Status (3)
Country | Link |
---|---|
US (1) | US11174035B2 (ja) |
JP (1) | JP7049234B2 (ja) |
CN (1) | CN111186584B (ja) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10906637B2 (en) | 2018-05-17 | 2021-02-02 | Textron Innovations Inc. | Assisted landing systems for rotorcraft |
JP7021054B2 (ja) * | 2018-11-08 | 2022-02-16 | 本田技研工業株式会社 | ハイブリッド飛行体 |
US11891166B2 (en) * | 2019-04-12 | 2024-02-06 | The Boeing Company | Hybrid multirotor vehicles and related methods |
US11453488B2 (en) * | 2019-09-30 | 2022-09-27 | Rolls-Royce Corporation | Lightweight parallel combustion lift system for vertical takeoff aircraft |
US11753174B2 (en) * | 2020-05-19 | 2023-09-12 | Pratt & Whitney Canada Corp. | Systems and methods for aircraft wing plug |
CN113306726B (zh) * | 2021-07-01 | 2023-09-22 | 西北工业大学 | 一种高速共轴双旋翼直升机推进*** |
CN115258146B (zh) * | 2022-09-26 | 2023-02-03 | 江苏友诚数控科技有限公司 | 一种电动旋翼垂直起降由燃油动力驱动向前飞行的固定翼飞机 |
Citations (5)
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JP3912560B2 (ja) | 1997-10-02 | 2007-05-09 | 株式会社イノアックコーポレーション | エアバッグ内蔵ピラーガーニッシュ |
JP2013174242A (ja) | 2007-04-06 | 2013-09-05 | Turbomeca | ガス発生器およびフリータービンを備えるヘリコプタターボシャフトエンジン |
JP2016180336A (ja) | 2015-03-23 | 2016-10-13 | 三菱重工業株式会社 | 回転翼機 |
US20170225573A1 (en) | 2014-09-23 | 2017-08-10 | Sikorsky Aircraft Corporation | Hybrid electric power drive system for a rotorcraft |
JP6272619B2 (ja) | 2013-11-13 | 2018-01-31 | フラウンホーファー−ゲゼルシャフト・ツール・フェルデルング・デル・アンゲヴァンテン・フォルシュング・アインゲトラーゲネル・フェライン | オーディオ信号の符号化用エンコーダ、オーディオ伝送システムおよび補正値の判定方法 |
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US20190118943A1 (en) * | 2017-10-24 | 2019-04-25 | General Atomics Aeronautical Systems, Inc. | Tail-Sitter Aircraft With Hybrid Propulsion |
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JP7057264B2 (ja) * | 2018-11-02 | 2022-04-19 | 本田技研工業株式会社 | ハイブリッド飛行体 |
JP7021054B2 (ja) * | 2018-11-08 | 2022-02-16 | 本田技研工業株式会社 | ハイブリッド飛行体 |
-
2018
- 2018-11-15 JP JP2018214791A patent/JP7049234B2/ja active Active
-
2019
- 2019-10-22 US US16/660,593 patent/US11174035B2/en active Active
- 2019-10-30 CN CN201911047276.4A patent/CN111186584B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3912560B2 (ja) | 1997-10-02 | 2007-05-09 | 株式会社イノアックコーポレーション | エアバッグ内蔵ピラーガーニッシュ |
JP2013174242A (ja) | 2007-04-06 | 2013-09-05 | Turbomeca | ガス発生器およびフリータービンを備えるヘリコプタターボシャフトエンジン |
JP6272619B2 (ja) | 2013-11-13 | 2018-01-31 | フラウンホーファー−ゲゼルシャフト・ツール・フェルデルング・デル・アンゲヴァンテン・フォルシュング・アインゲトラーゲネル・フェライン | オーディオ信号の符号化用エンコーダ、オーディオ伝送システムおよび補正値の判定方法 |
US20170225573A1 (en) | 2014-09-23 | 2017-08-10 | Sikorsky Aircraft Corporation | Hybrid electric power drive system for a rotorcraft |
JP2016180336A (ja) | 2015-03-23 | 2016-10-13 | 三菱重工業株式会社 | 回転翼機 |
Also Published As
Publication number | Publication date |
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JP2020082755A (ja) | 2020-06-04 |
CN111186584A (zh) | 2020-05-22 |
US20200156801A1 (en) | 2020-05-21 |
US11174035B2 (en) | 2021-11-16 |
CN111186584B (zh) | 2023-04-14 |
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