JPH03118897U - - Google Patents

Info

Publication number
JPH03118897U
JPH03118897U JP2621290U JP2621290U JPH03118897U JP H03118897 U JPH03118897 U JP H03118897U JP 2621290 U JP2621290 U JP 2621290U JP 2621290 U JP2621290 U JP 2621290U JP H03118897 U JPH03118897 U JP H03118897U
Authority
JP
Japan
Prior art keywords
wingtip
main wing
wing body
wings
aircraft
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.)
Pending
Application number
JP2621290U
Other languages
Japanese (ja)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP2621290U priority Critical patent/JPH03118897U/ja
Publication of JPH03118897U publication Critical patent/JPH03118897U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Transmission Devices (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

第１図ａは本考案の第１実施例の平面図、同図
ｂは同実施例の後面図、第２図ａは本考案の第２
実施例の平面図、同図ｂは同実施例の後面図、第
３図は上記実施例に共通の作動フロー図、第４図
ａは従来の航空機の一例の平面図、同図ｂは同例
の後面図、第５図ａは従来の航空機の他の例の平
面図、同図ｂは同例の後面図である。 １……翼端翼、２……アクチユエータ、３……
油圧装置、４……ケーブル、５……コンピユータ
、６……ケーブル、７……パイロツトステイツク
、８……主翼本体、９……胴体、１０……高揚力
装置、１１……水平尾翼、１２……垂直尾翼、１
３……横揺れモーメント、１４……翼端翼、１４
ａ……ヒンジ、１５……方向舵、１６……エルロ
ン、２１Ａ，２１Ｂ……偏揺れモーメント、２２
……スポイラ。 Fig. 1a is a plan view of the first embodiment of the present invention, Fig. 1b is a rear view of the same embodiment, and Fig. 2a is the second embodiment of the invention.
FIG. 3 is an operational flow diagram common to the above-mentioned embodiments; FIG. 4a is a plan view of an example of a conventional aircraft; FIG. FIG. 5a is a plan view of another example of a conventional aircraft, and FIG. 5b is a rear view of the same example. 1... Wing tip wing, 2... Actuator, 3...
Hydraulic system, 4... Cable, 5... Computer, 6... Cable, 7... Pilot station, 8... Main wing body, 9... Fuselage, 10... High lift device, 11... Horizontal stabilizer, 12 ...Vertical tail, 1
3... Rolling moment, 14... Wing tip wing, 14
a...Hinge, 15...Rudder, 16...Aileron, 21A, 21B...Yaw moment, 22
...Spoiler.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 主翼本体の両端部にそれぞれ装着された張出し
引込み可能な翼端翼、およびパイロツトの操作に
応じて同翼端翼を移動させ主翼本体外部への露出
面積を変更する制御装置を備えたことを特徴とす
る航空機の横操縦装置。 It is characterized by being equipped with extensible and retractable wingtip wings attached to both ends of the main wing body, and a control device that moves the wingtip wings in response to pilot operations to change the area exposed to the outside of the main wing body. side control system for aircraft.
JP2621290U 1990-03-16 1990-03-16 Pending JPH03118897U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2621290U JPH03118897U (en) 1990-03-16 1990-03-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2621290U JPH03118897U (en) 1990-03-16 1990-03-16

Publications (1)

Publication Number Publication Date
JPH03118897U true JPH03118897U (en) 1991-12-09

Family

ID=31529118

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2621290U Pending JPH03118897U (en) 1990-03-16 1990-03-16

Country Status (1)

Country Link
JP (1) JPH03118897U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101825069A (en) * 2010-06-04 2010-09-08 西安交通大学 Blade folding structure for wind driven generator
JP2011518712A (en) * 2008-04-23 2011-06-30 エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング Aircraft wing
JP2014004993A (en) * 2012-06-21 2014-01-16 Boeing Co Swing tip assembly rotation joint
JP2015074444A (en) * 2013-10-06 2015-04-20 ザ・ボーイング・カンパニーＴｈｅＢｏｅｉｎｇ Ｃｏｍｐａｎｙ Swing wing tip system, assembly and method with dual load path structure

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH024199A (en) * 1988-06-23 1990-01-09 Mitsubishi Heavy Ind Ltd Steering device for missile

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH024199A (en) * 1988-06-23 1990-01-09 Mitsubishi Heavy Ind Ltd Steering device for missile

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011518712A (en) * 2008-04-23 2011-06-30 エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング Aircraft wing
CN101825069A (en) * 2010-06-04 2010-09-08 西安交通大学 Blade folding structure for wind driven generator
JP2014004993A (en) * 2012-06-21 2014-01-16 Boeing Co Swing tip assembly rotation joint
JP2015074444A (en) * 2013-10-06 2015-04-20 ザ・ボーイング・カンパニーＴｈｅＢｏｅｉｎｇ Ｃｏｍｐａｎｙ Swing wing tip system, assembly and method with dual load path structure

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