CN207658050U - A kind of helicopter pitch fast leveling component - Google Patents

A kind of helicopter pitch fast leveling component Download PDF

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Publication number
CN207658050U
CN207658050U CN201721871674.4U CN201721871674U CN207658050U CN 207658050 U CN207658050 U CN 207658050U CN 201721871674 U CN201721871674 U CN 201721871674U CN 207658050 U CN207658050 U CN 207658050U
Authority
CN
China
Prior art keywords
leveling
mounting plate
support column
main shaft
helicopter
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
Application number
CN201721871674.4U
Other languages
Chinese (zh)
Inventor
么世广
童庆禧
华棣
于本水
薛永琪
张立福
杨航
张洪明
吴太夏
岑怡
杨磊
王斌
郝强
刘学
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.)
TIANJIN SANYAO AEROSPACE SCIENCE AND TECHNOLOGY DEVELOPMENT Co Ltd
Original Assignee
TIANJIN SANYAO AEROSPACE SCIENCE AND TECHNOLOGY DEVELOPMENT 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 TIANJIN SANYAO AEROSPACE SCIENCE AND TECHNOLOGY DEVELOPMENT Co Ltd filed Critical TIANJIN SANYAO AEROSPACE SCIENCE AND TECHNOLOGY DEVELOPMENT Co Ltd
Priority to CN201721871674.4U priority Critical patent/CN207658050U/en
Application granted granted Critical
Publication of CN207658050U publication Critical patent/CN207658050U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of helicopter pitch fast leveling component, including mounting plate and leveling board, and the leveling board is secured transverse to the top of mounting plate, and the mounting plate is for leveling board to be fixed on main shaft;The upper surface of the leveling board is vertically equipped with the identical support column of multiple height, and the support column is cylindrical structure, and the distance of the axis of the axis of the support column to main shaft is all identical, and the upper surface of multiple support columns is all in one plane.Helicopter pitch fast leveling modular construction described in the utility model is simple, it is only necessary to be adsorbed by magnet, without complicated installing and dismounting process, leveling is rapid, time saving and energy saving, effectively raises the efficiency of pitch leveling.

Description

A kind of helicopter pitch fast leveling component
Technical field
The utility model belongs to helicopter equipment technical field, more particularly, to a kind of helicopter pitch fast leveling group Part.
Background technology
Pitch be helicopter flight steerable system transmit important component, may be implemented helicopter in flight course to The offset of any directions such as front, rear, left and right must give pitch to keep the deviation angle of helicopter more acurrate before Leveling is carried out, the existing most structure of pitch leveling component is complex, and leveling is slower.
Invention content
In view of this, the utility model is directed to a kind of helicopter pitch fast leveling component, it is existing to solve Leveling modular construction is complicated, the slower situation of leveling.
In order to achieve the above objectives, the technical solution of the utility model is realized in:
A kind of helicopter pitch fast leveling component, including mounting plate and leveling board, the leveling board are secured transverse to The top of mounting plate, the mounting plate is for leveling board to be fixed on main shaft;
The upper surface of the leveling board is vertically equipped with the identical support column of multiple height, and the support column is cylinder knot The distance of structure, the axis of the axis of the support column to main shaft is all identical, and the upper surface of multiple support columns is all put down at one On face.
Further, the support column is three.
Further, the leveling board is V-type plate, and the crotch of the V-type plate is arcuate structure, the arcuate structure patch Main shaft installation is closed, the apex in V-type plate is arranged in three support columns.
Further, the mounting plate is c-type plate, and the recess side of the c-type plate is arc groove, the arc groove Diameter is identical as the diameter of main shaft.
Further, the outside of the mounting plate is equipped with strong magnets.
Compared with the existing technology, helicopter pitch fast leveling component described in the utility model has the advantage that:
Helicopter pitch fast leveling modular construction described in the utility model is simple, it is only necessary to be inhaled by magnet Attached, without complicated installing and dismounting process, leveling is rapid, time saving and energy saving, effectively raises the efficiency of pitch leveling.
Description of the drawings
The attached drawing for constituting the part of the utility model is used to provide a further understanding of the present invention, this practicality is new The illustrative embodiments and their description of type are not constituted improper limits to the present invention for explaining the utility model. In attached drawing:
Fig. 1 is the helicopter pitch fast leveling component overall structure diagram described in the utility model embodiment;
Fig. 2 is the helicopter pitch fast leveling component bottom view described in the utility model embodiment.
Reference sign:
1- leveling boards;11- support columns;2- mounting plates;21- strong magnets;3- main shafts.
Specific implementation mode
It should be noted that in the absence of conflict, the feature in the embodiments of the present invention and embodiment can To be combined with each other.
In the description of the present invention, it should be understood that term "center", " longitudinal direction ", " transverse direction ", "upper", "lower", The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of describing the present invention and simplifying the description, rather than indicate Or imply that signified device or element must have a particular orientation, with specific azimuth configuration and operation, therefore cannot understand For limitations of the present invention.In addition, term " first ", " second " etc. are used for description purposes only, and should not be understood as indicating Or it implies relative importance or implicitly indicates the quantity of indicated technical characteristic." first ", " second " etc. are defined as a result, Feature can explicitly or implicitly include one or more this feature.It is in the description of the present invention, unless another It is described, the meaning of " plurality " is two or more.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally Connection;It can be mechanical connection, can also be electrical connection;Can be directly connected, can also indirectly connected through an intermediary, It can be the connection inside two elements.For the ordinary skill in the art, on being understood by concrete condition State the concrete meaning of term in the present invention.
The utility model will be described in detail below with reference to the accompanying drawings and embodiments.
Such as Fig. 1, shown in Fig. 2, a kind of helicopter pitch fast leveling component, including mounting plate 2 and leveling board 1, it is described Leveling board 1 is secured transverse to the top of mounting plate 2, and the mounting plate 2 is used to leveling board 1 being fixed on main shaft 3;
The upper surface of the leveling board 1 is vertically equipped with the identical support column 11 of multiple height, and the support column 11 is cylinder The distance of body structure, the axis of the axis of the support column 11 to main shaft 3 is all identical, and the upper surface of multiple support columns 11 is all In one plane.
The support column 11 is three.When leveling, mounting plate 2 is adsorbed on main shaft 3, the upper surface of three support columns 11 It is all bonded with the lower section of pitch, has both realized the leveling of pitch, it is easy to operate, it is easy to use, effectively raise leveling Efficiency.
The leveling board 1 is V-type plate, and the crotch of the V-type plate is arcuate structure, and the arcuate structure is bonded main shaft 3 The apex in V-type plate is arranged in installation, three support columns 11.
The mounting plate 2 is c-type plate, and the recess side of the c-type plate is arc groove, the diameter of the arc groove and master The diameter of axis 3 is identical.The outside of the mounting plate 2 is equipped with strong magnets 21.Using magnet leveling, complicated installation is needed not move through Disassembly process effectively raises pitch leveling speed.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model Protection domain within.

Claims (5)

1. a kind of helicopter pitch fast leveling component, it is characterised in that:Including mounting plate (2) and leveling board (1), the tune Tablet (1) is secured transverse to the top of mounting plate (2), and the mounting plate (2) is used to leveling board (1) being fixed on main shaft (3);
The upper surface of the leveling board (1) is vertically equipped with the identical support column of multiple height (11), and the support column (11) is circle The distance of column structure, the axis of the axis of the support column (11) to main shaft (3) is all identical, multiple support columns (11) Upper surface is all in one plane.
2. helicopter pitch fast leveling component according to claim 1, it is characterised in that:The support column (11) is Three.
3. helicopter pitch fast leveling component according to claim 2, it is characterised in that:The leveling board (1) is V The crotch of template, the V-type plate is arcuate structure, and the arcuate structure fitting main shaft (3) is installed, and three support columns (11) set Set the apex in V-type plate.
4. helicopter pitch fast leveling component according to claim 1, it is characterised in that:The mounting plate (2) is C The recess side of template, the c-type plate is arc groove, and the diameter of the arc groove is identical as the diameter of main shaft (3).
5. helicopter pitch fast leveling component according to claim 4, it is characterised in that:The mounting plate (2) Outside is equipped with strong magnets (21).
CN201721871674.4U 2017-12-27 2017-12-27 A kind of helicopter pitch fast leveling component Expired - Fee Related CN207658050U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721871674.4U CN207658050U (en) 2017-12-27 2017-12-27 A kind of helicopter pitch fast leveling component

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721871674.4U CN207658050U (en) 2017-12-27 2017-12-27 A kind of helicopter pitch fast leveling component

Publications (1)

Publication Number Publication Date
CN207658050U true CN207658050U (en) 2018-07-27

Family

ID=62943900

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721871674.4U Expired - Fee Related CN207658050U (en) 2017-12-27 2017-12-27 A kind of helicopter pitch fast leveling component

Country Status (1)

Country Link
CN (1) CN207658050U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109018426A (en) * 2018-09-12 2018-12-18 北京清航紫荆装备科技有限公司 A kind of helicopter pitch leveller

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109018426A (en) * 2018-09-12 2018-12-18 北京清航紫荆装备科技有限公司 A kind of helicopter pitch leveller

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Legal Events

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180727

Termination date: 20181227