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MIL H 8775D 飞机和导弹液压系统部件通用规范 (1976年6月11日) [S SEA AS8775]

ID：52200

大小：1.20 MB

页数：33页

时间：2023-03-23

金币：20

上传者：战必胜
.—.
MIL-H-8775D
11 June 1976
SUPERSEDING
MIL-H-8’775C
8 January 1964
MILITARY SPECIFICATION
HYDRAULIC SYSTEM COMPONENTS, AfRCRA~ AND
1.
SCOPE
1.1
MISSILES, GENERAL SPECIFICATION FOR
This speci5cation is approved for use by all Depart-
ments and Agenciee of the Department of Defemee.
Scope - This specification covers the general requirements
that are common to m=ydraulic ‘components (see 6.2), used in aeronautical
hydraulic systeme (see 6. 1).
1.2
Classification - Aircraft hydraulic systems in which com-
ponents covered by this specification are to be used shall be of the followtng
+.
types, as specified:
Type I
-65° to +160n F fluid temperature range
TYW II
-65” bJ +275” F fluid temperature range
2.
APPLICABLE DOCUMENTS
2.1
The following documents of the issue la effect on date of
invitation for bids or request fcr proposal, form a part of the apeciflcation to
the extent specified herein.
SPECIFICATIONS
Federal
QQ-C-320
QQ-N-290
QQ-P-416
Chromium Plating (Eleotrodeposited)
Nickel Plstlng (EIectrodewsited)
Plating, Cadmium (Eleotmdepoeited)
L
●
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