CN105620774A - Angle adjusting mechanism for wing outer end feeler lever - Google Patents

Angle adjusting mechanism for wing outer end feeler lever Download PDF

Info

Publication number
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
Authority
CN
China
Prior art keywords
feeler lever
bolt
tooth plate
oscillating bearing
adjusting mechanism
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.)
Granted
Application number
CN201410588861.6A
Other languages
Chinese (zh)
Other versions
CN105620774B (en
Inventor
陈洲蛟
万昌俊
张余
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin Aircraft Industry Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN201410588861.6A priority Critical patent/CN105620774B/en
Publication of CN105620774A publication Critical patent/CN105620774A/en
Application granted granted Critical
Publication of CN105620774B publication Critical patent/CN105620774B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Pivots And Pivotal Connections (AREA)

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

A kind of angle adjusting mechanism of wing outer end feeler lever
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:
α = 2 × arcsin L 2 R
�� 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:
α = 2 × arcsin L 2 R
�� 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.
CN201410588861.6A 2014-10-28 2014-10-28 A kind of angle adjusting mechanism of wing outer end feeler lever Active CN105620774B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410588861.6A CN105620774B (en) 2014-10-28 2014-10-28 A kind of angle adjusting mechanism of wing outer end feeler lever

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410588861.6A CN105620774B (en) 2014-10-28 2014-10-28 A kind of angle adjusting mechanism of wing outer end feeler lever

Publications (2)

Publication Number Publication Date
CN105620774A true CN105620774A (en) 2016-06-01
CN105620774B CN105620774B (en) 2017-09-26

Family

ID=56036201

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410588861.6A Active CN105620774B (en) 2014-10-28 2014-10-28 A kind of angle adjusting mechanism of wing outer end feeler lever

Country Status (1)

Country Link
CN (1) CN105620774B (en)

Citations (4)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
CN105620774B (en) 2017-09-26

Similar Documents

Publication Publication Date Title
CN109211068A (en) Angle measurement unit
CN206912464U (en) Stud welding servicing unit
CN105620774A (en) Angle adjusting mechanism for wing outer end feeler lever
CN205861067U (en) With magnetic azimuth location can self-calibration teleclinometer calibrating installation
JP2013217889A (en) Slide-type vehicle frame hole position measuring apparatus
CN103776354B (en) Concentric detector
CN202753062U (en) Cycloid water turbine installation retainer with measurement function
JP2016166743A (en) Fixture of anemometer
CN104458090B (en) Sidewall contact device of logging device universal measurement device
CN207779932U (en) A kind of pipeline radiographic inspection rack
CN104389366B (en) A kind of point-supporting curtain universal fixture
CN102729181B (en) Cycloid water turbine installation retainer with measuring function
CN105318153A (en) Universal mounting mechanism for supporting, fixing, mounting and debugging equipment
CN206095099U (en) Steel plate length inspects tool
RU136455U1 (en) DEVICE FOR STATIC TESTING OF SOIL CARRYING ABILITY
CN205015033U (en) Flowmeter support
CN214538088U (en) Ultrasonic flowmeter probe positioning device
CN203260711U (en) Satellite antenna frame with pointer gasket
CN209295810U (en) Vernier caliper
CN107882874B (en) Detachable and rotatable guide rail type aligning device
CN109482603A (en) Frock clamp and crystal clamping and loading method
RU144336U1 (en) TRIPOD FOR MEASURING LINEAR PARTS OF PARTS
CN203894247U (en) ADCP sensor underwater verticality adjusting device
CN207830935U (en) A kind of gas flowmeter fixing device
CN204202506U (en) A kind of orientable tape measure

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant