JPH0429498U - - Google Patents

Info

Publication number
JPH0429498U
JPH0429498U JP7063290U JP7063290U JPH0429498U JP H0429498 U JPH0429498 U JP H0429498U JP 7063290 U JP7063290 U JP 7063290U JP 7063290 U JP7063290 U JP 7063290U JP H0429498 U JPH0429498 U JP H0429498U
Authority
JP
Japan
Prior art keywords
aircraft
intervals
pylon
pylon mounting
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.)
Granted
Application number
JP7063290U
Other languages
Japanese (ja)
Other versions
JP2542744Y2 (en
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 JP1990070632U priority Critical patent/JP2542744Y2/en
Publication of JPH0429498U publication Critical patent/JPH0429498U/ja
Application granted granted Critical
Publication of JP2542744Y2 publication Critical patent/JP2542744Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tents Or Canopies (AREA)

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の説明図、第２図は
従来のパイロンの搭載装置の説明図である。 １……前方内側のハードポイント、２……前方
外側のハードポイント、３……後方のハードポイ
ント、４……追加されたハードポイント、５……
主翼。 FIG. 1 is an explanatory diagram of an embodiment of the present invention, and FIG. 2 is an explanatory diagram of a conventional pylon mounting device. 1... Front inside hard point, 2... Front outside hard point, 3... Rear hard point, 4... Added hard point, 5...
Main wing.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ほゞ機軸方向に間隔をおいて機体に設けられパ
イロンを取付ける前方及び後方のハードポイント
により形成されるステーシヨンを複数個互いに間
隔をおいて横方向に並設した航空機のパイロンの
搭載装置において、隣接するステーシヨンの中間
において機体にハードポイントを追加して設けた
ことを特徴とする航空機のパイロンの搭載装置。 In an aircraft pylon mounting system, a plurality of stations formed by front and rear hard points, which are provided on the fuselage at intervals in the axial direction and are attached to the pylon, are arranged in parallel in the lateral direction at intervals from each other. An aircraft pylon mounting device characterized by having an additional hard point on the aircraft body in the middle of the station.
JP1990070632U 1990-07-04 1990-07-04 Aircraft pylon mounted equipment Expired - Lifetime JP2542744Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1990070632U JP2542744Y2 (en) 1990-07-04 1990-07-04 Aircraft pylon mounted equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1990070632U JP2542744Y2 (en) 1990-07-04 1990-07-04 Aircraft pylon mounted equipment

Publications (2)

Publication Number Publication Date
JPH0429498U true JPH0429498U (en) 1992-03-10
JP2542744Y2 JP2542744Y2 (en) 1997-07-30

Family

ID=31606951

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1990070632U Expired - Lifetime JP2542744Y2 (en) 1990-07-04 1990-07-04 Aircraft pylon mounted equipment

Country Status (1)

Country Link
JP (1) JP2542744Y2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018520038A (en) * 2015-06-03 2018-07-26 エックス デベロップメント エルエルシー Hard point strain relief

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018520038A (en) * 2015-06-03 2018-07-26 エックス デベロップメント エルエルシー Hard point strain relief

Also Published As

Publication number Publication date
JP2542744Y2 (en) 1997-07-30

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Legal Events

Date Code Title Description
EXPY Cancellation because of completion of term