CN103057696A - Novel fixed-wing aircraft starting device - Google Patents
Novel fixed-wing aircraft starting device Download PDFInfo
- Publication number
- CN103057696A CN103057696A CN2012105762568A CN201210576256A CN103057696A CN 103057696 A CN103057696 A CN 103057696A CN 2012105762568 A CN2012105762568 A CN 2012105762568A CN 201210576256 A CN201210576256 A CN 201210576256A CN 103057696 A CN103057696 A CN 103057696A
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- battery
- wing aircraft
- start button
- starter motor
- starter
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The present invention provides a novel fixed-wing aircraft starting device, belonging to the technical field of fixed-wing aircrafts. The starting device is characterized by comprising: a starter cup shield, a battery, a starter motor, a start button, and a converter. The battery is electrically connected with the converter, the start motor and the start button; the battery supplies power to the starter motor; the start button is used for control of the switch of the circuit; and the starter motor is connected with a starter cup shield shaft. The starting device also comprises a starting rack, handles are arranged on both sides of the starting rack, the start button is located on the handle of one side, the battery is installed on the outer side of the start rack, the outside of the battery is the starter cup shield, the starter motor and the converter are arranged at the inner side of the starting rack. As a result of the above technical proposal, the tedious steps the during the starting of the traditional fixed-wing aircraft are reduced, thereby making flight operations of the fixed-wing aircraft more convenient, and improving work efficiency of flight operations.
Description
Technical field
The invention belongs to the fixed wing aircraft technical field, especially relate to a kind of novel fixed wing aircraft starter gear.
Background technology
The actuator that existing fixed wing aircraft generally adopts starts mechanical device and the startup power supply separates, and the degree of so taking off step is loaded down with trivial details, and the equipment that carries when going out to fly operation is more.For example, need on some actuators all must to couple together with the electrical generator of automobile front in the time of each the startup with two not only long but also thick startup lines, perhaps carry a homemade power generation assembly, so just increased the weight of article, and it is also inconvenient to operate.Reduced to a certain extent the efficient of flight operation.
Summary of the invention
The problem to be solved in the present invention provides a kind of novel fixed wing aircraft starter gear, and troublesome operation step when having reduced the fixed wing aircraft startup has improved the efficient of flight operation.
For solving the problems of the technologies described above, the technical solution used in the present invention is: a kind of novel fixed wing aircraft starter gear, it is characterized in that: comprise actuator cup cover, battery, starter motor, start button, conv, above-mentioned battery is electrically connected with conv, starter motor and start button, battery is the starter motor power supply, and start button is used for the switch of control circuit; Starter motor is connected with actuator cup cover axle.
Further, also comprise the startup frame, the both sides of described startup frame are provided with handle, and described start button is positioned on the side grip, and described battery is installed in the outside that starts frame, and the outside of battery is actuator cup cover, and the installed inside that starts frame has starter motor and conv.
Further, described battery is lithium cell.
Further, described battery is positioned in the battery compartment, and described battery compartment comprises battery compartment loam cake and battery compartment side plate.
Further, described battery compartment loam cake links to each other with the startup frame by the magnet adsorption mode.
Advantage and good effect that the present invention has are: owing to adopting technique scheme, the loaded down with trivial details step when having reduced traditional fixed wing aircraft and starting makes the fixed wing aircraft operation of going out to fly convenient, has improved the high efficiency of the operation of going out to fly.
Description of drawings
Fig. 1 is structural representation of the present invention
Among the figure:
1, actuator cup cover 2, battery 3, starter motor
4, start button 5, conv 6, startup frame
7, handle 81, battery compartment loam cake 82, battery compartment side plate
The specific embodiment
As shown in Figure 1, novel fixed wing aircraft starter gear provided by the invention, comprise actuator cup cover 1, battery 2, starter motor 3, start button 4, conv 5, above-mentioned battery 2 is electrically connected with conv 5, starter motor 3 and start button 4, battery 2 is starter motor 3 power supplies, and start button 4 is used for the switch of control circuit; Starter motor 3 covers 1 axle with the actuator cup and is connected.Also be provided with startup frame 6, the both sides that start frame 6 are provided with handle 7, and described start button 4 is positioned on the side grip 7, and described battery 2 is installed in the outside that starts frame 6, and the outside of battery 2 is actuator cup cover 1, and the installed inside that starts frame 6 has starter motor 3 and conv 5.Battery 2 is preferably lithium cell, also can adopt the close battery of volume and capacity of cell.Described battery 2 is positioned in the battery compartment, and described battery compartment comprises battery compartment loam cake 81 and battery compartment side plate 82, and battery compartment loam cake 81 links to each other with startup frame 6 by the magnet adsorption mode.
Above one embodiment of the present of invention are had been described in detail, but described content only is preferred embodiment of the present invention, can not be considered to be used to limiting practical range of the present invention.All equalizations of doing according to the present patent application scope change and improve etc., all should still belong within the patent covering scope of the present invention.
Claims (5)
1. novel fixed wing aircraft starter gear, it is characterized in that: comprise actuator cup cover, battery, starter motor, start button, conv, above-mentioned battery is electrically connected with conv, starter motor and start button, battery is the starter motor power supply, and start button is used for the switch of control circuit; Starter motor is connected with actuator cup cover axle.
2. novel fixed wing aircraft starter gear according to claim 1, it is characterized in that: also comprise the startup frame, the both sides of described startup frame are provided with handle, described start button is positioned on the side grip, described battery is installed in the outside that starts frame, the outside of battery is actuator cup cover, and the installed inside that starts frame has starter motor and conv.
3. novel fixed wing aircraft starter gear according to claim 1, it is characterized in that: described battery is lithium cell.
4. novel fixed wing aircraft starter gear according to claim 1 and 2, it is characterized in that: described battery is positioned in the battery compartment, and described battery compartment comprises battery compartment loam cake and battery compartment side plate.
5. novel fixed wing aircraft starter gear according to claim 4 is characterized in that: described battery compartment loam cake by the magnet adsorption mode with start frame and link to each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012105762568A CN103057696A (en) | 2012-12-25 | 2012-12-25 | Novel fixed-wing aircraft starting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012105762568A CN103057696A (en) | 2012-12-25 | 2012-12-25 | Novel fixed-wing aircraft starting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103057696A true CN103057696A (en) | 2013-04-24 |
Family
ID=48100660
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012105762568A Pending CN103057696A (en) | 2012-12-25 | 2012-12-25 | Novel fixed-wing aircraft starting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103057696A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5535713A (en) * | 1994-09-14 | 1996-07-16 | Braddock; Douglas J. | Combination field box and engine starter for model airplane engines |
| WO1999040316A1 (en) * | 1998-02-10 | 1999-08-12 | Johnson Controls Technology Company | Battery and starter motor assembly |
| JP2011043081A (en) * | 2009-08-19 | 2011-03-03 | Makita Corp | Attachment for starting engine of working machine by using power tool |
-
2012
- 2012-12-25 CN CN2012105762568A patent/CN103057696A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5535713A (en) * | 1994-09-14 | 1996-07-16 | Braddock; Douglas J. | Combination field box and engine starter for model airplane engines |
| WO1999040316A1 (en) * | 1998-02-10 | 1999-08-12 | Johnson Controls Technology Company | Battery and starter motor assembly |
| JP2011043081A (en) * | 2009-08-19 | 2011-03-03 | Makita Corp | Attachment for starting engine of working machine by using power tool |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C05 | Deemed withdrawal (patent law before 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130424 |