CN200963523Y - Device for manufacturing and detecting spotting hand-thrown model aeroplane - Google Patents
Device for manufacturing and detecting spotting hand-thrown model aeroplane Download PDFInfo
- Publication number
- CN200963523Y CN200963523Y CN 200620067084 CN200620067084U CN200963523Y CN 200963523 Y CN200963523 Y CN 200963523Y CN 200620067084 CN200620067084 CN 200620067084 CN 200620067084 U CN200620067084 U CN 200620067084U CN 200963523 Y CN200963523 Y CN 200963523Y
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- CN
- China
- Prior art keywords
- upper counterangle
- fuselage
- vertical panel
- model
- keeper
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
A producing and detecting device of an ejecting handing model aircraft relates to an ejecting and handing model aircraft, providing a producing and detecting device of an ejecting handing model aircraft. The utility model comprises an airframe base, an airframe positioning component, a position processing and testing platform of an upper dihedral angle and a back sweepback, a position adjusting and testing platform of the upper dihedral angle, an upper dihedral angle adjusting fixing rod and an upper dihedral angle finger; the airframe positioning component is arranged in the cavity of the airframe base; the position processing and testing platform of the upper dihedral angle and the back sweepback comprises left and right side boards, the inner side of which is movably connected with the cavity of the airframe base; the position adjusting and testing platform of the upper dihedral angle comprises left and right vertical boards, which are fixed with the outside of the airframe base and the front of the left and right side boards; the left and right vertical boards are provided with an upper dihedral angle scale adjusting groove; the upper dihedral angle adjusting fixing rod comprises left and right adjusting rods, which are fixed on the left and right vertical boards through the adjusting groove; the upper dihedral angle finger comprises left and right fingers, one end of the left and right fingers are connected with the left and right adjusting rods. The utility model is of high working efficiency and good glue quality.
Description
Technical field
The utility model relates to a kind of launching and the hand-thrown model of an airplane, especially relates to a kind of hand-thrown model of an airplane that launches and makes and checkout gear.
Background technology
In the model airplane activity, the processing of the wing upper counterangle of the ejection model airplane and the hand-thrown model of an airplane and processing of the angle at angle of sweep and position of centre of gravity etc. is a big difficult point, especially the initial stage contacts the teenager that model aircraft is made, will be in thick only 3 millimeter, be symmetrical measurement on the wing of convexo-plane and process the oblique angles of required tens degree, then left and right sides wing is composed and have certain upper counterangle and angle of sweep, it is the zero degree established angle that ejection model airplane work sheet and hand-thrown model of an airplane work sheet generally require wing, and the hand-thrown rectilinear flight model of an airplane generally requires the angle of sweep (different design drawings then has different design angles to require) about wing sweepback 20 degree.And wing, empennage and the fuselage that processing and fabricating is finished carried out the assembling of complete machine again according to desired angle, and adjustment center of gravity, guarantee the balance of the model of an airplane, the specification requirement of everything is to participating in more scabrous technical problem of teenager Lai Shuoshi of model activity.Simultaneously its detection is not seen that relevant report is arranged yet.
Summary of the invention
The purpose of this utility model is participating in the movable more scabrous technical problem that is run in the model aircraft of making of model aircraft at the teenager, provides a kind of hand-thrown model of an airplane that launches to make and checkout gear.
The utility model is provided with fuselage base, fuselage keeper, the upper counterangle and angle of sweep location processing and fixed bar and upper counterangle pointer are regulated in detection platform, upper counterangle location adjusting and detection platform, the upper counterangle.The fuselage keeper is used for the location of fuselage, and the fuselage keeper is located at the fuselage base intracavity; The upper counterangle and the processing of location, angle of sweep comprise left plate and right plate with detection platform, and the inboard of left plate and right plate and fuselage base intracavity flexibly connect, and left plate and right plate are provided with 0～90 ° of angle of sweep scale; Location, the upper counterangle is regulated with detection platform and is comprised left vertical panel and right vertical panel, left side vertical panel and right vertical panel are separately fixed at fuselage chassis outer side and left plate and right plate leading section, are respectively equipped with 0～30 ° of upper counterangle scale and upper counterangle regulating tank on left vertical panel and right vertical panel; The upper counterangle is regulated fixed bar and is comprised left adjusting rod and right adjusting rod, and left adjusting rod and right adjusting rod pass upper counterangle regulating tank, and are separately fixed on left vertical panel and the right vertical panel, the translation in the regulating tank of the upper counterangle respectively of left adjusting rod and right adjusting rod; Upper counterangle pointer is used to indicate the upper counterangle, and upper counterangle pointer comprises left pointer and right pointer, and an end of left pointer and right pointer is connected with right adjusting rod with left adjusting rod respectively.
The fuselage keeper can be established forebody keeper and rear body keeper, and the forebody keeper is located at the front portion of fuselage base intracavity, and the rear body keeper is located at the rear portion of fuselage base intracavity.
Constitute because in fact the utility model measures processing gummed, wing upper counterangle mensuration processing gummed, complete machine gummed and four parts such as detection and the detection of model position of centre of gravity by wing oblique angle and wing setting, therefore to the wing of the aerofoil profile that machined, in order to have improved operating efficiency in aspects such as processing, upper counterangle degree on inclined-plane, the upper counterangle are accurately measured, gummed; At the bonding quality that improves the model of an airplane, guarantee flight safety in addition, the angle that particularly improves each parts is made, complete machine is assembled on the accuracy and is significantly improved; Can also measure model of an airplane position of centre of gravity simultaneously.Because the utility model can accurately measure each angle, be improved providing, detect the data accuracy rate of related angle data to the flight achievement.Providing and detecting data accurately to periodic check or through the model of an airplane of maintenance.
Description of drawings
Fig. 1 is the structural representation of the utility model embodiment.
The specific embodiment
Following examples will be further described the utility model in conjunction with the accompanying drawings.
Referring to Fig. 1, the utility model is provided with grooved fuselage base 1, forebody keeper 21, rear body keeper 22, the upper counterangle and angle of sweep location processing and fixed bar and upper counterangle pointer are regulated in detection platform, upper counterangle location adjusting and detection platform, the upper counterangle.The fuselage keeper is used for the location of fuselage, forebody keeper 21 is located at the front portion of fuselage base 1 inner chamber, rear body keeper 22 is located at the rear portion of fuselage base 1 inner chamber, is respectively equipped with the groove 211 and 221 that is used for fixing fuselage in mmi machine body keeper 21 and the rear body keeper 22.The upper counterangle and the processing of location, angle of sweep comprise left plate 31 and right plate 32 with detection platform, and left plate 31 flexibly connects by loose-leaf 4 with the inboard and fuselage base 1 inner chamber of right plate 32, and left plate 31 and right plate 32 are provided with 0～90 ° of angle of sweep scale.Location, the upper counterangle is regulated with detection platform and is comprised left vertical panel 51 and right vertical panel 52, left side vertical panel 51 and right vertical panel 52 are separately fixed at fuselage base 1 outside and left plate 31 and right plate 32 leading sections, are respectively equipped with 0～30 ° of upper counterangle scale and upper left dihedral regulating tank 511 and upper right dihedral regulating tank 521 on left vertical panel 51 and right vertical panel 52.The upper counterangle is regulated fixed bar and is comprised left adjusting rod 61 and right adjusting rod 62, left side adjusting rod 61 and right adjusting rod 62 pass upper left dihedral regulating tank 511 and upper right dihedral regulating tank 521 respectively, and be separately fixed on left vertical panel 51 and the right vertical panel 52 translation in upper left dihedral regulating tank 511 and upper right dihedral regulating tank 521 respectively of left adjusting rod 61 and right adjusting rod 62.Upper counterangle pointer is used to indicate the upper counterangle, and upper counterangle pointer comprises left pointer 71 and right pointer 72, and an end of left pointer 71 and right pointer 72 is connected with right adjusting rod 62 with left adjusting rod 61 respectively.
Below provide and launch the concrete grammar that the hand-thrown model of an airplane is made processing and detected.
1. location, the upper counterangle is regulated and is detected
It is also fixing that the left and right adjusting bar is adjusted to the angle that needs, this moment the left and right sides vertical panel corresponding angle that tilts immediately, the upper counterangle can be made as 0～35 degree, the left and right sides wing that machines is lain in the upper counterangle and processing of location, angle of sweep and detection platform, lean against the vertical straight down polishing of platform left and right sides wing with husky cloth, just the inclined-plane that will glue together angle can be accurately processed, the wing gummed can be carried out simultaneously.
2. processing of the upper counterangle and angle of sweep location and detection
When needs are processed with the model at angle of sweep, left and right sides wing is aimed at the upper counterangle and processing of location, angle of sweep and detection platform (upper counterangle and angle of sweep can process and glue together simultaneously), use the same method and just can process the upper counterangle and angle of sweep accurately.
3. complete machine assembling and detection
The part (fuselage, wing, empennage) that processes under the detection of assembly platform, is carried out the complete machine assembling according to needed angle.
4. position of centre of gravity detects
When needing the position of centre of gravity of monitoring model aircraft, can on monitor station, carry out at any time by pilot pin (for example large size quilt sewing needle).
Claims (3)
1. launching the hand-thrown model of an airplane makes and checkout gear, it is characterized in that being provided with fuselage base, fuselage keeper, the upper counterangle and angle of sweep location processing and detection platform, upper counterangle location adjusting and detection platform, the upper counterangle and regulate fixed bar and upper counterangle pointer, the fuselage keeper is located at the fuselage base intracavity; The upper counterangle and the processing of location, angle of sweep comprise left plate and right plate with detection platform, and the inboard of left plate and right plate and fuselage base intracavity flexibly connect; Location, the upper counterangle is regulated with detection platform and is comprised left vertical panel and right vertical panel, left side vertical panel and right vertical panel are separately fixed at fuselage chassis outer side and left plate and right plate leading section, are respectively equipped with 0～30 ° of upper counterangle scale and upper counterangle regulating tank on left vertical panel and right vertical panel; The upper counterangle is regulated fixed bar and is comprised left adjusting rod and right adjusting rod, and left adjusting rod and right adjusting rod pass upper counterangle regulating tank, and are separately fixed on left vertical panel and the right vertical panel; Upper counterangle pointer comprises left pointer and right pointer, and an end of left pointer and right pointer is connected with right adjusting rod with left adjusting rod respectively.
2. the hand-thrown model of an airplane that launches as claimed in claim 1 is made and checkout gear, it is characterized in that left plate and right plate are provided with 0～90 ° of angle of sweep scale.
3. the hand-thrown model of an airplane that launches as claimed in claim 1 is made and checkout gear, it is characterized in that the fuselage keeper establishes forebody keeper and rear body keeper, the forebody keeper is located at the front portion of fuselage base intracavity, and the rear body keeper is located at the rear portion of fuselage base intracavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620067084 CN200963523Y (en) | 2006-11-06 | 2006-11-06 | Device for manufacturing and detecting spotting hand-thrown model aeroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620067084 CN200963523Y (en) | 2006-11-06 | 2006-11-06 | Device for manufacturing and detecting spotting hand-thrown model aeroplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN200963523Y true CN200963523Y (en) | 2007-10-24 |
Family
ID=38867540
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620067084 Expired - Fee Related CN200963523Y (en) | 2006-11-06 | 2006-11-06 | Device for manufacturing and detecting spotting hand-thrown model aeroplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN200963523Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106902522A (en) * | 2016-10-30 | 2017-06-30 | 天津师范大学 | A kind of wing for being applied to ejection type soaring aeroplane model |
-
2006
- 2006-11-06 CN CN 200620067084 patent/CN200963523Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106902522A (en) * | 2016-10-30 | 2017-06-30 | 天津师范大学 | A kind of wing for being applied to ejection type soaring aeroplane model |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20071024 Termination date: 20101106 |