Energy transforming unit for distance measurement sensor
09634543 ยท 2017-04-25
Assignee
Inventors
Cpc classification
F03G1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B60G2300/60
PERFORMING OPERATIONS; TRANSPORTING
F16F9/3292
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03G1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
H02K7/18
ELECTRICITY
B60G13/14
PERFORMING OPERATIONS; TRANSPORTING
F03G1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F9/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The subject invention relates to an air spring (1) with a distance measurement sensor (100), an energy transforming unit (200), a first mounting element (10) being adapted for being mounted to a first vehicle portion (2) and a second mounting element (20) being adapted for being mounted to a second vehicle portion (3). An air volume (50) is arranged between the first mounting element and the second mounting element. The energy transforming unit is adapted to transform a transition of the air spring from a first state (s1) of the air spring to a second state (s2) of the air spring into electrical energy and to provide the generated electrical energy to the distance measurement sensor. The energy transforming unit is arranged in the air volume (50) of the air spring.
Claims
1. An air spring, comprising: a distance measurement sensor; an energy transforming unit comprising a propeller and a generator; a first mounting element being adapted for being mounted to a first vehicle portion; a second mounting element being adapted for being mounted to a second vehicle portion; an air volume arranged between the first mounting element and the second mounting element, wherein the energy transforming unit is adapted to transform a transition of the air spring from a first state (s1) of the air spring to a second state (s2) of the air spring into electrical energy and to provide the generated electrical energy to the distance measurement sensor; wherein the propeller is adapted for being moved when transitioning from the first state to the second state and is adapted to drive the generator, wherein the generator generates the electrical energy; and wherein the distance measurement sensor is arranged within and receives the generated electrical energy within the air volume of the air spring; and a pneumatic pressure generator adapted for varying air pressure within the air spring, wherein the pneumatic pressure generator is positioned within the air volume of the air spring, and wherein the pneumatic pressure generator is adapted to modulate a pressure in the air volume when the generated electrical energy is below a threshold.
2. The air spring according to claim 1, wherein the propeller is adapted to being rotated when the pressure in the air volume of the air spring varies as a result of the transition from the first state to the second state.
3. The air spring according to claim 1 wherein the propeller is mechanically coupled to the generator via an axis.
4. The air spring according to claim 3, wherein the energy transforming unit comprises a housing with an opening and rigid walls, and wherein the propeller is arranged in the opening.
5. The air spring according to claim 4, wherein the propeller is adapted to being rotated when an air pressure in the air volume of the air spring varies such as to cause an air flow through the opening.
6. The air spring according to claim 5, wherein a rotation plane of the propeller extends along an opening plane of the opening such that a rotation axis of the propeller extends along an air flow direction through the opening.
7. The air spring according to claim 6, wherein the housing comprises an interior space such that a variation of the air pressure in the air spring leads to an air exchange between an interior space outside the housing and the interior space inside the housing through the opening; and wherein the air exchange causes the propeller to rotate.
8. The air spring according to claim 5, wherein a rotation plane of the propeller is parallel to an opening plane of the opening.
9. The air spring according to claim 8, wherein the housing comprises an interior space such that a variation of the air pressure in the air spring leads to an air exchange between an interior space outside the housing and the interior space inside the housing through the opening; and wherein the air exchange causes the propeller to rotate.
10. The air spring according to claim 5, wherein the housing comprises an interior space such that a variation of the air pressure in the air spring leads to an air exchange between an interior space outside the housing and the interior space inside the housing through the opening; and wherein the air exchange causes the propeller to rotate.
11. The air spring according to claim 1, wherein the energy transforming unit and the distance measurement sensor are each attached to the first mounting element; and wherein the energy transforming unit is electrically connected via a power line to the distance measurement sensor.
12. An air spring comprising: a distance measurement sensor; an energy transforming unit comprising a thermoelectric cooler which is adapted for generating electrical energy out of a temperature gradient; a first mounting element being adapted for being mounted to a first vehicle portion; a second mounting element being adapted for being mounted to a second vehicle portion; and an air volume arranged between the first mounting element and the second mounting element, wherein the energy transforming unit is adapted to transform a transition of the air spring from a first state (s1) of the air spring to a second state (s2) of the air spring into electrical energy and to provide the generated electrical energy to the distance measurement sensor, wherein the distance measurement sensor is arranged within and receives the generated electrical energy within the air volume of the air spring; and wherein the temperature gradient is a temperature gradient between temperature fluctuations of gas in the air volume of the air spring.
13. An air spring comprising: a distance measurement sensor; an energy transforming unit; a pneumatic pressure generator adapted for varying air pressure within the air spring; a first mounting element being adapted for being mounted to a first vehicle portion; a second mounting element being adapted for being mounted to a second vehicle portion; and an air volume arranged between the first mounting element and the second mounting element, wherein the energy transforming unit is adapted to transform a transition of the air spring from a first state (s1) of the air spring to a second state (s2) of the air spring into electrical energy and to provide the generated electrical energy to the distance measurement sensor, wherein the energy transforming unit generates the electrical energy using the variations of the air pressure in the air spring, wherein the distance measurement sensor is arranged within and receives the generated electrical energy within the air volume of the air spring; and wherein the pneumatic pressure generator is positioned within the air volume of the air spring.
14. The air spring according to claim 13, wherein the pneumatic pressure generator is adapted to vary the air pressure within the air volume of the air spring prior to an operating state of the air spring.
15. The air spring according to claim 13, wherein the pneumatic pressure generator is adapted to vary the air pressure within the air volume of the air spring during an operating state of the air spring.
16. The air spring according to claim 13, wherein the pneumatic pressure generator is adapted to vary the air pressure within the air volume of the air spring during an operating state of the air spring.
17. An air spring, comprising: a distance measurement sensor; an energy transforming unit comprising a coil and a magnetic element; a first mounting element adapted for being mounted to a first vehicle portion; a second mounting element adapted for being mounted to a second vehicle portion; an air volume arranged between the first mounting element and the second mounting element, wherein the energy transforming unit is adapted to transform a transition of the air spring from a first state (s1) of the air spring to a second state (s2) of the air spring into electrical energy and to provide the generated electrical energy to the distance measurement sensor, wherein the electrical energy is transformed when the coil is moved with respect to the magnetic element, and wherein the distance measurement sensor is arranged within and receives the generated electrical energy within the air volume of the air spring; and a pneumatic pressure generator adapted for varying air pressure within the air spring, wherein the pneumatic pressure generator is positioned within the air volume of the air spring, and wherein the pneumatic pressure generator is adapted to modulate a pressure in the air volume when the generated electrical energy is below a threshold.
18. The air spring of claim 17, wherein the distance measurement sensor and the energy transforming unit are adapted to be coupled to either the first mounting element or the second mounting element.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8) The reference numerals used in conjunction with the drawings hereof are as follows:
(9) 1 air spring
(10) 2 first vehicle portion
(11) 3 second vehicle portion
(12) 10 first mounting element
(13) 20 second mounting element
(14) 30 belly
(15) 31 first edge
(16) 32 second edge
(17) 40 working stroke
(18) 50 air volume
(19) 60 air pipe/pressure pipe
(20) 70 pneumatic pressure generator
(21) 100 air spring height sensor
(22) 101 receiver
(23) 102 height measuring signal transmitter
(24) 200 energy transforming unit
(25) 210 housing
(26) 220 opening
(27) 225A first air flow direction
(28) 225B second air flow direction
(29) 227 opening plane
(30) 230 supporting arm
(31) 240 propeller
(32) 245 direction of rotation
(33) 247 rotation plane
(34) 250 rotation axis
(35) 260 generator
(36) 265 thermoelectric cooler
(37) 270 power line
(38) 280 interior space inside the housing 210
(39) 281 interior space outside of the housing 210 and inside of the air volume 50
(40) 300 method for providing energy
DETAILED DESCRIPTION OF THE INVENTION
(41)
(42) The belly encloses an air volume 50 such that the working stroke 40 of the air spring represents a movement of one of the first mounting element 10 and the second mounting element 20 towards the other one of the first mounting element 10 and the second mounting element 20.
(43) The air spring further comprises a pneumatic pressure generator 70 which is pneumatically connected to the air volume 50 of the air spring 1 by the air pipe or pressure pipe 60.
(44) A receiver 101 in form of a coil and a height measuring signal transmitter 102 are located within the air volume of the air spring as indicated by the air spring illustrated in dotted lines. The receiver 101 is located close to the first mounting element 10 of the air spring and the height measuring signal transmitter 102 is located close to the second mounting element 20 of the air spring. Both, the receiver and the height measuring signal transmitter may be designed as coreless coils such that a working stroke 40 of the air spring is not reduced by these devices which are located within the air volume of the air spring.
(45) The energy transforming unit 200 is electrically connected to the sensor or sensor electronics, i.e. to the receiver 101 and to the height measuring signal transmitter 102. The energy transforming unit 200 may be arranged inside of the air spring, i.e. within the air volume 50.
(46)
(47) The air spring as described above and hereinafter may in particular be a smart air spring with an air spring height sensor as described above and hereinafter as air spring level unit or height measurement system. The air spring may in particular be an air spring with intelligent sensor and actuator functions. One of the important features is the integrated air spring height sensor. The function of the air spring height sensor is it to measure with reasonable accuracy the current absolute axial position of the air spring, i.e. the distance between the first mounting element and the second mounting element. In other words, it determines or measures the current length of the air spring. Such a sensor solution may require its own, application specific electronics which will be described in more detail below.
(48) The air spring height sensor as described above and hereinafter may offer the following features: reduced or no sensitivity to electromagnetic interferences (EMI), insensitive or fully compensated for the potential effects caused by temperature and temperature fluctuations or variations, reasonably high signal resolution for the targeted measurement range, no shortening of the original operating or working stroke of the air spring, low electric current consumption, fast signal response with a wide signal bandwidth range, low or no emissions of electromagnetic interferences, insensitive to metallic objects of different kinds that may be placed near the air spring or placed inside the air spring, wherein in the latter limits of maximum size and maximum mass of the metallic object apply, insensitive to changes of humidity, dirt and dust to a certain extent.
(49) The air spring height sensor as described above and hereinafter is not limited to air spring applications. Wherever a large measurement stroke of a linear-position-sensor is required, this described electronics solution may be applicable. Large measurement stroke means that the signal amplitude ratio may change in exponential ratio, for example in a range greater than 1:100. Examples are (but not limited to): height and position changes in vehicle suspension system including all types of vehicles, like trucks, passenger cars, rains, planes, motor bikes, etc., control of industrial processing equipment like tooling, milling, drilling, mixing, filling, shifting, sorting, like luggage sorting and handling at airports, parcel sorting at the mail service, etc., test equipment like flight simulator, engine test bed, furniture reliability tests, sports equipment testing, etc., large scale, indirect load measurement systems like weight-on-beam design, large scale mining equipment like oil drilling, tunneling, steering and position control systems in ships (rudder position), planes (flaps, rudder,). Other applications for this application may be measuring accurately the distance to a metallic object, like when the engine (locomotive) of a train is coupling to a rail-road wagon, or when a pushing-truck at the airport is automatic or semi-automatic coupling to the front-wheel of a plain. When implementing an air spring height sensor as described above and hereinafter into a smart air spring system, it may be important not to shorten the actual mechanical stroke of the air spring.
(50) There may exist several different ways to integrate an air spring height sensor as described above and hereinafter into an air spring.
(51)
(52) The specification of an air spring set by manufacturers may define the usable working stroke range 40 which is shown in connection with the first state and the second state of the air spring in
(53) The second state is the state in which the sensor signal transfer is most efficient and therefore the largest height signal can be expected at the output of the passive or active working signal receiver. This signal may also be called the original or untreated height signal.
(54) When moving from the second state to the first state, the distance between the height measuring signal transmitter and the receiver steadily increases such that the original height signal is decreasing, wherein the decreasing may occur exponentially.
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(58) The propeller 240 is connected to the generator 260 via the shaft 250. Thus, when the air flow 225A, 225B flows into or out of the housing 210 from the interior space 280 within the housing to the interior space 281 outside the housing, the propeller is being turned or set in rotation such that the generator is driven to generate electric energy. The generator provides the electric energy to the sensor electronics via the power line 270. In addition to the generator, a thermoelectric cooler element 265 may be provided within or out of the housing in order to generate electric current for providing to the sensor electronics via the power line 270.
(59)
(60)
(61) This application claims benefit of European Patent Application Serial No. EP 1315663.5, filed on Jan. 17, 2013. While certain representative embodiments and details have been shown for the purpose of illustrating the subject invention, it will be apparent to those skilled in this art that various changes and modifications can be made therein without departing from the scope of the subject invention.