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Viewing 17761 to 17790 of 19490
1956-04-06
Standard
AS6372-2
No scope available.
1956-04-06
Standard
AS6373-2
No scope available.
1956-04-06
Standard
AS6367-3
No scope available.
1956-04-06
Standard
AS6374-2
No scope available.
1956-04-06
Standard
AS6369-3
No scope available.
1956-04-06
Standard
AS6368-3
No scope available.
1956-04-06
Standard
AS6370-3
No scope available.
1956-02-13
Standard
RS438-2
No scope available.
1956-02-13
Standard
AS6261-1
No scope available.
1956-02-13
Standard
AS6262-1
No scope available.
1956-02-13
Standard
AS6609-1
No scope available.
1956-02-13
Standard
AS4648-2
No scope available.
1956-02-13
Standard
AS4646-2
No scope available.
1956-02-13
Standard
AS4647-2
No scope available.
1956-02-13
Standard
AS4645-2
No scope available.
1956-02-13
Standard
AS6384-2
No scope available.
1956-01-19
Standard
AS6330-1
No scope available.
1956-01-01
Technical Paper
560167
J. B. STEVENS
DIGEST A description of the application of Axial Face Seals to Aircraft Gas Turbine Main Shaft Bearings, Gear Boxes or Accessory Pads and Accessories; their limitations with respect to sealing media, temperatures, pressures and rubbing surface speeds; the influence of these factors on the selection of materials of construction. A statement of the current status of the art and projected future requirements.
1956-01-01
Technical Paper
560168
RICHARD V. BLAIR
The Controlled Gap Seal consists of a carbon sealing ring with a steel retaining ring shrink fitted on the outside diameter, two steel mating rings, a spacer ring, and an outer shell. In operation under ideal conditions there is a pressure differential across the seal with the air side pressure being higher than the oil side. This differential prevents oil leakage and holds the carbon sealing ring against the oil side mating ring while the shaft turns freely within the sealing ring. The Controlled Gap Seal will operate with unlimited axial movement, is of rugged construction and will give long life and very low heat generation. It is good for high temperature operation since there are no rubber or plastic materials used.
1956-01-01
Technical Paper
560169
J. W. PENNINGTON, T. C. KUCHLER, E. J. TASCHENBERG
1956-01-01
Technical Paper
560171
JOSEPH PALSULICH, R. H. RIEDEL
This paper describes some of the problems encountered in sealing various media in aircraft gas turbine engine main shaft and accessory drive applications. The major types of seals are illustrated, and the individual design and operating limits of each are discussed. The seal performance requirements for the present and near future gas turbine engines are indicated. An evaluation program directed towards the development of a seal materials combination which will be compatible for extremely high speed and high temperature operation is described and some tests results enumerated. The equipment used for testing of materials and complete seal assemblies is described and pictured.
1956-01-01
Technical Paper
560307
R. C. GRASBY
1956-01-01
Technical Paper
560249
E. J. Eckert
1955-12-01
Standard
AS6256-2
No scope available.
1955-12-01
Standard
AS6258-1
No scope available.
1955-12-01
Standard
AS6257-2
No scope available.
1955-12-01
Standard
AS6260-3
No scope available.
1955-12-01
Standard
AS6259-1
No scope available.
1955-12-01
Standard
AS6348-1
No scope available.
1955-12-01
Standard
AS6351-1
No scope available.
Viewing 17761 to 17790 of 19490

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