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公开(公告)号:US10577979B2
公开(公告)日:2020-03-03
申请号:US15958527
申请日:2018-04-20
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Todd A. Davis , Mark Ronski , David Allen Stachowiak
Abstract: An oil tank mounting system for use on a structure of a turbine engine, includes three mounts with each mount configured to constrain the oil tank with a different number of degrees of freedom of movement. A first mount may have fix the oil tank in one degree of freedom, a second mount may fix the oil tank in two degrees of freedom, and a third mount may fix the oil tank in three degrees of freedom. This allows limited rotational and expansion movement while coupling the oil tank to the engine. The mount attachments may be embodied in rubber, with pins, or with spherical joints in a variety of configurations. Frangible pins may be used to absorb energy but still retain the oil tank in the event of a high energy event.
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公开(公告)号:US10514107B2
公开(公告)日:2019-12-24
申请号:US15620180
申请日:2017-06-12
Applicant: United Technologies Corporation
Inventor: David Allen Stachowiak
Abstract: An oil tank for a gas turbine engine includes a top and a bottom disposed vertically beneath the top. An overfill return passage extends from the bottom of the oil tank toward the top of the oil tank. An outlet is formed on the bottom of the oil tank and inside the overfill return passage. A check valve is inside the overfill return passage and is connected to the outlet. The check valve includes a seat circumscribing the outlet and a plug inside the overfill return passage. The plug has a lower density than an oil disposed inside the oil tank. The check valve does not include a spring such that the plug is configured to translate freely inside the overfill return passage.
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公开(公告)号:US20180355987A1
公开(公告)日:2018-12-13
申请号:US15620180
申请日:2017-06-12
Applicant: United Technologies Corporation
Inventor: David Allen Stachowiak
CPC classification number: F16K17/20 , F01D25/18 , F01M11/04 , F05D2260/98 , F16K15/021 , F16K15/044 , F16K31/20 , F16N7/00 , F16N19/00 , F16N23/00 , F16N2210/02 , F16N2210/08 , F16N2280/00 , G05D9/02
Abstract: An oil tank for a gas turbine engine includes a top and a bottom disposed vertically beneath the top. An overfill return passage extends from the bottom of the oil tank toward the top of the oil tank. An outlet is formed on the bottom of the oil tank and inside the overfill return passage. A check valve is inside the overfill return passage and is connected to the outlet. The check valve includes a seat circumscribing the outlet and a plug inside the overfill return passage. The plug has a lower density than an oil disposed inside the oil tank. The check valve does not include a spring such that the plug is configured to translate freely inside the overfill return passage.
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