The present invention relates to micro air vehicles, and, more particularly, to an improved starter for micro air vehicles.
Micro air vehicles and other unmanned aerial vehicles are of emerging importance today, particularly for military applications. For example, micro air vehicles can be valuable in providing reconnaissance without the need for human pilots. Micro air vehicles often include engines that are started using a manual starter assembly similar to those commonly used with commercial lawn mowers. However, in certain situations, the activation of such a starter assembly may require significant pull force, which may in turn result in unwanted movement of certain micro air vehicle components (e.g. a guidance system), and/or may result in wear on one or more components of the micro air vehicle.
Accordingly, there is a need for an improved starter assembly that requires a relatively lower pull force, and/or that results in reduced movement and/or reduced induced inertia on the engine. In addition, there is a need for such an improved starter assembly that does not rely on any external electrical power sources. There is also a need for such an improved starter assembly with a reduced weight. The present invention addresses one or more of these needs.
The present invention provides a manual starter for an engine. In one embodiment, and by way of example only, the manual starter comprises a main housing, an output shaft, a spring housing, a spring, and an attachment unit. The output shaft is disposed at least partially inside the main housing, and is configured to supply a starting torque to the engine. The spring housing is disposed in the main housing. This spring is disposed in the spring housing, and is configured to receive an initial force from a starter cord and to supply the starting torque to the output shaft. The attachment unit is configured to selectively couple the spring to the output shaft before the engine has started and decouple the spring from the output shaft after the engine has started.
In another embodiment, and by way of example only, the manual starter comprises a main housing, a starter cord, a spring housing, a drive assembly, a spring, an output shaft, and an attachment unit. The starter cord is disposed at least partially outside the main housing, and is configured to receive an initial force. The spring housing is disposed in the main housing. The drive assembly is disposed at least partially within the main housing, and is configured to transfer the initial force from the starter cord to the spring housing. The spring is disposed in the spring housing, and is configured to receive the initial force from the spring housing and to supply a starting torque for the engine. The output shaft is disposed at least partially inside the main housing, and is configured to receive the starting torque from the spring and to supply the starting torque to the engine. The attachment unit is configured to selectively couple the spring to the output shaft before the engine has started and to decouple the spring from the output shaft after the engine has started. The attachment unit comprises a pawl and a coupler. The pawl is coupled to the output shaft. The coupler is coupled to the spring, and is configured to be selectively engaged and disengaged to the pawl.
The invention also provides a micro air vehicle. In one embodiment, and by way of example only, the micro air vehicle comprises a main body, a plurality of electronic pods, an engine, and a manual starter system. The plurality of electronic pods are coupled to the main body. The engine is disposed in the main body, and is coupled to the plurality of electronic pods. The manual starter system comprises a main housing, a starter cord, a spring housing, a drive assembly, a spring, an output shaft, and an attachment unit. The starter cord is disposed at least partially outside the main housing, and is configured to receive an initial force. The spring housing is disposed in the main housing. The drive assembly is disposed at least partially within the main housing, and is configured to transfer the initial force from the starter cord to the spring housing. The spring is disposed in the spring housing, and is configured to receive the initial force from the spring housing and to supply a starting torque for the engine. The output shaft is disposed at least partially inside the main housing, and is configured to receive the starting torque from the spring and to supply the starting torque to the engine. The attachment unit is configured to selectively couple the spring to the output shaft before the engine has started and to decouple the spring from the output shaft after the engine has started. The attachment unit comprises a pawl and a coupler. The pawl is coupled to the output shaft. The coupler is coupled to the spring, and is configured to be selectively engaged and disengaged to the pawl.
Other independent features and advantages of the preferred manual starter assembly will become apparent from the following detailed description, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
Before proceeding with the detailed description, it is to be appreciated that the described embodiment is not limited to use in conjunction with a particular type of device. Thus, although the present embodiment of the manual starter assembly is, for convenience of explanation, depicted and described as being implemented in a micro air vehicle, it will be appreciated that it can be implemented in various other types of vehicles, and in various other devices that implement an internal combustion engine.
The engine 106 is disposed in the main body 102, and is coupled to the electronic pods 104. The engine 106, once started, stimulates the flight of the micro air vehicle 100, for example through the activation of the fan 109 coupled thereto. The engine 106 is started by the manual starter assembly 108, which will be discussed in greater detail now below in connection with
The starter cord 204 is disposed at least partially outside the main housing 202, and preferably inside a tube 216 that is coupled to the main housing 202. The power cord 204 is configured to receive an initial force from an individual or device (not depicted) for starting the engine 106, while the individual or device simultaneously holds onto at least a portion of the main body 102. In addition, a retraction spring housing 218 and a retraction spring 220 housed within the retraction spring housing 218, retract the starter cord 204 after a pull sequence in which the starter cord 204 receives an initial force. The power spring housing 206 is disposed in the main housing 202, and houses the power spring 210. The drive assembly 208 is also disposed at least partially within the main housing 202, and is configured to transfer the initial force from the starter cord 204 to the power spring 210.
In the depicted embodiment, the drive assembly 208 includes a pulley 222, an input shaft 224, one or more input pawls 226, an output shaft end 227, and one or more release pawls 228. The drive assembly may be considered to also include one or more of the starter cord 204, the power spring housing 206, the power spring 210, and the output shaft 212. The pulley 222 is coupled to the retraction spring 220, and to the power spring housing 206 via the input pawls 226, which are coupled to both the pulley 222 and the power spring housing 206. The input pawls 226 preferably each include a spring 213 (depicted in
The power spring housing 206 is configured to rotate around the input shaft 224 upon receiving the initial force from the pulley 222 via the input pawls 226, and to thereby energize the power spring 210. This rotation of the power spring housing 206 is stabilized at least in part by a plurality of bearings 232, and a shim 221 helps to keep the power spring 210 from causing wear on the power spring housing 206 (see
The output shaft 212 is disposed at least partially inside the main housing 202, and includes an output shaft end 227 and one or more stops 234 for the release pawls 228 (see
The stops 234 on the output shaft 212 are configured to prevent release pawls 228 from rotating more than a predetermined angle following disengagement from the power spring 210, as will be shown in greater detail further below in
The attachment unit 214 includes a plurality of release pawls 228 and a coupler 230, and is configured to selectively couple the power spring 210 to the output shaft 212 before the engine 106 has started, and to decouple the power spring 210 from the output shaft 212 after the engine 106 has started. The release pawls 228 are each coupled to the output shaft 212, and selectively engage and disengage the coupler 230. Specifically, the release pawls 228 disengage the coupler 230 after the engine 106 has started, due to an increase in centrifugal force from the rotational speed of the engine 106, as will be described in greater detail further below in connection with
The coupler 230 is coupled to, and configured to interface with, each of the release pawls 228 and the power spring 210. The coupler 230 is configured to at least facilitate the selective coupling and separation of the power spring 210 and the power spring housing 206 from the output shaft 212. The coupler 230 is further configured to interface with the release pawls 228 to transfer torque, and to release the release pawls 228 at high rotational speeds, as will be described in greater detail further below in connection with
Turning now to
As depicted in
As shown in
As shown in
The bottom portion 248 is configured to mate with the power spring 210, preferably at least in part by having the power spring 210 wrap around the bottom portion 248 (see
Having now described the structural features of the manual starter assembly 108, the operation of an exemplary embodiment of the manual starter assembly 108 will now be described. For a user, the operation of the manual starter assembly 108 feels similar to pulling the cord on a commercial lawn mower, but with a relatively lower pull force. Once the end of the output shaft end 227 is interfaced with the output shaft 212 of the engine 106, the compression of the engine 106 thereby applies the above-mentioned holding force, thereby preventing rotation of the output shaft 212.
Once the starter cord 204 is pulled, the initial force is transferred to the power spring housing 206 via the drive assembly 208. Specifically, when the starter cord 204 is pulled, the retraction spring 220 is wound, and the starter cord 204 is at least partially unwound from the pulley 222. The pulley 222 rotates around the input shaft 224, thereby causing the input pawls 226 to rotate, and thereby causing the power spring housing 206 to rotate, around the input shaft 224. The starting torque is thus transferred from the pulley 222 to the power spring housing 206 via the input pawls 226. Preferably, the drive assembly 208 works similar to that of a commercial lawn mower.
The power spring housing 206 then rotates and winds the power spring 210. Meanwhile, the coupler 230, the release pawls 228, and the output shaft 212 are not yet rotating, due to the holding force exerted by the compression of the engine 106 interfacing with the output shaft end 227. During this time, the power spring 210 is energized in a direction opposing the holding force supplied by the engine compression through the interface with the output shaft end 227. The power spring 210 subsequently unwinds, or releases, once the power spring 210 is energized sufficiently to overcome the holding force applied by the engine compression.
Once the power spring 210 unwinds, it releases the starting torque, which turns the output shaft 212 and thereby starts the engine 106. Specifically, because the power spring 210 is coupled to the coupler 230, the coupler 230 rotates as the power spring 210 unwinds. The release pawls 228 at this point are engaged with the coupler 230, and similarly rotate. This in turn causes the output shaft 212 to spin, thereby starting the engine 106.
The power spring 210 and the power spring housing 206 are then disconnected from the output shaft 212, as the release pawls 228 disengage from the coupler 230. Specifically, the high rotational speed of the engine 106 after it is started causes the release pawls 228 to disengage from the coupler 230, utilizing the inertia of the mass of the release pawls 228. The stops 234 prevent the release pawls 228 from rotating more than thirty degrees following this disengagement, to minimize unnecessary movement and wear. Meanwhile, the output shaft 212 continues to spin while the engine 106 is running, but is now disconnected from the coupler 230, the power spring 210, and the power spring housing 206. Also, preferably at this point the input pawls 226 also disengage from the pulley 222 (see, e.g., the second coupler 230 depicted in
Eventually, when the engine 106 stops, the release pawls 228 re-engage with the coupler 230, thereby reconnecting the output shaft 212 to the power spring 210 and the power spring housing 206. The manual starter assembly 108 is then ready for the next time that the engine 106 is to be started, at which point in time the process repeats.
The manual starter assembly 108 can be potentially advantageous in a number of different manners. For example, the disengagement feature of the release pawl 228 design potentially reduces wear on the drive assembly 208 and/or other components of the power spring housing 206, potentially reduces unwanted movement of micro air vehicle 100 components during the start-up process, and also reduces induced inertia loads on the engine 106. The starter hub can be easily removed from the engine interface regardless of whether the engine 106 is running or stopped, thereby allowing the micro air vehicle to be placed on the ground for launching or for storage and transporting. In addition, the manual starter assembly 108 is relatively light in weight, and does not rely on any external electrical power sources. The starting process for the engine 106 is also made easier by inducing a force exerted by the power spring 210 on the output shaft 212 that assists in overcoming the engine compression force. While a particular micro air vehicle 100 is depicted in
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt to a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
This invention was made with Government support under contract number MDA972-01-9-0018 awarded by the Defense Advanced Research Processes Agency (DARPA). The Government has certain rights in this invention.
Number | Name | Date | Kind |
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6676084 | Asseline et al. | Jan 2004 | B2 |
6782863 | Leasure et al. | Aug 2004 | B2 |
6981482 | Tsunoda et al. | Jan 2006 | B2 |
Number | Date | Country | |
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20080315041 A1 | Dec 2008 | US |