JP4365688B2 - ディスエンゲージ装置 - Google Patents
ディスエンゲージ装置 Download PDFInfo
- Publication number
- JP4365688B2 JP4365688B2 JP2004013293A JP2004013293A JP4365688B2 JP 4365688 B2 JP4365688 B2 JP 4365688B2 JP 2004013293 A JP2004013293 A JP 2004013293A JP 2004013293 A JP2004013293 A JP 2004013293A JP 4365688 B2 JP4365688 B2 JP 4365688B2
- Authority
- JP
- Japan
- Prior art keywords
- rod
- push
- recess
- fitting
- disengagement
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Fee Related
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Classifications
-
- 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
- B64C13/24—Transmitting means
-
- 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)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
Description
村山大二郎著、「航空工学講座 第17巻 オートパイロット」、日本航空技術協会、昭和58年4月10日、p.83−84
2 操縦桿
3 サーボモータ(駆動装置)
6 プッシュプルロッド
10 第1ロッド
11 第1ロッドの一方の端部
12 第1ロッドの他方の端部
13 中空部
20 第2ロッド
21 第2ロッドの一方の端部
22 第2ロッドの他方の端部
23 凹部
30 枝管
32 ネジ(付勢力調整手段)
40 球状体(嵌合部材)
50 弾性体
60 プッシュプルケーブル(嵌合解除手段)
70 ディスエンゲージレバー(嵌合解除手段)
80 エンゲージ表示ランプ(エンゲージ状態報知手段)
Claims (6)
- 操縦桿及び操縦舵面と、前記操縦舵面を駆動する駆動装置と、前記駆動装置の駆動力又は前記操縦桿を介して伝達された操作入力を前記操縦舵面に伝達するプッシュプルロッドと、を有する航空機に搭載され、前記駆動装置の駆動力が前記操縦舵面に伝達されることを阻止するディスエンゲージ装置であって、
一方の端部が前記駆動装置に接続され、他方の端部で開口した所定長の中空部が形成されてなる第1ロッドと、
この第1ロッドの前記中空部の側壁に連接されて前記中空部に連通する枝管と、
一方の端部が前記プッシュプルロッドに接続され、他方の端部から一方の端部側に延在する所定長の部分が前記第1ロッドの前記中空部に挿入され、この挿入される部分の側壁の一部に凹部が形成されてなる第2ロッドと、
前記枝管内に移動自在に配置されるとともに前記凹部に嵌合する嵌合部材と、
を備えることを特徴とするディスエンゲージ装置。 - 前記嵌合部材を前記凹部に押し付ける付勢力を発生させて前記嵌合部材と前記凹部との嵌合状態を維持させる弾性体と、
この弾性体の付勢力を低減させて前記嵌合部材と前記凹部との嵌合状態を解除する嵌合解除手段と、
を備えることを特徴とする請求項1に記載のディスエンゲージ装置。 - 前記弾性体の付勢力を調整する付勢力調整手段を備えることを特徴とする請求項2に記載のディスエンゲージ装置。
- 前記嵌合解除手段は、
前記弾性体に接続されたプッシュプルケーブルと、
操作されることにより前記プッシュプルケーブルに所定の張力を加えて前記弾性体の付勢力を低減させるディスエンゲージレバーと、
から構成されることを特徴とする請求項2又は3に記載のディスエンゲージ装置。 - 前記嵌合部材は、
球状体であることを特徴とする請求項1から4の何れか一項に記載のディスエンゲージ装置。 - 前記第1ロッドと前記第2ロッドとがエンゲージ状態にあるか否かを報知するエンゲージ状態報知手段を備えることを特徴とする請求項1から5の何れか一項に記載のディスエンゲージ装置。
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2004013293A JP4365688B2 (ja) | 2004-01-21 | 2004-01-21 | ディスエンゲージ装置 |
US11/038,725 US7316373B2 (en) | 2004-01-21 | 2005-01-19 | Disengage device for aircraft control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2004013293A JP4365688B2 (ja) | 2004-01-21 | 2004-01-21 | ディスエンゲージ装置 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2005205989A JP2005205989A (ja) | 2005-08-04 |
JP4365688B2 true JP4365688B2 (ja) | 2009-11-18 |
Family
ID=34835803
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2004013293A Expired - Fee Related JP4365688B2 (ja) | 2004-01-21 | 2004-01-21 | ディスエンゲージ装置 |
Country Status (2)
Country | Link |
---|---|
US (1) | US7316373B2 (ja) |
JP (1) | JP4365688B2 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102504025B1 (ko) * | 2022-08-29 | 2023-02-27 | 주식회사 비거텍코리아 | 항공기용 트림탭 작동장치 |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7837143B2 (en) * | 2005-03-14 | 2010-11-23 | Matos Jeffrey A | Method and apparatus for disabling pilot control of a hijacked aircraft |
JP5411661B2 (ja) * | 2009-11-12 | 2014-02-12 | 富士重工業株式会社 | ディスエンゲージ装置 |
CN103596843B (zh) | 2010-10-18 | 2017-04-26 | 本田专利技术北美有限责任公司 | 用于飞机起落架的快速释放组件 |
WO2012068136A2 (en) * | 2010-11-15 | 2012-05-24 | Lam Aviation, Inc. | Mechanical control mixer and method therefor |
US9403591B2 (en) * | 2013-07-23 | 2016-08-02 | Mason Electric Co. | Landing gear control system |
KR102548773B1 (ko) * | 2023-02-17 | 2023-06-28 | 주식회사 비거텍코리아 | 추력 편향 조종장치를 구비한 비행체 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5042749A (en) * | 1990-04-10 | 1991-08-27 | Sundstrand Corporation | Mechanism for limiting rotation of a rotatably mounted shaft |
FR2737698B1 (fr) * | 1995-08-08 | 1997-10-24 | Aerospatiale | Systeme pour commander une gouverne articulee sur une structure d'un vehicule |
-
2004
- 2004-01-21 JP JP2004013293A patent/JP4365688B2/ja not_active Expired - Fee Related
-
2005
- 2005-01-19 US US11/038,725 patent/US7316373B2/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102504025B1 (ko) * | 2022-08-29 | 2023-02-27 | 주식회사 비거텍코리아 | 항공기용 트림탭 작동장치 |
Also Published As
Publication number | Publication date |
---|---|
JP2005205989A (ja) | 2005-08-04 |
US7316373B2 (en) | 2008-01-08 |
US20050178926A1 (en) | 2005-08-18 |
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