Oil level sensor guide
11346701 · 2022-05-31
Assignee
Inventors
- Hung Duong (Unionville, CT, US)
- Wesley P. Long (Glastonbury, CT, US)
- Jonathan Zimmitti (Glastonbury, CT, US)
- David A. Stachowiak (Manchester, CT, US)
- Lakshminarayan S. Bettagere (Farmington, CT, US)
- Brian V. Abedon (West Hartford, CT, US)
Cpc classification
G01F23/00
PHYSICS
F05D2220/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D21/003
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
G01F23/00
PHYSICS
F01D21/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A fluid tank system comprises a fluid container that includes a sensor opening in a fluid container wall defined by a rim, and a fluid level sensor comprising a radial flange on a proximate end of a longitudinally extending electronics stem that includes a distal end. The distal end of the electronic stem is inserted into the fluid container via the sensor opening and the radial flange seats on the rim. The distal end of the electronics stem is guided via a first radial support and a second radial support to a seat that is located coaxial with the sensor opening, where the first and second radial supports are longitudinally separated and radially spaced apart to allow the electronics stem to longitudinally pass between the first and second radial supports until the flange seats on the rim ensuring that the distal end of the electronic stem is longitudinally positioned adjacent to the seat.
Claims
1. A fluid tank system, comprising: a fluid container that includes a sensor opening in a fluid container wall defined by a rim; a fluid level sensor comprising a radial flange on a proximate end of a longitudinally extending electronics stem that includes a distal end; a guide tube that radially surrounds the longitudinally extending electronics stem and axially contacts a flanged surface of the longitudinally extending electronics stem located within the fluid container, where the longitudinally extending electronics stem, the guide tube and the sensor opening are co-axial about a central axis, the guide tube comprising an inner radial surface which defines a sensor cavity and an outer radial surface, the outer radial surface and the fluid container defining a fluid cavity therebetween, the guide tube further comprising at least one fluid leak hole extending through the guide tube from the outer radial surface to the inner radial surface; wherein the fluid container comprises a first end having the sensor opening and a second end opposite the first end and wherein the guide tube extends from the sensor opening to the second end of the fluid container and contacts the second end of the fluid container; and wherein a proximate end portion of the sensor cavity located at the sensor opening has a first diameter and a distal end portion of the sensor cavity opposite the proximate end portion has a second diameter and wherein the first diameter is greater than the second diameter.
2. The fluid tank system of claim 1, wherein the at least one fluid leak hole is located in the guide tube proximate the distal end portion of the sensor cavity.
3. The fluid tank system of claim 1, wherein the guide tube is integrally formed with the fluid container.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The present disclosure is illustrated by way of example and not limited in the accompanying figures in which like reference numerals indicate similar elements. The drawing figures are not necessarily drawn to scale unless specifically indicated otherwise.
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DETAILED DESCRIPTION
(15) It is noted that various connections are set forth between elements in the following description and in the drawings (the contents of which are incorporated in this specification by way of reference). It is noted that these connections are general and, unless specified otherwise, may be direct or indirect and that this specification is not intended to be limiting in this respect. A coupling between two or more entities may refer to a direct connection or an indirect connection. An indirect connection may incorporate one or more intervening entities or a space/gap between the entities that are being coupled to one another.
(16) Aspects of the disclosure may be applied in connection with a gas turbine engine.
(17) The engine sections 18-21 are arranged sequentially along the centerline 12 within an engine housing 22. Each of the engine sections 18-19B, 21A and 21B includes a respective rotor 24-28. Each of these rotors 24-28 includes a plurality of rotor blades arranged circumferentially around and connected to one or more respective rotor disks. The rotor blades, for example, may be formed integral with or mechanically fastened, welded, brazed, adhered and/or otherwise attached to the respective rotor disk(s).
(18) The fan rotor 24 is connected to a gear train 30, for example, through a fan shaft 32. The gear train 30 and the LPC rotor 25 are connected to and driven by the LPT rotor 28 through a low speed shaft 33. The HPC rotor 26 is connected to and driven by the HPT rotor 27 through a high speed shaft 34. The shafts 32-34 are rotatably supported by a plurality of bearings 36; e.g., rolling element and/or thrust bearings. Each of these bearings 36 is connected to the engine housing 22 by at least one stationary structure such as, for example, an annular support strut.
(19) As one skilled in the art would appreciate, in some embodiments a fan drive gear system (FDGS), which may be incorporated as part of the gear train 30, may be used to separate the rotation of the fan rotor 24 from the rotation of the rotor 25 of the low pressure compressor section 19A and the rotor 28 of the low pressure turbine section 21B. For example, such an FDGS may allow the fan rotor 24 to rotate at a different (e.g., slower) speed relative to the rotors 25 and 28.
(20) During operation, air enters the turbine engine 10 through the airflow inlet 14, and is directed through the fan section 18 and into a core gas path 38 and a bypass gas path 40. The air within the core gas path 38 may be referred to as “core air”. The air within the bypass gas path 40 may be referred to as “bypass air”. The core air is directed through the engine sections 19-21, and exits the turbine engine 10 through the airflow exhaust 16 to provide forward engine thrust. Within the combustor section 20, fuel is injected into a combustion chamber 42 and mixed with compressed core air. This fuel-core air mixture is ignited to power the turbine engine 10. The bypass air is directed through the bypass gas path 40 and out of the turbine engine 10 through a bypass nozzle 44 to provide additional forward engine thrust. This additional forward engine thrust may account for a majority (e.g., more than 70 percent) of total engine thrust. Alternatively, at least some of the bypass air may be directed out of the turbine engine 10 through a thrust reverser to provide reverse engine thrust.
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(23) When the distal end 216 of the electronic stem is inserted into the tank via the sensor opening 206, the guide tube 218 radially aligns the distal end 216 with a distal end receiver 220. The longitudinal length of the guide tube 218 is selected based upon the length of the tank that the distal end 216 has to traverse. For example, the longer the distance to traverse the longer the guide 218 should be to ensure the distal end 216 is in radial alignment with the distal end receiver 220 when the flange 212 seats on a rim of the sensor opening 206.
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(25) During assembly of the sensor into the tank, the assembly tooling guide pins 244, 246 are inserted into assembly tool bores 258, 260 in the rim. As the longitudinally extending electronic stem 250 passes through the sensor opening 252 the assembly tooling guide pins 244, 246 pass through apertures 261, 262, respectively, of the flange 254, ensuring that the distal end 248 of the electronic stem is aligned and positioned with respect to the seat 256. Once the flange 254 is seated on the rim (e.g., via a gasket), then the assembly tooling guide pins 244, 246 are moved, and fasteners (not shown) are inserted into the assembly tool bores 258, 260 to secure the flange 254 to the rim 256.
(26) In another embodiment for operably positioning the sensor in the tank,
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(31) In yet another embodiment,
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(34) The spring holder 342 may include a radially interior surface 356 that each of the springs applies a radial force to. In the interest of ease of illustration the radial exterior surface that the springs contact is not shown. Referring to
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(36) It is contemplated that the radially interior surface 356 may be a single surface that surrounds an area co-axial with the sensor opening 344, or the radially interior surface 356 may comprise a plurality of surfaces that surrounds the area co-axial with the sensor opening 344. In either embodiment the interior surface(s) align the distal end 357 of the sensor stem to ensure proper installation on the level sensor. A tapered distal end 360 of the O-ring projection 358 may be used to allow the O-ring projection 358 to smoothly engage the spring holder 342.
(37) To assist with removal of the sensor from the tank, the spring holder 342 includes a tapered proximate end surface 368, which is smoothly contacted by the tapered surface 370 of the O-ring projection as the fluid level sensor is being removed from the tank.
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(40) While various embodiments of the present invention have been disclosed, it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible within the scope of the invention. For example, the present invention as described herein includes several aspects and embodiments that include particular features. Although these features may be described individually, it is within the scope of the present invention that some or all of these features may be combined with any one of the aspects and remain within the scope of the invention. Accordingly, the present invention is not to be restricted except in light of the attached claims and their equivalents.