CN105620774A - Angle adjusting mechanism for wing outer end feeler lever - Google Patents
Angle adjusting mechanism for wing outer end feeler lever Download PDFInfo
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- CN105620774A CN105620774A CN201410588861.6A CN201410588861A CN105620774A CN 105620774 A CN105620774 A CN 105620774A CN 201410588861 A CN201410588861 A CN 201410588861A CN 105620774 A CN105620774 A CN 105620774A
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- feeler lever
- bolt
- tooth plate
- oscillating bearing
- adjusting mechanism
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Abstract
The invention relates to an angle adjusting mechanism for a wing outer end feeler lever. The angle adjusting mechanism is composed of a feeler lever joint (1), a knuckle bearing (2), a bearing support (3), a nut (4), a feeler lever end (5), tile covers (6), bolts I (7), bolts II (8), brackets (9), a feeler lever middle portion (10), toothed pads (11) and toothed boards (12). When the feeler lever middle portion (10) is adjusted to the proper position, the bolts II (8) are locked, sawteeth of the toothed pads (11) and sawteeth of the toothed boards (12) are engaged, the feeler lever middle portion (10) is limited, and the feeler lever is fixed after the angle of the feeler lever is adjusted. By the adoption of the angle adjusting mechanism, the requirement for adjusting the angle of the feeler lever can be met, and the feeler lever can also be completely fixed when the adjusted position is proper.
Description
Technical field
The present invention relates to a kind of fixed wing airplane structural design, be particularly well-suited to the design of wing outer end feeler lever.
Background technology
At present on fixed wing airplane wing, increase equipment carries out reequiping varied, technology relative maturity, installing overhanging feeler lever additional in wing outer end is also one of common approach in repacking, general version is to connect hold-down support on suitable two ribs of wing outer end span, coordinate the fixing feeler lever of the FE Tiler being spirally connected, use bolt to be completely fixed. This kind of version Stability Analysis of Structures, it is easy to implement, easy to assembly, but equipment can not do the adjustment of any angle. When feeler lever is installed the precision equipments such as some exploration, tests, require over the error changing feeler lever angle to compensate fit on accumulation, or when needing to regulate the relative position of detecting devices and change test data, the hold-down support version of prior art cannot meet instructions for use, it is necessary to formulates a set of new scheme.
Summary of the invention
The technical problem to be solved in the present invention:
It is an object of the invention to provide a kind of needs that can meet feeler lever angular adjustment, the version being completely fixed by feeler lever again when adjusting position is suitable.
Technical scheme:
The technical solution of the present invention by the middle part of probing rod joint 1, oscillating bearing 2, bearing spider 3, nut 4, feeler lever end 5, FE Tiler 6, bolt I 7, bolt II 8, support 9, feeler lever 10, dentiform gasket 11, tooth plate 12 form. oscillating bearing 2 is put in the bearing spider 3 being connected with rib, and probing rod joint 1 may be inserted in oscillating bearing 2, and nut 4 is connected with probing rod joint 1 and is clipped in the middle by oscillating bearing 2, and probing rod joint 1 and feeler lever end 5 are spirally connected, and secure feeler lever end 5, two FE Tilers 6 are fastened in the middle part of feeler lever on 10, two bolts I 7 are connected to FE Tiler 6 both sides, FE Tiler 6 is made to clamp in the middle part of feeler lever 10, two tooth plates 12 are riveted on two supports 9 being connected with rib, and bolt II 8 runs through in the middle part of support 9, feeler lever 10, dentiform gasket 11, tooth plate 12 are fixed in the middle part of feeler lever 10, on support 9 and tooth plate 12, processing has the space of bolt II 8 activity when adjusting for feeler lever, after unclamping bolt II 8, the sawtooth of dentiform gasket 11 and tooth plate 12 separates, in the middle part of feeler lever 10 can along with bolt II 8 adjust in space movable, feeler lever end 5 is connected with oscillating bearing 2, feeler lever end 5 arbitrarily can rotate around the geometric center of oscillating bearing 2, 10 can with the geometric center of oscillating bearing 2 for the center of circle in the middle part of feeler lever, adjust for the arc track of radius R with the geometric center of oscillating bearing 2 to the distance of bolt II 8 axis, the tooth pitch of dentiform gasket 11 and tooth plate 12 is L, so dentiform gasket 11 and tooth plate 12 often adjust a sawtooth, feeler lever have adjusted �� degree, complete the angular adjustment of feeler lever, parameters relationship is as follows:
�� degree of regulation unit is degree
L dentiform gasket and tooth plate tooth pitch unit are millimeter
R center of rotation is millimeter to stay bolt axial line distance unit
When in the middle part of feeler lever, 10 adjustment are to correct position, clamping screw II 8, the sawtooth of dentiform gasket 11 and tooth plate 12 is meshed, and carries out spacing in the middle part of feeler lever 10, completes fixing after feeler lever angular adjustment.
Beneficial effects of the present invention:
It is stable that this invention has overall structure, structure takes up room little, it is to avoid the advantage such as complex parts and closed assembly appearance, has effectively used the engaging structure of sawtooth, has had feature easy to adjust, accurate positioning. Function aspects can make feeler lever in place on be completely fixed, as required the angle of feeler lever can be carried out again quick and easy convenient adjustment, the effective position changing equipment, compensate the error of accumulation in each link, and degree of regulation can be provided by simple calculating, offer help for structural design from now on, provide strong technical support and help for the monitoring of later aeronautical meteorology, geological prospecting or other precision measurements etc.
Accompanying drawing explanation
Fig. 1 is the feeler lever end construction of the present invention;
Fig. 2 is the feeler lever central structure of the present invention;
Fig. 3 is the overall structure form of the present invention;
Fig. 4 is sectional view in the middle part of the feeler lever of the present invention;
Fig. 5 is sectional view partial enlarged drawing in the middle part of the feeler lever of upper clamp;
Wherein, 1 be probing rod joint, 2 be oscillating bearing, 3 be bearing spider, 4 be nut, 5 be feeler lever end, 6 be FE Tiler, 7 for bolt I, 8 for bolt II, 9 be support, 10 in the middle part of feeler lever, 11 be dentiform gasket, 12 be tooth plate.
Detailed description of the invention
The technical solution of the present invention by the middle part of probing rod joint 1, oscillating bearing 2, bearing spider 3, nut 4, feeler lever end 5, FE Tiler 6, bolt I 7, bolt II 8, support 9, feeler lever 10, dentiform gasket 11, tooth plate 12 form.
Referring to Fig. 1, oscillating bearing 2 is put in the bearing spider 3 being connected with rib, and probing rod joint 1 may be inserted in oscillating bearing 2, and nut 4 is connected with probing rod joint 1 and is clipped in the middle by oscillating bearing 2, probing rod joint 1 and feeler lever end 5 are spirally connected, so that feeler lever end 5 is fixed on rib.
Referring to Fig. 2-3, two FE Tilers 6 are fastened in the middle part of feeler lever on 10, two bolts I 7 are connected to FE Tiler 6 both sides, FE Tiler 6 is made to clamp in the middle part of feeler lever 10, two tooth plates 12 are riveted on two supports 9 being connected with rib, and bolt II 8 runs through in the middle part of support 9, feeler lever 10, dentiform gasket 11, tooth plate 12 are fixed on rib by the middle part of feeler lever 10, by 10 two positions fixing in the middle part of feeler lever end 5 and feeler lever, limit whole six-freedom degrees of feeler lever, be fixed.
Referring to Fig. 4-5, on support 9 and tooth plate 12, processing has the space of bolt II 8 activity when adjusting for feeler lever, after unclamping bolt II 8, the sawtooth of dentiform gasket 11 and tooth plate 12 separates, in the middle part of feeler lever 10 can along with bolt II 8 adjust in space movable, feeler lever end 5 is connected with oscillating bearing 2, feeler lever end 5 arbitrarily can rotate around the geometric center of oscillating bearing 2, 10 can with the geometric center of oscillating bearing 2 for the center of circle in the middle part of feeler lever, adjust for the arc track of radius R with the geometric center of oscillating bearing 2 to the distance of bolt II 8 axis, the tooth pitch of dentiform gasket 11 and tooth plate 12 is L, so dentiform gasket 11 and tooth plate 12 often adjust a sawtooth, feeler lever have adjusted �� degree, complete the angular adjustment of feeler lever, parameters relationship is as follows:
�� degree of regulation unit is degree
L dentiform gasket and tooth plate tooth pitch unit are millimeter
R center of rotation is millimeter to stay bolt axial line distance unit.
Embodiment 1
On the basis of detailed description of the invention, the sawtooth of dentiform gasket 11 and tooth plate 12 is lance tooth, and FE Tiler 6 is semicircle. On support 9 and tooth 12, the space of bolt II 8 activity when adjusting for feeler lever of processing is Long Circle. L is 1 millimeter, and R is 555 millimeters, and calculating �� is 0.1 ��, namely dentiform gasket 11 and every one sawtooth of play of tooth plate 12, and feeler lever rotates 0.1 ��; When in the middle part of feeler lever, 10 adjustment are to correct position, clamping screw II 8, the sawtooth of dentiform gasket 11 and tooth plate 12 is meshed, and carries out spacing in the middle part of feeler lever 10, completes fixing after feeler lever angular adjustment.
Claims (4)
1. an angle adjusting mechanism for wing outer end feeler lever, the angle adjusting mechanism of described wing outer end feeler lever includes probing rod joint (1), oscillating bearing (2), bearing spider (3), nut (4), feeler lever end (5), FE Tiler (6), bolt I (7), bolt II (8), support (9), in the middle part of feeler lever (10), dentiform gasket (11), tooth plate (12), it is characterized in that: oscillating bearing (2) is put in the bearing spider (3) being connected with rib, probing rod joint (1) may be inserted in oscillating bearing (2), nut (4) is connected with probing rod joint (1) and is clipped in the middle by oscillating bearing (2), probing rod joint (1) and feeler lever end (5) are spirally connected, two FE Tilers (6) are fastened in the middle part of feeler lever on (10), two bolts I (7) are connected to FE Tiler (6) both sides, in the middle part of FE Tiler (6) clamping feeler lever (10), two tooth plates (12) are riveted on two supports (9) being connected with rib, bolt II (8) runs through support (9), in the middle part of feeler lever (10), dentiform gasket (11), tooth plate (12), support (9) and the upper processing of tooth plate (12) have the space that when adjusting, bolt II (8) is movable for feeler lever, after unclamping bolt II (8), the sawtooth of dentiform gasket (11) and tooth plate (12) can separate, in the middle part of feeler lever, (10) can along with bolt II (8) activity in adjustment space, feeler lever end (5) is connected with oscillating bearing (2), feeler lever end (5) arbitrarily can rotate around the geometric center of oscillating bearing (2), in the middle part of feeler lever, (10) can with the geometric center of oscillating bearing (2) for the center of circle, adjust for the arc track of radius R with the geometric center of oscillating bearing (2) to the distance of bolt II (8) axis, the tooth pitch of dentiform gasket (11) and tooth plate (12) is L, dentiform gasket (11) and tooth plate (12) often adjust a sawtooth, feeler lever have adjusted �� degree, ��, L, there is following relation in R:
Wherein �� is degree of regulation, and unit is degree; L is dentiform gasket and tooth plate tooth pitch, and unit is millimeter; R is that center of rotation arrives stay bolt axial line distance, and unit is millimeter; Clamping screw II (8), the sawtooth of dentiform gasket (11) and tooth plate (12) is meshed, and completes fixing after feeler lever angular adjustment.
2. the angle adjusting mechanism of a kind of wing outer end as claimed in claim 1 feeler lever, it is characterised in that: the sawtooth of described dentiform gasket (11) and tooth plate (12) is lance tooth.
3. the angle adjusting mechanism of a kind of wing outer end as claimed in claim 1 feeler lever, it is characterised in that: FE Tiler (6) is semicircle.
4. the angle adjusting mechanism of a kind of wing outer end as claimed in claim 1 feeler lever, it is characterised in that: the space that when adjusting for feeler lever, bolt II (8) is movable of support (9) and the upper processing of tooth plate (12) is Long Circle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201410588861.6A CN105620774B (en) | 2014-10-28 | 2014-10-28 | A kind of angle adjusting mechanism of wing outer end feeler lever |
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CN201410588861.6A CN105620774B (en) | 2014-10-28 | 2014-10-28 | A kind of angle adjusting mechanism of wing outer end feeler lever |
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CN105620774A true CN105620774A (en) | 2016-06-01 |
CN105620774B CN105620774B (en) | 2017-09-26 |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874616A (en) * | 1973-07-02 | 1975-04-01 | Us Army | Electrostatic field measuring device |
US4428549A (en) * | 1980-10-24 | 1984-01-31 | British Aerospace Public Limited Company | Arrangements for mounting a probe on an aircraft |
CN203638103U (en) * | 2013-12-12 | 2014-06-11 | 哈尔滨飞机工业集团有限责任公司 | Tail feeler lever of aeromagnetic holoaxial gradient plane |
CN203638104U (en) * | 2013-12-12 | 2014-06-11 | 哈尔滨飞机工业集团有限责任公司 | Aircraft wingtip probe |
-
2014
- 2014-10-28 CN CN201410588861.6A patent/CN105620774B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874616A (en) * | 1973-07-02 | 1975-04-01 | Us Army | Electrostatic field measuring device |
US4428549A (en) * | 1980-10-24 | 1984-01-31 | British Aerospace Public Limited Company | Arrangements for mounting a probe on an aircraft |
CN203638103U (en) * | 2013-12-12 | 2014-06-11 | 哈尔滨飞机工业集团有限责任公司 | Tail feeler lever of aeromagnetic holoaxial gradient plane |
CN203638104U (en) * | 2013-12-12 | 2014-06-11 | 哈尔滨飞机工业集团有限责任公司 | Aircraft wingtip probe |
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