CN204809401U - Circular flexible honeycomb - Google Patents

Circular flexible honeycomb Download PDF

Info

Publication number
CN204809401U
CN204809401U CN201420815170.0U CN201420815170U CN204809401U CN 204809401 U CN204809401 U CN 204809401U CN 201420815170 U CN201420815170 U CN 201420815170U CN 204809401 U CN204809401 U CN 204809401U
Authority
CN
China
Prior art keywords
honeycomb
circular
utility
model
tangent
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.)
Active
Application number
CN201420815170.0U
Other languages
Chinese (zh)
Inventor
曲秀晓
李兴德
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.)
AVIC Research Institute Special Structures Aeronautical Composites
Original Assignee
AVIC Research Institute Special Structures Aeronautical Composites
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 AVIC Research Institute Special Structures Aeronautical Composites filed Critical AVIC Research Institute Special Structures Aeronautical Composites
Priority to CN201420815170.0U priority Critical patent/CN204809401U/en
Application granted granted Critical
Publication of CN204809401U publication Critical patent/CN204809401U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Laminated Bodies (AREA)

Abstract

The utility model belongs to the technical field of combined material, concretely relates to circular flexible honeycomb, the honeycomb is arranged by the tangent quadrature of the circular honeycomb unit of a plurality of and is constituteed, honeycomb unit including two kinds of shapes, the honeycomb unit is star types circular and four yuan of tangent constitutions respectively. The utility model discloses broken through conventional hexagon honeycomb non -deformable's under the circumstances of great camber restriction, utility model's honeycomb has deformability and crooked deformability in the sufficient face, distributing of stress is even during the deformation, has improved simultaneously at vertical plane orientation bearing capacity, has consequently solved the contradiction that honeycomb sandwich structure bore the weight of at face internal strain and off -plate.

Description

A kind of circular flexible honeycomb
Technical field
The utility model belongs to technical field of composite materials, is specifically related to a kind of circular flexible honeycomb.
Background technology
In radome, usually there is a lot of structure to there is larger curvature, in this deep camber situation, still adopt conventional hexagonal shape honeycomb sandwich construction, be difficult to resist the requirement of high-mechanic outside large deformation and face in the face in making and using, easily occur saddle effect.
Utility model content
Technical problem to be solved in the utility model is: the flexibility increasing honeycomb, avoids honeycomb sandwich construction to occur saddle effect when larger curvature.
The technical solution of the utility model is: a kind of circular flexible honeycomb, and described honeycomb is made up of the tangent orthogonal arrangement of several circular cellular units, comprises the cellular unit of two kinds of shapes, and described cellular unit is respectively circle and four and justifies the star-like of tangent compositions.
The beneficial effects of the utility model are: breach conventional hexagonal cell when compared with restriction on-deformable when deep camber, the honeycomb of institute's utility model has sufficient in-plane deformation ability and crooked deformability, during distortion, stress distribution is even, improve in vertical plane direction bearing capacity simultaneously, therefore solve the contradiction that honeycomb sandwich construction carries outside in-plane deformation and face.
Accompanying drawing explanation
Fig. 1 is circular flexible cellular unit schematic diagram;
Fig. 2 is phase cut unit group schematic diagram;
Fig. 3 is star-like cell schematics;
Fig. 4 is circular flexible cellular board schematic diagram.
Embodiment
Below in conjunction with accompanying drawing and case study on implementation, the utility model is described in further detail.
The circular flexible honeycomb of the utility model indication is the circular cell of diameter 6mm, and unit is made up of three layers of aramid fiber honeycomb paper laying impregnation, and unit form as shown in Figure 1.
The cellular board be made up of circular flexible cellular unit as shown in Figure 4.Cellular board is formed by some groups of tangent circular flexible cellular unit orthogonal arrangement, tangent circular flexible cellular unit forms several unit groups and sees Fig. 2, each phase cut unit group forms a star-like unit, 4 limits of star-like unit are 1/4 arc length of four tangent circular flexible honeycomb unit, length and width are circular flexible cellular unit diameter, and star-like unit is shown in Fig. 3.
The circular flexible honeycomb that the utility model provides is compared to existing hexagonal honeycomb structure, and its performance advantage is:
First, stretch modulus in the equivalent face of this circular flexible honeycomb of the utility model ratio of the distortion in unit length (pulling force on unit cross-sectional area with) is 41% of conventional hexagonal cell, under equal large side crops industry (100N ﹒ mm) effect, the total deformation of hexagon cellular structure and circular flexible honeycomb is respectively 6.46mm, 60.5mm, the saddle effect relative deformation ratio of cellular board total deformation (the maximum saddle distortion absolute value with) is respectively 0.315 and 0.075, and visible circular flexible honeycomb is more yielding than hexagon cellular.
The second, the bond area of the circular honeycomb of same specification is 1.3 times of hexagonal cell, improves circular honeycomb in vertical plane direction bearing capacity.

Claims (1)

1. a circular flexible honeycomb, is characterized in that, described honeycomb is made up of the tangent orthogonal arrangement of several circular cellular units, comprises the cellular unit of two kinds of shapes, and described cellular unit is respectively circle and four and justifies the star-like of tangent compositions.
CN201420815170.0U 2014-12-19 2014-12-19 Circular flexible honeycomb Active CN204809401U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420815170.0U CN204809401U (en) 2014-12-19 2014-12-19 Circular flexible honeycomb

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420815170.0U CN204809401U (en) 2014-12-19 2014-12-19 Circular flexible honeycomb

Publications (1)

Publication Number Publication Date
CN204809401U true CN204809401U (en) 2015-11-25

Family

ID=54594174

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420815170.0U Active CN204809401U (en) 2014-12-19 2014-12-19 Circular flexible honeycomb

Country Status (1)

Country Link
CN (1) CN204809401U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105619889A (en) * 2015-12-22 2016-06-01 中国航空工业集团公司济南特种结构研究所 Manufacturing method for round flexible honeycomb

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105619889A (en) * 2015-12-22 2016-06-01 中国航空工业集团公司济南特种结构研究所 Manufacturing method for round flexible honeycomb
CN105619889B (en) * 2015-12-22 2018-07-24 中国航空工业集团公司济南特种结构研究所 A kind of cellular production method of circular flexible

Similar Documents

Publication Publication Date Title
CN101795850B (en) Structural frame of a composite material and aircraft fuselage including such frame
WO2014155293A8 (en) Wind turbine blade root and process for manufacturing a wind turbine blade root
GB201018081D0 (en) Improvements in or relating to composite structures
CN204850239U (en) Former bamboo beam column construction
CN204809401U (en) Circular flexible honeycomb
CN204361276U (en) A kind of waveform flexible honeycomb
CN202329424U (en) Puncture-proof sheet for bulletproof clothing
CN204361278U (en) A kind of recessed hexagon flexible honeycomb structure
CN205244293U (en) Modified star gear
CN205416642U (en) Adjustable honeycomb of modulus
CN206048419U (en) A kind of battenboard hold down gag
CN202573660U (en) Radial aircraft tire
CN102996936A (en) Flange plate combination structure
CN203080804U (en) Support horse-shaped bench for surface rib protection layer
CN203758377U (en) Novel target for archery
CN203202023U (en) Novel bearing body of hollow shaft type hydrostatic bearing
GB2501614A (en) Improvements in and relating to structural tubes
CN205207465U (en) Universal pitch chain
CN202869346U (en) Arc condenser sectional material
CN203651091U (en) Overdrawn-formed aramid honeycomb
CN203212942U (en) Damp curtain paper
CN201843303U (en) Floor stress slot
CN202671797U (en) Special fiber warp knitting fabric
CN202805782U (en) Composite shell fabric of prolivon fibers and silk
CN203510858U (en) Sensor diaphragm

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant