Embodiments are generally related to sensor methods and systems. Embodiments are also related to methods and systems for configuring and implementing sensors. Embodiments are additionally related to components for maintaining sensors.
A wide variety of solid-state sensors are used in a variety of commercial and industrial applications. For example, such sensors are actively used in pressure and temperature sensing applications. In general, a sensor can be thought of as a device that responds to a stimulus, such as heat, light, or pressure, and generates a signal that can be measured or interpreted. Such sensors typically incorporate some form of a sensing element, which is a basic component that usually changes some physical parameter to an electrical signal for detection purposes.
Some sensors are based on magnetic components. For example, magnetic position sensors can include digital and analog Hall Effect position sensors, magnetoresistive digital sensors, Hall Effect vane sensors, gear tooth sensors, Hall Effect basic switch, and magnets. Magnetic Position Sensors are reliable, high speed, long life sensors and are directly compatible with other electronic circuits.
These sensors respond to the presence or the interruption of a magnetic field by producing either a digital or an analog output proportional to the magnetic field strength. Digital and analog “sensor-only” devices are operated by the magnetic field from a permanent magnet or electromagnet. Actuation mode depends on the type of magnets used. Integral magnet position sensors can be operated by either a vane passing through a gap or a magnet mounted on a plastic plunger. Positions sensors, for example, are typically used in applications that require accurate, reliable outputs. They are found in brushless DC motors, utility meters, welding equipment, vending machines, home appliances, computers, and so on.
Other types of sensors include force sensors, mass airflow sensors, silicon pressure sensors, and stainless steel pressure sensors. Force sensors, for example, are utilized for precise reliable performance in compact commercial grade packages. Amplified and unamplified microbridge mass airflow sensors typically provide a sensitive and fast response to the flow of air or other gas over the chip. Silicon pressure sensors usually contain sensing elements that include piezoresistors buried in the face of a thin, chemically-etched silicon diaphragm. A pressure change causes the diaphragm to flex, inducing a stress or strain in the diaphragm and the buried resistors. Resistor values change in proportion to the stress applied to produce an electrical output. Stainless steel pressure sensors, on the other hand, range from miniature surface mount sensors to high-end stainless steel isolated transmitters used for stringent process control.
One of the problems with current sensors and sensor packaging technology is that such devices require expensive over-molds or post-mold inserted bushings along with costly components such as bolts with thread locking mechanisms. Such devices are particularly susceptible to assembly errors or damage caused by vibration in a high vibration environment. Vibration can often result in so-called “cold flow” or other deformations of the sensor or sensor mounting surface, which can negatively affect the sensor performance.
Based on the foregoing it is believed that an improved sensor method and system is necessary to overcome these problems. Such an improved sensor, including methods and systems thereof, is disclosed herein.
The following summary of the invention is provided to facilitate an understanding of some of the innovative features unique to the present invention and is not intended to be a full description. A full appreciation of the various aspects of the invention can be gained by taking the entire specification, claims, drawings, and abstract as a whole.
It is, therefore, one aspect of the present invention to provide for improved sensor methods and systems.
It is another aspect of the present invention to provide an improved method and system for mounting a sensor to a mounting surface, while avoiding the consequences of harsh vibration environments.
The aforementioned aspects of the invention and other objectives and advantages can now be achieved as described herein. A sensor system and method are disclosed. In general, a sensor is associated with a mounting surface. An O-ring can be positioned between the sensor and the mounting surface, such that the O-ring is compressible when the sensor is fixed to the mounting surface. A fixing mechanism can also be provided for permanently fixing the sensor to the mounting surface, such that the O-ring located between the sensor and the mounting surface provides a proper tension thereof which prevents the sensor from being adversely affected by vibration resulting from a harsh vibration environment in which the sensor operates. The fixing mechanism can be implemented as a fixing joint between the sensor and the mounting surface. Additionally, the O-ring and the sensor are configured with respect to one another and the mounting surface to maintain tension in the fixing joint.
The accompanying figures, in which like reference numerals refer to identical or functionally-similar elements throughout the separate views and which are incorporated in and form a part of the specification, further illustrate the present invention and, together with the detailed description of the invention, serve to explain the principles of the present invention.
The particular values and configurations discussed in these non-limiting examples can be varied and are cited merely to illustrate at least one embodiment of the present invention and are not intended to limit the scope of the invention.
In general, sensor mounting system 10 includes a sensor 12 associated with a mounting surface 14. An O-ring 16 can be positioned between the sensor 12 and the mounting surface 14, such that the O-ring 16 is compressible when the sensor 12 is fixed to the mounting surface 14. A fixing mechanism 18 can be provided for permanently fixing the sensor 12 to the mounting surface 14, such that the O-ring 16 located between the sensor 12 and the mounting surface 14 provides a proper tension on the fixing mechanism thereof which prevents the sensor 12 from being adversely affected by vibration resulting from a harsh vibration environment in which the sensor 12 operates.
The fixing mechanism 18 can be implemented as a fixing joint between the sensor 12 and the mounting surface 14. In general, the fixing mechanism 18 can be formed from mounting surface 14 and protrude from mounting surface 14 in order to couple with and/or receive sensor 12. Note that the fixing mechanism 18 can form a circular end 19, which protrudes above the top side of sensor 12. Note that as depicted herein, sensor 12 can comprise an actual sensor or, for example, a sensing element that forms a part of larger sensor device or system, depending upon design considerations.
The circular end 19 is depicted generally in
The O-ring 16 and the sensor 12 are generally configured with respect to one another and the mounting surface 14 to maintain tension in the fixing joint or fixing mechanism 18. The sensor 12 can therefore be permanently fixed to the mounting surface 14 utilizing an assembly component, such as, for example O-ring 16, fixing joint 18 and/or other types of components. The preferred mounting of sensor 12 utilizes O-ring 16 positioned between the sensor 12 and the mounting surface 14, such that the O-ring 16 will be compressed when the sensor 12 is fixed to the mounting surface 14. Alternatively, the O-ring 16 can be utilized such that it is compressed between the dome shaped end portion 20 and the sensor 12.
The sensor 12 can then be permanently fixed to the mounting surface 14 utilizing a low-cost assembly method, such as, for example, riveting, heat-staking, snap-fitting, and the like. One alternative example of a low-cost assembly method that can be adapted for use in accordance with the embodiments disclosed herein is “twist-lock” style mounting configuration that employs the o-ring 16 for tension. The use of the O-ring 16 between the sensor 12 and the mounting surface 14 can provide a methodology and system for maintaining proper tension in the fixing joint or fixing mechanism 18 so that the sensor 12 is not affected by vibration, regardless of any “cold flow” or other deformation of sensor 12 or mounting surface 14.
The configuration depicted in
It will be appreciated that variations of the above-disclosed and other features and functions, or alternatives thereof, may be desirably combined into many other different systems or applications. Also that various presently unforeseen or unanticipated alternatives, modifications, variations or improvements therein may be subsequently made by those skilled in the art which are also intended to be encompassed by the following claims.
Number | Name | Date | Kind |
---|---|---|---|
3140614 | Willis | Jul 1964 | A |
4050307 | McMullen et al. | Sep 1977 | A |
4132237 | Kennedy et al. | Jan 1979 | A |
4524038 | Heinemann et al. | Jun 1985 | A |
4665376 | Heinrich | May 1987 | A |
4665740 | Matsumoto et al. | May 1987 | A |
4715220 | Eitoku et al. | Dec 1987 | A |
4774626 | Charboneau et al. | Sep 1988 | A |
5191178 | Baker | Mar 1993 | A |
5338907 | Baker et al. | Aug 1994 | A |
5348267 | Lanting et al. | Sep 1994 | A |
5454270 | Brown et al. | Oct 1995 | A |
5889284 | Mattis | Mar 1999 | A |
6405593 | Palfenier et al. | Jun 2002 | B1 |
6470739 | Matsumura et al. | Oct 2002 | B1 |
6813952 | Yamashita et al. | Nov 2004 | B2 |
6898972 | Bauer et al. | May 2005 | B2 |
7339612 | Yajima | Mar 2008 | B1 |
20040150144 | Goepfert et al. | Aug 2004 | A1 |
20040182163 | Yamashita et al. | Sep 2004 | A1 |
20040187559 | Yokoi | Sep 2004 | A1 |
20040201464 | Oonishi | Oct 2004 | A1 |
20040211875 | Wisniewski et al. | Oct 2004 | A1 |
20050076725 | Heiland | Apr 2005 | A1 |
20050149464 | Nugent | Jul 2005 | A1 |
20050149465 | Nugent | Jul 2005 | A1 |
20050151615 | Nugent | Jul 2005 | A1 |
20060171704 | Bingle et al. | Aug 2006 | A1 |
20070085248 | Chang | Apr 2007 | A1 |
20080078259 | Duff | Apr 2008 | A1 |
Number | Date | Country |
---|---|---|
7607712 | Dec 1976 | DE |
629785 | Dec 1994 | EP |
61053525 | Mar 1986 | JP |
07009567 | Jan 1995 | JP |
2001215139 | Aug 2001 | JP |
2001 332878 | Nov 2001 | JP |
Number | Date | Country | |
---|---|---|---|
20070039397 A1 | Feb 2007 | US |