Embodiments of the present disclosure relate generally to a system that improves heat distribution throughout an internal cooking cavity of an oven. The embodiments described may find particular use in ovens used on-board passenger transport vehicles, but they may also be incorporated into other ovens, such as residential and other commercial ovens.
Currently, cooking cavity temperatures are monitored by a temperature sensor that is located at the back of the cavity. Typically, this sensor is located behind the baffle plate that separates the meals that are contained inside the cavity from the oven's hardware, such as the heating elements and the blower wheel. The temperature sensor is designed to turn the heating elements on and off, depending upon the temperature of the cooking cavity. This can be referred to as “cycling” of the oven.
The baffle plate is designed to control air distribution in the cooking cavity. It may have an opening in the middle that pulls in air from the cooking cavity. Heated air can then be allowed to travel around sides of the baffle plate, back to the cooking cavity in order to create an air loop.
In one aspect, the temperature sensor can be programmed to prompt the heaters to switch off at a pre-set temperature. Because the rear of the oven (which is where the sensor and the heating elements are located) will heat more quickly than the interior of the cooking cavity, this pre-set temperature is generally lower than the temperature of the rest of the cooking cavity. This means that shutting off the heating elements at the pre-set temperature results in uneven temperatures throughout the cooking cavity. The ambient temperature behind the baffle plate does not reflect the ambient temperature in the rest of the cooking cavity, as the temperature in this area may be considerably higher than the rest of the cooking cavity. In this scenario, the temperatures at the front of the cooking cavity are lower than the temperatures at the back of the cooking cavity. This can result in large variations of meal temperatures, longer cooking times, and variations in meal quality.
Embodiments described herein thus provide a system to measure the temperature at various locations in the cooking cavity and to adjust the temperature at which the heating elements turn on and off. Embodiments of this disclosure seek to improve the temperature variations in meals by creating a more uniform cooking cavity temperature for the duration of the cooking cycle. Multiple temperature sensors are provided in order to determine an average oven temperature from points measured at multiple areas of the cooking cavity.
Ovens for use on board aircraft are generally used to re-heat meals. According to aircraft regulations, the meals should be heated to a minimum temperature, generally above about 70° C. In order to comply with this requirement, aircraft ovens may need to run longer than necessary in order to have all meals heated to this temperature. One problem this creates is that some meals will be heated to temperatures that are higher than desired, which can result in meal degradation. Similar situations can occur with other residential and commercial ovens.
As shown in
If the pre-set value is 200° F., and the rear temperature sensor 12 senses a 200° F. temperature in the sensing area, it will trigger a control system to turn off the heating element(s) 16. However, when the temperature in the sensing area behind the baffle plate 14 is 200° F., it is likely that the area of the cooking cavity 10 in front of the baffle plate 14 is not that high. Variations of up to several degrees can occur.
Accordingly, the present disclosure provides one or more front temperature sensors 20, 22 at areas in the cooking cavity 10 in front of the baffle plate 14. One example is shown in
The value recorded by the rear temperature sensor 12 can be combined with the value recorded by the one or more front temperature sensors 20, 22 in order to determine an optimal shut off point for the heating element(s) 16. This combination may be run by an algorithm or formula that will account for various variables, including optimal cooking temperature and an optimal working temperature for the hardware. Thus, rather than shutting off at a pre-set value, the heating elements 16 can be allowed to continue to heat until a more optimal temperature in the cooking cavity 10 has been reached, based on information obtained from various data points in the cooking cavity 10.
In one method 300 as illustrated in the flowchart of
In short, temperature data and/or measured variable(s) from the one or more front temperature sensors 20, 22 will be combined with temperature data and/or measured variable(s) from the rear temperature sensor 12 in order to determine an optimal temperature value, rather than simply using an automatic pre-set value. The communication system can run an algorithm designed to optimize the temperature and the point at which the heating elements should be cycled (i.e., turned on and/or off). The controller then implements the instructions from the communication system. The controller and the communication system may be designed to be integral with the oven, such that they are components installed with or near the oven. In other embodiments, the controller and the communication system may be designed to be remote from the oven, such that they compute and control at a distance away from the oven and relay instructions back to the oven. They may be connected with a wired connection or a wireless connection, either to one another and/or to the oven cooking cavity.
As shown in the schematic information flow of
It is possible to create the algorithm so that the rear temperature sensor 410 is the master and the one or more front temperature sensors 420 are slaves. This results in the rear temperature sensor being the controlling factor in the equation, but being adjustable based on the values sensed by the slave sensors 420.
Changes and modifications, additions and deletions may be made to the structures and methods recited above and shown in the drawings without departing from the scope or spirit of the invention and the following claims.
This application claims the benefit of U.S. Provisional Application Ser. No. 61/733,257, filed Dec. 4, 2012, titled “Temperature Control System,” the entire contents of which are hereby incorporated by reference.
Number | Date | Country | |
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61733257 | Dec 2012 | US |