JP6813302B2 - 回転翼機操縦装置およびかかる回転翼機操縦装置を備えた回転翼機 - Google Patents
回転翼機操縦装置およびかかる回転翼機操縦装置を備えた回転翼機 Download PDFInfo
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- JP6813302B2 JP6813302B2 JP2016159501A JP2016159501A JP6813302B2 JP 6813302 B2 JP6813302 B2 JP 6813302B2 JP 2016159501 A JP2016159501 A JP 2016159501A JP 2016159501 A JP2016159501 A JP 2016159501A JP 6813302 B2 JP6813302 B2 JP 6813302B2
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- 230000015654 memory Effects 0.000 claims description 49
- 210000000078 claw Anatomy 0.000 claims description 29
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- 238000000034 method Methods 0.000 description 17
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- 230000007704 transition Effects 0.000 description 7
- 230000007935 neutral effect Effects 0.000 description 5
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- 230000001174 ascending effect Effects 0.000 description 2
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
- B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
-
- 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
- B64D31/02—Initiating means
- B64D31/04—Initiating means actuated personally
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
- G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
- G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
- G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
- G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
- G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
- G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks
- G05G2009/04774—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks with additional switches or sensors on the handle
-
- 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
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Control Devices (AREA)
- User Interface Of Digital Computer (AREA)
Description
124 プロセッサ
126 メモリ
1012 プロセッサ
1013 ローカル・メモリ
1014 揮発性メモリ
1016 不揮発性メモリ
1020 インタフェース
1022 入力装置(複数可)
1024 出力装置(複数可)
1026 ネットワーク
1028 大容量記憶部
1032 符号化された命令
Claims (8)
- 第1の入力を提供するための第1の方向および第2の入力を提供するための前記第1の方向に対向する第2の方向に回転可能な回転インタフェースを含む、航空機に対するコレクティブ操縦桿と、
命令を格納するためのメモリと、
前記第1の入力に応答して、前記航空機を飛行させることに関連付けられた動作を前記航空機に実施させる前記命令を実行し、前記第2の入力に応答して、前記航空機をアイドリングさせることに関連付けられた動作を前記航空機に実施させる前記命令を実行する、プロセッサと、
を備え、
前記回転インタフェースは前記コレクティブ操縦桿を少なくとも部分的に囲むカラーを含み、
前記カラーは、前記コレクティブ操縦桿のグリップの先細り面と係合するようにバイアスされるフォロワを含む、装置。 - 前記カラーは、前記コレクティブ操縦桿の縦軸に対する前記カラーの回転位置を示すための前記カラーの外面上の表面構造を含む、請求項1に記載の装置。
- 前記カラーは、縦方向に、回転して、前記第1の入力に関連付けられた前記カラーの第1の位置および前記第2の入力に関連付けられた前記カラーの第2の位置の間の中心位置にバイアスされる、請求項1に記載の装置。
- 前記中心位置において、前記フォロワは偶然の回転に対して前記カラーを十分に保護するための爪で受けられる、請求項3に記載の装置。
- 前記カラーは、前記フォロワを前記爪から取り外し、前記カラーを前記第1の方向または前記第2の方向の何れかに回転可能とするように、前記コレクティブ操縦桿の縦軸に対して移動可能である、請求項4に記載の装置。
- 前記コレクティブ操縦桿はグリップおよびヘッドを含み、前記回転インタフェースは前記グリップおよび前記ヘッドの間に配置される、請求項1に記載の装置。
- 前記第1の方向への前記回転インタフェースの回転または前記第2の方向への前記回転インタフェースの回転に応答するスイッチをさらに備え、前記スイッチは、前記プロセッサが前記第1の入力または前記第2の入力を受信できるように前記プロセッサに接続される、請求項1に記載の装置。
- 前記第1の方向への前記回転インタフェースの回転または前記第2の方向への前記回転入力の回転に応答するスイッチをさらに備え、前記スイッチは、前記プロセッサが前記第1の入力または前記第2の入力を受信できるように前記プロセッサに接続される、請求項1に記載の装置。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/921,878 | 2015-10-23 | ||
US14/921,878 US10035583B2 (en) | 2015-10-23 | 2015-10-23 | Rotorcraft controls and rotorcraft including such rotorcraft controls |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2017081528A JP2017081528A (ja) | 2017-05-18 |
JP6813302B2 true JP6813302B2 (ja) | 2021-01-13 |
Family
ID=56740158
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2016159501A Active JP6813302B2 (ja) | 2015-10-23 | 2016-08-16 | 回転翼機操縦装置およびかかる回転翼機操縦装置を備えた回転翼機 |
Country Status (5)
Country | Link |
---|---|
US (1) | US10035583B2 (ja) |
EP (1) | EP3159261B1 (ja) |
JP (1) | JP6813302B2 (ja) |
CN (1) | CN107031833B (ja) |
ES (1) | ES2764450T3 (ja) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2997569C (en) * | 2017-03-06 | 2020-09-01 | Bell Helicopter Textron Inc. | Collective control stick mounted throttle control assembly |
US10011348B1 (en) | 2017-05-02 | 2018-07-03 | Kitty Hawk Corporation | Vertical thrust lever |
US10870482B2 (en) * | 2018-04-13 | 2020-12-22 | Hamilton Sunstrand Corporation | Aircraft control selector levers |
KR20210039455A (ko) * | 2018-08-30 | 2021-04-09 | 에섹스 인더스트리스, 아이엔씨. | 회전익기용 콜렉티브 제어 시스템 |
WO2020046436A1 (en) * | 2018-08-30 | 2020-03-05 | Essex Industries, Inc. | Collective control system for a rotorcraft |
USD897929S1 (en) | 2018-11-29 | 2020-10-06 | Essex Industries, Inc. | Controller for rotorcraft |
US10591948B1 (en) * | 2018-08-30 | 2020-03-17 | Essex Industries, Inc. | Collective control system for a rotorcraft |
US11623736B2 (en) * | 2020-07-29 | 2023-04-11 | Textron Innovations Inc. | Collective control stick mounted throttle control assembly |
US11828043B2 (en) * | 2020-12-21 | 2023-11-28 | Caterpillar Inc. | Manual input device and method |
CN113277067B (zh) * | 2021-05-26 | 2022-11-01 | 贵州华阳电工有限公司 | 减速板手柄可调节操纵力机械结构 |
CN114056549B (zh) * | 2021-11-01 | 2024-05-10 | 中国商用飞机有限责任公司 | 侧杆装置、侧杆控制器、侧杆控制方法和飞行器 |
US11919622B1 (en) * | 2022-08-22 | 2024-03-05 | BETA Technologies, Inc. | Cockpit assembly and a method for adjusting a cockpit |
Family Cites Families (14)
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US4130259A (en) * | 1977-08-10 | 1978-12-19 | Textron Inc. | Helicopter collective lever |
US4667909A (en) * | 1985-10-10 | 1987-05-26 | Alfred Curci | Single-stick control system for helicopters |
FR2713592B1 (fr) * | 1993-12-13 | 1996-03-01 | Sextant Avionique | Dispositif pour la commande des manettes de gaz contrôlant deux moteurs d'un même aérodyne. |
US5403155A (en) | 1993-12-17 | 1995-04-04 | Mcdonnell Douglas Helicopter Company | Power management for a turbine powered helicopter |
US5472156A (en) | 1994-03-28 | 1995-12-05 | The United States Of America As Represented By The Secretary Of The Army | Air combat collective control head |
WO2001087706A1 (en) * | 2000-05-16 | 2001-11-22 | Bell Helicopter Textron Inc. | Multi-mode tiltrotor nacelle control system with integrated envelope protection |
US8973863B1 (en) | 2010-09-09 | 2015-03-10 | Groen Brothers Aviation, Inc. | Blade root attachment apparatus and method |
FR2986572B1 (fr) * | 2012-02-07 | 2016-04-29 | Eurocopter France | Procede automatique de regulation d'un groupe de motorisation d'aeronef, dispositif et aeronef |
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US9056675B2 (en) * | 2012-02-10 | 2015-06-16 | Bell Helicopter Textron Inc. | Pilot control system with hand rest |
FR3005934B1 (fr) * | 2013-05-23 | 2015-05-01 | Airbus Operations Sas | Systeme et procede de commande d’un aeronef |
US9096325B2 (en) * | 2013-11-18 | 2015-08-04 | Bell Helicopter Textron Inc. | Fly-by-wire engine power control system |
JP6267945B2 (ja) * | 2013-11-25 | 2018-01-24 | 三菱航空機株式会社 | 航空機のエンジン制御コンピュータ、および航空機 |
US9500138B1 (en) * | 2015-08-17 | 2016-11-22 | United Technologies Corporation | Twin-engine rotorcrafts and load power sharing control systems thereof and methods for load power sharing control |
-
2015
- 2015-10-23 US US14/921,878 patent/US10035583B2/en active Active
-
2016
- 2016-08-16 JP JP2016159501A patent/JP6813302B2/ja active Active
- 2016-08-19 ES ES16184909T patent/ES2764450T3/es active Active
- 2016-08-19 EP EP16184909.6A patent/EP3159261B1/en active Active
- 2016-10-24 CN CN201610939113.7A patent/CN107031833B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
ES2764450T3 (es) | 2020-06-03 |
EP3159261B1 (en) | 2019-10-16 |
US20170113783A1 (en) | 2017-04-27 |
JP2017081528A (ja) | 2017-05-18 |
US10035583B2 (en) | 2018-07-31 |
EP3159261A1 (en) | 2017-04-26 |
CN107031833A (zh) | 2017-08-11 |
CN107031833B (zh) | 2019-09-17 |
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