JPS6321861U - - Google Patents

Info

Publication number
JPS6321861U
JPS6321861U JP11551786U JP11551786U JPS6321861U JP S6321861 U JPS6321861 U JP S6321861U JP 11551786 U JP11551786 U JP 11551786U JP 11551786 U JP11551786 U JP 11551786U JP S6321861 U JPS6321861 U JP S6321861U
Authority
JP
Japan
Prior art keywords
support member
static pressure
pressure tube
tip
fuselage
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
JP11551786U
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 JP11551786U priority Critical patent/JPS6321861U/ja
Publication of JPS6321861U publication Critical patent/JPS6321861U/ja
Pending legal-status Critical Current

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Description

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

第1図は本考案の一実施例としての二重枢着式
ピトー静圧管装置の一部を破断して示す模式的な
側面図であり、第2図は従来の二重枢着式ピトー
静圧管装置の一部を破断して示す模式的な側面図
である。 1……ピトー静圧管、1a……円錐部、2a…
…第1のスウイベル部、2b…第2のスウイベル
部、3a…第1の支持部材、3b…第2の支持部
材、4…機体。
FIG. 1 is a schematic side view, partially cut away, of a double pivot type pitot static pressure tube device as an embodiment of the present invention, and FIG. 2 is a conventional double pivot type pitot static pressure tube device. It is a typical side view which breaks and shows a part of pressure pipe apparatus. 1... Pitot static pressure tube, 1a... Conical part, 2a...
...first swivel part, 2b...second swivel part, 3a...first support member, 3b...second support member, 4...body.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 機体の先端部に支持部材を介して装着されたピ
トー静圧管をそなえ、上記支持部材が、上記機体
の先端部に固定された第1の支持部材と、同第1
の支持部材の先端部に第1のスウイベル部を介し
回転制御可能に枢着された第2の支持部材とで構
成されて、同第2の支持部材の先端に上記ピトー
静圧管が第2のスウイベル部を介し回転制御可能
に枢着されたことを特徴とする、二重枢着式ピト
ー静圧管装置。
A pitot static pressure tube is attached to the tip of the fuselage via a support member, and the support member is connected to a first support member fixed to the tip of the fuselage, and the first support member is fixed to the tip of the fuselage.
and a second support member pivotally connected to the distal end of the support member via a first swivel portion so as to be rotationally controllable, and the pitot static pressure tube is connected to the distal end of the second support member. A double pivot type pitot static pressure tube device, characterized in that it is pivotally connected through a swivel portion so that rotation can be controlled.
JP11551786U 1986-07-28 1986-07-28 Pending JPS6321861U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11551786U JPS6321861U (en) 1986-07-28 1986-07-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11551786U JPS6321861U (en) 1986-07-28 1986-07-28

Publications (1)

Publication Number Publication Date
JPS6321861U true JPS6321861U (en) 1988-02-13

Family

ID=30999243

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11551786U Pending JPS6321861U (en) 1986-07-28 1986-07-28

Country Status (1)

Country Link
JP (1) JPS6321861U (en)

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