Simplified system for disconnecting a power outlet of a cardan in a vehicle with a trailer
11571967 · 2023-02-07
Assignee
Inventors
Cpc classification
B60D1/145
PERFORMING OPERATIONS; TRANSPORTING
B60K25/06
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
Disclosed herein is a vehicle (1)—preferably a tractor—with a trailer (2) operatively connected thereto with a cardan (3), said cardan (3) comprising a power take-off, said power take-off being switched off when said cardan (3) builds with said vehicle (1) and/or with said trailer (2) an angle (ε) smaller than a first threshold value (a) and/or larger than a second threshold value (β) and being switched on when said angle (ε) exceeds again said first threshold value (β) thanks to suitable actuators, including detection means of the angle formed between the cardan (3) and said vehicle and/or trailer. According to the present invention, said angle (ε) is detected by a detector consisting of a magnetic device (4) placed on the trailer (2) or the vehicle (1) and an electronic compass (5) placed on the vehicle (1) or on the trailer (2). Preferably, the angle (ε) insisting on the cardan (3) is obtained according to the formula: ε=180−Y−arcsen (l/m sen y) (3) where y is the angle the compass (5) forms with respect to the straight travel with the magnet (4), I is the distance between the cardan (3) and the compass (5), m is the distance between the cardan (3) and the magnet (4).
Claims
1. A system for disconnecting a power take-off in a vehicle which is operatively connected to a trailer via a cardan, said system comprising a detection means for disconnecting said power take-off when said cardan forms with said vehicle and/or with said trailer an angle ε smaller than a first threshold value α and/or greater than a second threshold value β, and connects the power take-off when said angle ε exceeds said first threshold value again and/or goes below said second threshold value β via one or more actuators, said one or more actuators cooperating with said detection means for detecting the angle formed between the cardan and said vehicle and/or trailer, wherein said detection means includes a magnetic device placed on the trailer or vehicle and an electronic compass arranged on the vehicle or on the trailer such that the detection means detects measurements corresponding to said angle ε.
2. The system of claim 1, wherein said compass is placed on the vehicle near the cardan or on the cardan near the vehicle.
3. The system of claim 1, wherein said magnetic device is selected from a permanent magnet and an electromagnet, which comes into operation with the motor of the vehicle via the power take-off.
4. The system of claim 1, wherein said first threshold angle is 145° and said second threshold angle β is 325°.
5. The system of claim 1, wherein the angle ε of the cardan is obtained according to a computation of: ε=180−γ−arcsen (I/m sen γ) where γ is an angle the compass forms with respect to straight travel with the magnet, I is a distance between the cardan and the compass, and m is a distance between the cardan and the magnet.
6. The system of claim 1, wherein the compass and the magnetic device are on a common axis during the straight travel of the vehicle and the trailer.
7. The system of claim 1 further comprising means for checking the speed (G) of the vehicle and means for comparing said speed with a smaller limit value(B), so that if G<B the power take-off is disconnected.
8. The system of claim 7 further comprising means for comparing said speed (G) with a higher limit value (T), so that if G>T and ε<α, where α is the first threshold value, the power take-off is connected.
9. The system of claim 1, wherein the vehicle and/or the trailer have a pair of side probes, one of said pair of side probes being positioned on each side of the vehicle and/or of the trailer.
10. The system of claim 9, wherein the side probes are at least one of electro-valves and photoelectric cells.
11. The system of claim 10, wherein said side probes are electro-valves having an active state, which are deactivated by lack of contact.
12. The system of claim 11, wherein said side probes are electro-valves having an inactive state, which are activated by contact.
13. The system of claim 9, wherein said side probes are adjustable-length rods.
14. The system of claim 9, wherein the side probes are removably fixed and have varying lengths.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further features and advantages of the invention will anyhow be more apparent from the following detailed description of a preferred embodiment, given by mere way of non-limiting example and illustrated in the accompanying drawings, wherein:
(2)
(3)
(4)
(5)
(6)
(7)
BEST MODE FOR CARRYING OUT THE INVENTION
(8)
(9) The cardan 3 is connected, as said, to a power take-off (not shown in the drawings), said power take-off being disengaged when said cardan 3 forms with said vehicle 1 and/or with said trailer 2 an angle ε below a first threshold value (α) and/or over a second threshold value (β) and being inserted when said angle exceeds again said first threshold value α or goes below said second threshold value β thanks to suitable actuators cooperating with means for detecting the angle ε formed between the cardan 3 and the said vehicle 1 and/or trailer 2. Advantageously, said smaller threshold angle α is 35° while said upper threshold angle β is 145° since, up to such angles, the operation of the power take-off does not have a negative effect on the cardan 3 and its integrity.
(10) According to the present invention, a magnet 4 is provided on the trailer 2, or in its immediate vicinity on the cardan 3. Conversely, on the vehicle 1—generally near the cardan 3—or on the cardan 3, in the immediate vicinity of the vehicle 1, an electronic compass 5 of a type per se known is provided. The magnet 4 can be a permanent magnet, or it can be an electromagnet, which comes into operation with the engine of the vehicle 1 from which it draws energy and acts on the compass 5, superimposing to the geographic north, thanks to the short distance and intensity of the magnet 4, and constituting a “fake north”, suitable for guiding the compass 5. The signal from the compass 5 is transmitted to a processing unit capable of acting on the actuator means.
(11)
(12) The probes 10, 11 may be of any known type, such as electrovalves, photoelectric cells or other devices known per se. They may be bolted to vehicle 1 or a movably fixed, provided they are sufficiently firm. In case two electrovalves are used, they can be of the always active type, which is deactivated by the lack of contact, and of the always inactive type, which is activated by the lack of contact.
(13) Preferably, the probes 10, 11 are fixed to vehicle 1 in a removable manner and have varying lengths, so as to provide greater versatility.
(14) During the straight travel of the vehicle 1, the situation is as shown in
(15) At the moment when vehicle 1 runs a bend, the situation is the one generally represented in
(16) The angle between the compass 5 and the magnet 4 is determined by the compass 5, which is oriented according to the position of the magnet 4 which, as mentioned above, replaces the geographic north as a fake north, and its correlation with angle ε may be carried out according to the most common methods known in the art. In practice, during the entire travel of the vehicle 1 and the trailer 2, the compass 5 detects the angle between the compass 5 and the cardan 3, bi-univocally connected to the angle ε, and transmits it to a processing unit (for example, a motor control unit) and correlates it to obtain the value of the angle ε which is formed at the cardan 3.
(17) When it is determined that the angle ε becomes smaller than a threshold value (e.g., preferably 145°) or greater than a second threshold value (e.g., and preferably 360°-35°, i.e., 180°+145°, i.e. 325°), the processing unit sends to the actuator means a signal which, in a manner known per se, disengages the power take-off so that the joint with the cardan 3 stops rotating, thereby preserving the integrity of the same cardan 3. The vehicle will continue to travel along the bend, until it finishes its path and resumes its normal travel.
(18) Once the angle returns above the first threshold value (e.g., preferably 145° or below a second threshold value (e.g., and preferably 360° to 35°, i.e. 180°+145°, i.e. 325°), the processing unit sends a signal which, in a known manner, causes, thanks to the same actuator means, the power take-off to be switched back on, so that the machine mounted on the trailer 2 (for example, but not limited thereto, a sprayer, a mower, a crushing machine, a hedger) will be restarted, avoiding an excessively long interruption, which would compromise the quality of the performed work.
(19) In practice, by using the device according to the present invention, movement occurs by obviating the opposite disadvantages of cardan breakage and insufficient work performance, avoiding both extremes in a useful and advantageous way.
(20) As for the correlation mechanisms, a preferred embodiment is illustrated in
(21) For clarification purposes, the distance between the cardan 3 and the compass 5 is indicated by letter l, while the distance between the cardan 3 and the magnet 4 is indicated by letter m. Advantageously, l and m are constant values during vehicle travel, depending solely on the relative arrangement of the cardan 3, the magnet 4 and the compass 5, as there is no reason to slide the magnet 4 or the compass 5 in a translational direction. In a further preferred way, l and m are manufacturing data of the vehicle 1 and of the trailer 2 contained in the vehicle processing unit 1 so that it is not necessary to set them at each start of the vehicle 1 itself. At the moment of the bend, the angle between the distance d between the magnet 4 and the electronic compass 5 and the side l is called γ, while the angle between the distance of the side m is called η.
(22) The situation that is being created is, according to trigonometry:
η=arcsen (l/m sen γ) (2)
similarly to what happened with formula (1) mentioned in the introduction.
(23) Taking into account that the sum of the angles inside a triangle (in this case the triangle 3, 4, 5) is 180°, formula (2) can also be written as:
ε=180−γ−arcsen (l/m sen γ) (3)
(24) Therefore, the angle ε which insists on the cardan 3 is immediately obtained according to the formula:
ε=180−γ−arcsen (l/m sen γ) (3)
where γ is the angle the compass 5 makes with respect to the straight travel with the magnet 4, l is the distance between the cardan 3 and the compass 5, m is the distance between the cardan 3 and the magnet 4.
(25) The necessary and sufficient condition for formula (3) to obtain the exact angle ε is that the compass 5 and the magnet 4 are on the same straight line during the straight travel of the vehicle 1 and the trailer 2. As can be immediately seen, formula (3) allows to obtain the angle ε (which insists on cardan 3) only as a function of the angle γ, which is continuously measured by the electronic compass 5 without the need for any other measure, so that the calculations are extremely simple, without an excessive computing load in the processing unit of the vehicle 1.
(26) By calling the smaller threshold angle α, the processing unit executes the process shown in
(27) In step 12, a value of γ is detected by compass 5 and transmitted to the processing unit. In the next step 13, the value of ε is calculated based on the detected value of γ. In step 14, the value of ε is compared to the value of α.
(28) If the value of ε is lower than the value of α, the process continues with step 15, in which the power take-off is disengaged and the cardan 3 stops rotating. Subsequently, the process returns to step 12 and resumes.
(29) If the value of ε is higher than the value of α, the process continues with step 16, the system checks whether the power take-off is disengaged.
(30) If it is disengaged, the process continues with step 17, the power take-off is reinserted and the cardan 3 restarts its rotation. Subsequently, the process goes back to step 12, the process resumes from the first step.
(31) If the power take-off is not disengaged, the process returns from step 16 to step 12 and resumes from the beginning.
(32) Analogous reasoning is for the second threshold angle β, the condition to be tested in 14 being now ε<β rather than ε>α.
(33) The embodiment shown in
(34) During travel, the probes 10 and 11 come into contact with the rows, for example 6 and 7, and are forcefully inclined by them towards the rear of vehicle 1. When one or both of the probes 10, 11 are no longer in contact with rows 6 or 7, respectively, they return to their original position perpendicular to the axle of the vehicle 1. When this happens, a signal is sent to the processing unit that disengages the power take-off even if the travel of the vehicle 1 and the trailer 2 is straight. In this way, continuation of work in the absence of rows is avoided and material is saved, avoiding an unnecessary burden on the environment.
(35) The process that is being created is that shown in
(36) The process starts in step 18, checking in step 19 whether there is a towed or carried tool.
(37) If the tool is towed, the process moves to step 20 or, if it is carried, to step 21.
(38) In step 20, a check is performed to see if ε is greater than α. If so, the process goes to step 21, otherwise it goes to step 23.
(39) At step 21, a check is performed to see if the sensor of 10 has felt something from a time less than τ. If so, the process goes to step 22, otherwise it goes to step 23.
(40) At step 22, a check is performed to see if the sensor of 11 has felt something from a time smaller than τ. If so, the process goes back to step 18 and resumes, otherwise it goes to step 23.
(41) At step 23, the power take-off is disengaged, going on to step 24.
(42) Step 24 occurs if a power take-off disengagement time of less than τ has passed. If so, the check is repeated remaining at step 24, otherwise the process resumes at step 18.
(43) As can be seen, the present invention may be applied to any type of vehicle operatively connected to a trailer with a cardan, providing for the automatic engagement and disengagement of the power take-off if the angle formed on the cardan 3 is dangerous for the integrity of the cardan 3 itself in case of continuation of its rotation. Contrary to the prior art systems, the arrangement of the fake north (magnet 4) and the electronic compass 5 allows to determine the angle that insists on the cardan 3 regardless of the type of vehicle 1 and trailer 2, which may include vehicles of any kind, with wheels or tracks or even a tracked vehicle and a wheeled trailer or a wheeled vehicle and a tracked trailer, the only parameter to be measured being the deviation angle (γ) of the magnet 4—fake north—compared to the straight travel, such angle being continuously monitored by the electronic compass 5.
(44) The embodiment shown in
(45) As an alternative to the embodiment shown in
(46) Once the vehicle 1 starts to travel, the angle γ is detected at step 12. At the same time, speed G is detected. Generally, if the tractor has a low speed, it means that it is describing a wide curve to switch from one row to another row and it will not be performing work, while a high speed G indicates work in progress. The speed G, with the switched-on power take-off, is compared with a smaller limit speed B at step 25.
(47) If G>B, the process continues to the next step 13, where the angle ε is calculated according to formula (3):
ε=180−γ−arcsen (l/m sen γ) (3)
If G<B, the power take-off is switched off anyway. At the next step 14, the angle ε is compared with the threshold angle α and, if it is smaller, the cardan 3 is disconnected at step 15; contrarily, if it is greater, the process goes to the next step 16. At step 16, a check is performed to see whether the cardan is connected or not.
(48) If the result of step 16 is that the cardan 3 is disconnected, the speed G is re-detected and if the value G is greater than the upper threshold value T, the cardan is re-connected in the next step 17 otherwise it remains disconnected. Indeed, a speed G greater than the threshold T means that the tractor is operating close to a row 6, 7, 8 or 9.
(49) In practice, the system according to this embodiment also comprises means for testing the speed G of the vehicle and means for comparing said speed with a smaller limit value B, so that if G<B the power take-off is disengaged. In addition, to complete the process, the system also includes means for comparing said speed G with a higher limit value T, so that if G>T and ε<α the power take-off is switched back on.
(50) In this way, it is possible to save on working when there are no rows, without the need for probes 10 or 11.
(51) It is understood, however, that the invention is not to be considered as limited by the particular arrangement illustrated above, which represents only an exemplary implementation of the same, but different variants are possible, all within the reach of a person skilled in the art, without departing from the scope of the invention itself, as defined by the following claims.
LIST OF REFERENCE NUMERALS
(52) 1 Vehicle
(53) 2 Trailer
(54) 3 Cardan
(55) 4 Magnet
(56) 5 Electronic compass
(57) 6 Row
(58) 7 Row
(59) 8 Row
(60) 9 Row
(61) 10 Side probe
(62) 11 Side probe
(63) 12 Process step
(64) 13 Process step
(65) 14 Process step
(66) 15 Process step
(67) 16 Process step
(68) 17 Process step
(69) B Towed tool
(70) C Detection
(71) D Detection
(72) E Angle comparison
(73) F Time from detection
(74) 18 Process step
(75) 19 Process step
(76) 20 Process step
(77) 21 Process step
(78) 22 Process step
(79) 23 Process step
(80) 24 Process step
(81) 25 Process step
(82) α Lower threshold angle
(83) β Upper threshold angle
(84) γ Angle between cardan (3) and compass (5)
(85) ε Angle on the cardan
(86) η Angle between cardan and magnet (4)