JPS61186838U - - Google Patents

Info

Publication number
JPS61186838U
JPS61186838U JP7046485U JP7046485U JPS61186838U JP S61186838 U JPS61186838 U JP S61186838U JP 7046485 U JP7046485 U JP 7046485U JP 7046485 U JP7046485 U JP 7046485U JP S61186838 U JPS61186838 U JP S61186838U
Authority
JP
Japan
Prior art keywords
stator
rotor
brake structure
held
aircraft brake
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
JP7046485U
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 JP7046485U priority Critical patent/JPS61186838U/ja
Publication of JPS61186838U publication Critical patent/JPS61186838U/ja
Pending legal-status Critical Current

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  • Braking Arrangements (AREA)

Description

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

第1図は本考案に係る航空機用ブレーキ構造を
示す部分断面図、第2図は摩擦トルクと面圧の関
係を示す図、第3図は従来の航空機用ブレーキ構
造を示す部分断面図である。 1…ロータ、2…ステータ、3…プレツシヤプ
レート、4…キヤリア、4a…ピストン、5…ト
ルクチユーブ、6…バツキングプレート、R…有
効摩擦摺動半径。
FIG. 1 is a partial sectional view showing an aircraft brake structure according to the present invention, FIG. 2 is a diagram showing the relationship between friction torque and surface pressure, and FIG. 3 is a partial sectional view showing a conventional aircraft brake structure. . 1... Rotor, 2... Stator, 3... Pressure plate, 4... Carrier, 4a... Piston, 5... Torque tube, 6... Backing plate, R... Effective friction sliding radius.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 車輪側に保持されたロータを機体側に保持され
たステータで挾圧し車輪側の回転を阻止するよう
に形成されてなる航空機用ブレーキ構造において
、ロータあるいはステータのいずれか一方はその
内周側摺接面が欠落され、有効摩擦摺動半径が増
大されるように形成されてなることを特徴とする
航空機用ブレーキ構造。
In an aircraft brake structure in which a rotor held on the wheel side is clamped by a stator held on the aircraft body side to prevent rotation of the wheel side, either the rotor or the stator has a sliding surface on its inner peripheral side. 1. An aircraft brake structure, characterized in that the contact surface is omitted and the effective frictional sliding radius is increased.
JP7046485U 1985-05-13 1985-05-13 Pending JPS61186838U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7046485U JPS61186838U (en) 1985-05-13 1985-05-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7046485U JPS61186838U (en) 1985-05-13 1985-05-13

Publications (1)

Publication Number Publication Date
JPS61186838U true JPS61186838U (en) 1986-11-21

Family

ID=30607066

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7046485U Pending JPS61186838U (en) 1985-05-13 1985-05-13

Country Status (1)

Country Link
JP (1) JPS61186838U (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS604634A (en) * 1983-06-22 1985-01-11 Hitachi Ltd Construction of disc brake

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS604634A (en) * 1983-06-22 1985-01-11 Hitachi Ltd Construction of disc brake

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