CN109018426A - A kind of helicopter pitch leveller - Google Patents
A kind of helicopter pitch leveller Download PDFInfo
- Publication number
- CN109018426A CN109018426A CN201811063222.2A CN201811063222A CN109018426A CN 109018426 A CN109018426 A CN 109018426A CN 201811063222 A CN201811063222 A CN 201811063222A CN 109018426 A CN109018426 A CN 109018426A
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- CN
- China
- Prior art keywords
- leveling
- sleeve
- pawl
- pitch
- helicopter
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of helicopter pitch levellers, comprising: the sleeve for being sheathed in the mast of helicopter；It is connected with sleeve, for at least three not conllinear leveling pawls that offset of leveling face of the pitch with helicopter, what all leveling pawls were used to offset with leveling face, which offset, holds coplanar, and all axis of plane and sleeve where end that offset are vertically arranged.The structure of the helicopter pitch leveller is simple, it is easy to use, and guarantee the verticality of pitch and mast by the verticality of leveling pawl and sleeve, precision is high, can guarantee once to be adjusted in place, low to the skill requirement of technical staff, substantially reduce the overall time of pitch leveling, it is significant for the debugging of helicopter to many conveniences of leveling calibration tape of pitch, solve a key factor for restricting Helicopter Development all the time.
Description
Technical field
The present invention relates to aircraft technical field of auxiliary equipment, level more specifically to a kind of helicopter pitch
Device.
Background technique
Important spare part of the pitch as helicopter is mainly used for transmitting helicopter and flies during helicopter flight
The lift of row steerable system, so that helicopter can all around vert.
During the assembling of new machine or aircraft bombing are repaired, need to carry out leveling calibration to pitch, to ensure that helicopter is inclined
Move the accuracy of angle.
However, pitch levelling problems are always the technical problem in helicopter debugging.There is no special in the prior art
Leveling tool, usually human eye is estimated, or is measured using ruler, or temporarily make easy leveling tool by oneself, for example, using
The steel wire of coiling is set on main shaft, and make from one end of coiling steel wire stretch out and bend elbow as leveling needle successively with incline
Multiple point contacts on swash plate, the levelness of pitch is calibrated with this.As can be seen that the side of this interim production simple tooling
Method needs temporarily to find suitable part and tool, production trouble, and precision is lower, the circularity for the tooling made, coaxial
Degree etc. does not often reach requirement, and higher to the skill requirement of technical staff.
In conclusion it is high and conveniently carry out the helicopter pitch tune of leveling calibration to pitch how to provide a kind of precision
Flat device, is a problem to be solved by those skilled in the art.
Summary of the invention
In view of this, the object of the present invention is to provide a kind of helicopter pitch leveller, helicopter pitch leveling
The structure of device is simple, easy to use, and precision is high, to many conveniences of leveling calibration tape of pitch.
To achieve the goals above, the invention provides the following technical scheme:
A kind of helicopter pitch leveller, comprising:
Sleeve for being sheathed in the mast of helicopter；
Be connected with the sleeve, for the pitch with the helicopter leveling face offset it is at least three not conllinear
Pawl is leveled, all leveling pawls are used to hold with offseting of offseting of the leveling face coplanar and flat where all ends that offset
Face and the axis of the sleeve are vertically arranged.
Preferably, the leveling pawl is connected by connector with the sleeve, and the connector and sleeve socket are solid
Fixed, the leveling pawl is fixedly arranged on the peripheral part of the connector.
Preferably, the connector include suit portion for being sheathed on the sleeve and be connected with the suit portion and
The extension being connected is corresponded with the leveling pawl.
Preferably, the leveling pawl is that arc levels pawl, and the end that offsets of arc leveling pawl protrude from it is described
Extension offsets the one side at end described in.
Preferably, the quantity of the leveling pawl is four.
Preferably, four leveling pawls are uniformly distributed along the circumferential direction of the sleeve.
Preferably, four leveling pawls arrive being equidistant for the axis of the sleeve respectively.
Preferably, the sleeve includes 7075 aviation aluminum sleeves, silicon carbide fibre matter sleeve or carbon fiber matter sleeve；Institute
Stating connector includes 7075 aviation aluminum connectors, silicon carbide fibre matter connector or carbon fiber matter connector；The leveling pawl
Pawl is leveled including 7075 aviation aluminums leveling pawl, silicon carbide fibre matter leveling pawl or carbon fiber matter.
Preferably, the length range of the sleeve is 0.5 times to 3 times of the sleeve diameter.
Preferably, the end that offsets is equipped with wear-resistant coating.
Helicopter pitch leveller provided by the invention makes sleeve in use, sleeve is set in mast
Then the axis collinear of axis and mast adjusts the position of pitch, specifically can be by adjusting the company being connected with pitch
The length of bar adjusts the position of pitch, tilts alternatively, being changed by the initial position for adjusting the steering engine being connected with connecting rod
The position of disk makes the leveling face of pitch and the end that offsets of all leveling pawls offset, since all offseting for pawl of leveling hold institute
It is vertically arranged in the axis of plane and sleeve, therefore, when the end that offsets in the leveling face of pitch and all leveling pawls offsets,
The leveling face that pitch can be released is vertical with the axis of mast, so that pitch be made to level.
The structure of the helicopter pitch leveller is simple, easy to use, and by leveling pawl and sleeve verticality come
Guarantee the verticality of pitch and mast, precision is high, can guarantee once to be adjusted in place, to the skill requirement of technical staff
It is low, the overall time of pitch leveling is substantially reduced, to many conveniences of leveling calibration tape of pitch, for helicopter
It is significant for debugging, solve a key factor for restricting Helicopter Development all the time.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 is the structural schematic diagram of helicopter pitch leveller specific embodiment provided by the present invention；
Fig. 2 is the top view of helicopter pitch leveller shown in Fig. 1；
Fig. 3 is the side view of helicopter pitch leveller shown in Fig. 1.
Appended drawing reference of the Fig. 1 into Fig. 3 is as follows:
1 it is sleeve, 2 be leveling pawl, 3 be connector, 31 is extension.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Core of the invention is to provide a kind of helicopter pitch leveller, the structure letter of the helicopter pitch leveller
It is single, it is easy to use, and precision is high, to many conveniences of leveling calibration tape of pitch.
Fig. 1-Fig. 3 is please referred to, Fig. 1 is that the structure of helicopter pitch leveller specific embodiment provided by the present invention is shown
It is intended to；Fig. 2 is the top view of helicopter pitch leveller shown in Fig. 1；Fig. 3 is helicopter pitch leveller shown in Fig. 1
Side view.
The present invention provides a kind of helicopter pitch leveller, including sleeve 1 and be connected with sleeve 1 several are conllinear
Leveling pawl 2, sleeve 1 is used to be sheathed on the mast of helicopter, to guarantee the axis of sleeve 1 and the axis of mast
Collinearly；Leveling pawl 2 is used to offset with the leveling face of the pitch of helicopter, is calibrated with the leveling face to pitch.It is all
Leveling pawl 2 is used to hold with offseting of offseting of leveling face coplanar, and plane is vertical with the axis of sleeve 1 where all ends that offset sets
It sets.
That is, the present invention is by guaranteeing that the verticality of offset end and 1 axis of sleeve of leveling pawl 2 guarantees pitch
With the verticality of mast, and guarantee by adjusting the levelness of pitch the verticality of pitch and mast.
It is understood that sleeve 1 is mainly used for being socketed with mast, therefore, the internal diameter of sleeve 1 is mainly by revolving
The outer diameter of wing main shaft determines that the internal diameter of sleeve 1 need to be matched with the outer diameter of mast, to avoid sleeve 1 and rotor
After main shaft socket, sleeve 1 shakes in mast, influences the concentricity of sleeve 1 Yu mast.
While guaranteeing the axis collinear of 1 axis of sleeve and mast, it is contemplated that property problem easy for installation, preferably
Ground, sleeve 1 are for the sleeve 1 with mast transition fit.
It is understood that sleeve 1 and the cooperation of mast are closer, then position of the sleeve 1 relative to mast
It is less susceptible to change, that is, more can guarantee the concentricity of sleeve 1 Yu mast；Simultaneously as the helicopter pitch leveller
Be mainly used for pitch leveling calibration, pitch leveling after, which need to be removed, therefore, in order to guarantee sleeve 1 with
Mast to neutral and concentricity, while installation easy to disassemble, present invention is preferably used in mast transition fit
Sleeve 1.
For the ease of installation, it is preferable that the end face inner bore of sleeve 1 is equipped with chamfering.
Leveling pawl 2 is mainly used for calibrating the levelness in the leveling face of pitch, determines that one is put down by not conllinear 3 points
The theoretical knowledge in face is it is found that the quantity of leveling pawl 2 is at least three, and at least three leveling pawls 2 are not conllinear, to ensure all tune
Flat pawl 2 is capable of forming a plane, that is, offset plane where end.The present embodiment is to the relative positional relationship (example between leveling pawl 2
Such as, the angle between adjacent leveling pawl 2) it is not specifically limited, as long as can guarantee that at least three leveling pawls 2 are not conllinear.
It is understood that the end that offsets of leveling pawl 2, for offseting with the leveling face of pitch, therefore, leveling pawl 2 is opposite
The distance of 1 axis of sleeve is determined by the leveling face of pitch with respect to the axial line distance of mast, to ensure to level the phase of pawl 2
It can offset with the leveling face of pitch to end.
The present invention to leveling pawl 2 and its end that offsets specific structure without limitation, for example, leveling pawl 2 can be column knot
Structure, the end that offsets can be tip-like or ball head-like structure, that is, the leveling face of leveling pawl 2 and pitch is point contact；Certainly,
Pawl 2 or block structure are leveled, offset end or planar structure, that is, leveling pawl 2 and the leveling face of pitch are
Face contact；Specifically, it levels pawl 2 and its end that offsets can be designed as different shape and structure according to actual needs, for example,
The concrete shape at the end that offsets can also be determined according to the concrete shape in leveling face, so that the localized contact at offset end and leveling face
Shape matches.
Preferably, the end that offsets of pawl 2 is leveled as closing the binding face to offset with leveling face paste.That is, leveling pawl 2 and inclining
The leveling face of swash plate is plane-plane contact.
End and level the contact precision in face to guarantee to offset, it is preferable that binding face be for leveling face radially-wide
The binding face being bonded completely on degree.That is, in the present embodiment, the size at the end that offsets by pitch leveling face radial ruler
It is very little to determine, to guarantee that the leveling face of pitch is bonded completely with the binding face of leveling pawl 2, thus the level in the leveling face of raising
Degree.
It should be noted that all ends that offset need to be coplanar, to the calibration benchmark as pitch leveling face, to guarantee to incline
The levelness of swash plate.
Further, all offset plane and the axis of sleeve 1 where end are vertically arranged, leveling face and institute when pitch
End is offseted when offseting, then shows that pitch is vertical with 1 axis of sleeve, sleeve 1 is sheathed in mast, that is, sleeve 1
The axis collinear of axis and mast, therefore, all offset plane and the axis of sleeve 1 where end are vertically arranged, it is ensured that
The leveling face of pitch is vertical with the axis of mast.
It should be noted that the present invention is not specifically limited leveling pawl 2 and the connection type of sleeve 1, leveling pawl 2 can be with
It is connected directly, can also be indirectly connected with sleeve 1, as long as can guarantee the leveling face phase at the offset end and pitch of leveling pawl 2
It supports.
In use, sleeve 1 is set in mast, make the axis of sleeve 1 and the axis collinear of mast, then
The position of pitch is adjusted, the position of pitch can be specifically adjusted by adjusting the length for the connecting rod being connected with pitch, or
Person changes the position of pitch by adjusting the initial position for the steering engine being connected with connecting rod, makes leveling face and the institute of pitch
There is the end that offsets of leveling pawl 2 to offset, since offset plane and the axis of sleeve 1 where end of all leveling pawls 2 are vertically arranged,
Therefore, when the end that offsets in the leveling face of pitch and all leveling pawls 2 offsets, leveling face and the rotor of pitch can be released
The axis of main shaft is vertical, so that pitch be made to level.
The structure of the helicopter pitch leveller is simple, easy to use, and passes through the verticality of leveling pawl 2 and sleeve 1
Guarantee the verticality of pitch and mast, precision is high, can guarantee once to be adjusted in place, want to the technical ability of technical staff
It asks low, the overall time of pitch leveling is substantially reduced, to many conveniences of leveling calibration tape of pitch, for helicopter
Debugging for it is significant, solve all the time restrict Helicopter Development a key factor.
In view of the specific implementation of the connection type of leveling pawl 2 and sleeve 1, on the basis of above-described embodiment, leveling
Pawl 2 is connected by connector 3 with sleeve 1, and connector 3 is sleeved and fixed with sleeve 1, and leveling pawl 2 is fixedly arranged on the periphery of connector 3
Portion.
That is, the present embodiment realizes therefore the connection of leveling pawl 2 and sleeve 1 can pass through by connector 3
Change the radial dimension of connector 3 to change the distance of leveling 2 relative sleeve of pawl 1 axis, is offseted with this to guarantee to level pawl 2
End can be contacted with the leveling face of pitch to offset.
The present embodiment to the specific structure of connector 3 and without limitation, as long as connection leveling pawl 2 and sleeve 1 can be played
Effect, and guarantee level 2 relative sleeve of pawl, 1 axis positional relationship.
The present embodiment does not do connector 3 and the fixed form and connector 3 and the fixed form of leveling pawl 2 of sleeve 1
It is specific to limit.For example, connector 3 can be sleeved and fixed with sleeve 1 by transition fit or interference fit, can also weld solid
It is fixed.Leveling pawl 2 can be fixedly arranged on the peripheral part of connector 3 by fasteners such as bolts, can also be soldered to the periphery of connector 3
Portion.
In view of simple and the being easy to implement property of 3 specific structure of connector, on the basis of above-described embodiment, connector
3 include suit portion for being sheathed on sleeve 1 and are connected with suit portion and correspond the extension being connected with leveling pawl 2
31。
That is, connector 3 in the present embodiment is the lantern ring with several extensions 31, the inner hole of lantern ring (
That is suit portion) it is sheathed on the peripheral part of sleeve 1, realization connector 3 is sleeved and fixed with sleeve 1；Several extensions of lantern ring
31 are connected with the leveling one-to-one correspondence of pawl 2 respectively, realize connector 3 and level the connection of pawl 2.
It can be seen that this connector 3 is the connection structure of frame clsss, the not entity structure of disc type, therefore,
Alleviate the overall weight of helicopter pitch leveller.
In view of leveling the specific structure of pawl 2, on the basis of above-described embodiment, leveling pawl 2 is arc leveling pawl, and
The end that offsets of arc leveling pawl protrudes from one side of the extension 31 towards the end that offsets.
It is understood that arc leveling pawl can further mitigate the overall weight of helicopter pitch leveller.
Arc leveling pawl offset end protrude from one side of the extension 31 towards the end that offsets, that is, respectively leveling pawl 2 with connect
Part 3 forms concave inward structure and avoids 3 extension of connector, 31 court to guarantee that the leveling face of pitch offsets with the end in contact that respectively offsets
It offsets with the contact at the end that offsets to the plane of exchanging on one side at the end that offsets and causes to interfere.
Stability in view of the simplicity of leveller this body structure and when adjusting the leveling face of pitch, above-mentioned any
On the basis of one embodiment, the quantity of leveling pawl 2 is four.
It is understood that the quantity of leveling pawl 2 is more, then the structure of leveller is more complicated, weight is bigger, therefore, needs
The fewer the quantity of leveling pawl 2 the better on the basis of guaranteeing to level pitch；Simultaneously as four point contacts are usually relatively more steady
Fixed, convenient for the leveling of pitch, therefore, the quantity of the leveling pawl 2 in the present embodiment is four.
Accordingly, the quantity of the extension 31 of the connector 3 in the present embodiment is four, and four extensions 31 are along sleeve 1
Circumferential direction be uniformly distributed, that is, the connector 3 in the present embodiment be cross connecting element.
In view of the harmony of leveller structure, on the basis of above-described embodiment, four leveling pawls 2 are along sleeve 1
Circumferentially it is uniformly distributed.That is, the angle of four leveling pawls 2 between any two is 90 °, four leveling pawls 2 form cross-shaped structure,
This can guarantee the centre symmetry of leveller structure and the whole uniformity of gravity.Also, it is understood that pitch is logical
It is often cross plate, four leveling pawls 2 can just be directed at four leveling points of cross pitch.
In order to guarantee to level precision, on the basis of above-described embodiment, four leveling pawls 2 arrive the axis of sleeve 1 respectively
Be equidistant.This can guarantee that the end that offsets of four leveling pawls 2 is respectively positioned on same anchor ring, to make on pitch leveling face
It contacts the part to offset with each leveling pawl 2 to be located on the same anchor ring of pitch, to guarantee the accuracy of pitch leveling.
In order to further mitigate the overall weight of helicopter pitch leveller, on the basis of above-mentioned any one embodiment
On, sleeve 1 includes 7075 aviation aluminum sleeves, silicon carbide fibre matter sleeve or carbon fiber matter sleeve；Connector 3 includes 7075
Aviation aluminum connector, silicon carbide fibre matter connector or carbon fiber matter connector；Pawl 2 is leveled to level including 7075 aviation aluminums
Pawl, silicon carbide fibre matter leveling pawl or carbon fiber matter level pawl.
It is understood that 7075 aviation aluminum components, silicon carbide fibre matter components or carbon fiber matter components
Specific gravity is small, specific strength and specific modulus are big, and therefore, quality is small, light-weight.
Influence in view of length of fit to sleeve 1 and the fit quality of mast, in above-mentioned any one embodiment
Basis on, the length range of sleeve 1 is 0.5 times to 3 times of 1 internal diameter of sleeve.
It should be noted that sleeve 1 is used to be socketed with mast, therefore, the internal diameter of sleeve 1 and mast
Outer diameter is consistent.That is, the length range of sleeve 1 is the diameter of axle of the mast for matching with sleeve 1 in the present embodiment
0.5 times to 3 times of size.
It is understood that the length of sleeve 1 is longer, then sleeve 1 and the length of fit of mast are longer.Sleeve 1
Too in short-term, after sleeve 1 is sheathed on mast, sleeve 1 slightly shakes length dimension, will lead to sleeve 1 relative to mast
Axis have biggish offset error；When the length dimension of sleeve 1 is too long, it is not easy to dismount.Therefore, the present embodiment middle sleeve
1 length range is 0.5 times to 3 times of 1 internal diameter of sleeve.
Preferably, the length dimension of sleeve 1 is consistent with the internal diameter of sleeve 1, that is, the length dimension and use of sleeve 1
It is consistent in the diameter of axle of mast cooperated with sleeve 1.
In order to improve the service life of helicopter pitch leveller, on the basis of above-mentioned any one embodiment,
End is offseted equipped with wear-resistant coating.
In order to improve the leveling precision of pitch, it is preferable that leveling pawl 2 offset end setting for incude offset end with
The pressure sensor of contact pressure between leveling face, pressure sensor are connected with controller, and controller is tilted with for adjusting
The pull rod of disk is connected, alternatively, controller is connected with the steering engine for being connected with connecting rod.
That is, the present embodiment detects the contact stress in leveling face with the end that offsets by pressure sensor, and will pressure
The stress signal of force snesor detection is sent to controller, makes controller according to the received stress feelings for contacting the position that offsets
Condition to send control instruction to connecting rod or steering engine, so that connecting rod or steering engine be made accurately to adjust the position of pitch, guarantees
The accuracy of pitch leveling.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.
Helicopter pitch leveller provided by the present invention is described in detail above.It is used herein specifically
Principle and implementation of the present invention are described for a example, the present invention that the above embodiments are only used to help understand
Method and its core concept.It should be pointed out that for those skilled in the art, not departing from original of the invention
, can be with several improvements and modifications are made to the present invention under the premise of reason, these improvement and modification also fall into right of the present invention and want
In the protection scope asked.
Claims (10)
1. a kind of helicopter pitch leveller characterized by comprising
Sleeve (1) for being sheathed in the mast of helicopter；
Be connected with the sleeve (1), for the pitch with the helicopter leveling face offset it is at least three not conllinear
It levels pawl (2), all leveling pawl (2) are used to hold coplanar, and all ends that offset with offseting of offseting of the leveling face
Place plane and the axis of the sleeve (1) are vertically arranged.
2. helicopter pitch leveller according to claim 1, which is characterized in that the leveling pawl (2) passes through connection
Part (3) is connected with the sleeve (1), and the connector (3) is sleeved and fixed with the sleeve (1), and the leveling pawl (2) is fixedly arranged on
The peripheral part of the connector (3).
3. helicopter pitch leveller according to claim 2, which is characterized in that the connector (3) includes being used for
The suit portion that is sheathed on the sleeve (1) and it is connected with the suit portion and corresponds with leveling pawl (2) and be connected
Extension (31).
4. helicopter pitch leveller according to claim 3, which is characterized in that the leveling pawl (2) is arc tune
Flat pawl, and the end that offsets of arc leveling pawl protrudes from the one side at the end that offsets described in the extension (31) direction.
5. helicopter pitch leveller according to claim 1-4, which is characterized in that the leveling pawl (2)
Quantity be four.
6. helicopter pitch leveller according to claim 5, which is characterized in that four leveling pawls (2) are along institute
The circumferential direction for stating sleeve (1) is uniformly distributed.
7. helicopter pitch leveller according to claim 5, which is characterized in that four leveling pawls (2) are respectively
Axis to the sleeve (1) is equidistant.
8. helicopter pitch leveller according to claim 1-4, which is characterized in that sleeve (1) packet
Include 7075 aviation aluminum sleeves, silicon carbide fibre matter sleeve or carbon fiber matter sleeve；The connector (3) includes 7075 aviation aluminium
Matter connector, silicon carbide fibre matter connector or carbon fiber matter connector；The leveling pawl (2) levels including 7075 aviation aluminums
Pawl, silicon carbide fibre matter leveling pawl or carbon fiber matter level pawl.
9. helicopter pitch leveller according to claim 1-4, which is characterized in that the sleeve (1)
Length range is 0.5 times to 3 times of the sleeve (1) internal diameter.
10. helicopter pitch leveller according to claim 1-4, which is characterized in that the end that offsets is set
There is wear-resistant coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811063222.2A CN109018426A (en) | 2018-09-12 | 2018-09-12 | A kind of helicopter pitch leveller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811063222.2A CN109018426A (en) | 2018-09-12 | 2018-09-12 | A kind of helicopter pitch leveller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109018426A true CN109018426A (en) | 2018-12-18 |
Family
ID=64621815
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811063222.2A Pending CN109018426A (en) | 2018-09-12 | 2018-09-12 | A kind of helicopter pitch leveller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109018426A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1076618A (en) * | 1978-06-05 | 1980-04-29 | Robert C. Anderson | Leveling clamp |
| US5029405A (en) * | 1989-06-02 | 1991-07-09 | Abbott-Interfast Corporation | Cleat for boot sole and the like |
| WO2012154724A1 (en) * | 2011-05-11 | 2012-11-15 | Imagine Tf, Llc. | Anchoring system with post angular adjustment |
| CN203109582U (en) * | 2013-03-18 | 2013-08-07 | 南车株洲电力机车研究所有限公司 | Brake disc leveling device |
| CN206782110U (en) * | 2017-05-31 | 2017-12-22 | 重庆北方天途无人机有限公司 | Unmanned aerial vehicle body levelling device |
| CN207106939U (en) * | 2017-07-17 | 2018-03-16 | 飞瑞航空科技（江苏）有限公司 | A kind of depopulated helicopter auto-bank unit leveling tool |
| CN207658050U (en) * | 2017-12-27 | 2018-07-27 | 天津三爻航空航天科技发展有限公司 | A kind of helicopter pitch fast leveling component |
| CN208802157U (en) * | 2018-09-12 | 2019-04-30 | 北京清航紫荆装备科技有限公司 | A kind of helicopter pitch leveller |
-
2018
- 2018-09-12 CN CN201811063222.2A patent/CN109018426A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1076618A (en) * | 1978-06-05 | 1980-04-29 | Robert C. Anderson | Leveling clamp |
| US5029405A (en) * | 1989-06-02 | 1991-07-09 | Abbott-Interfast Corporation | Cleat for boot sole and the like |
| WO2012154724A1 (en) * | 2011-05-11 | 2012-11-15 | Imagine Tf, Llc. | Anchoring system with post angular adjustment |
| CN203109582U (en) * | 2013-03-18 | 2013-08-07 | 南车株洲电力机车研究所有限公司 | Brake disc leveling device |
| CN206782110U (en) * | 2017-05-31 | 2017-12-22 | 重庆北方天途无人机有限公司 | Unmanned aerial vehicle body levelling device |
| CN207106939U (en) * | 2017-07-17 | 2018-03-16 | 飞瑞航空科技（江苏）有限公司 | A kind of depopulated helicopter auto-bank unit leveling tool |
| CN207658050U (en) * | 2017-12-27 | 2018-07-27 | 天津三爻航空航天科技发展有限公司 | A kind of helicopter pitch fast leveling component |
| CN208802157U (en) * | 2018-09-12 | 2019-04-30 | 北京清航紫荆装备科技有限公司 | A kind of helicopter pitch leveller |
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