CN115077847A - Guide support device for wind tunnel body - Google Patents

Guide support device for wind tunnel body Download PDF

Info

Publication number
CN115077847A
CN115077847A CN202210995810.XA CN202210995810A CN115077847A CN 115077847 A CN115077847 A CN 115077847A CN 202210995810 A CN202210995810 A CN 202210995810A CN 115077847 A CN115077847 A CN 115077847A
Authority
CN
China
Prior art keywords
wind tunnel
connecting plate
sliding
end guide
guide piece
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
CN202210995810.XA
Other languages
Chinese (zh)
Other versions
CN115077847B (en
Inventor
刘新朝
袁野
刘振德
崔晓春
邢汉奇
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 Shenyang Aerodynamics Research Institute
Original Assignee
AVIC Shenyang Aerodynamics Research Institute
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 Shenyang Aerodynamics Research Institute filed Critical AVIC Shenyang Aerodynamics Research Institute
Priority to CN202210995810.XA priority Critical patent/CN115077847B/en
Publication of CN115077847A publication Critical patent/CN115077847A/en
Application granted granted Critical
Publication of CN115077847B publication Critical patent/CN115077847B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details

Abstract

The invention relates to a guide support device for a wind tunnel body, and belongs to the technical field of aerodynamic wind tunnel tests. The problem that the wind tunnel is difficult to bear the lateral force of a large wind tunnel when the wind tunnel is installed in the traditional bridge support form is solved. The wind tunnel comprises a lower connecting plate, a lower end guide piece, an upper end guide piece, a connecting plate and a sliding body, wherein the lower connecting plate is connected with a pre-buried steel plate, the lower connecting plate is connected with the sliding body through the lower end guide piece, the upper portion of the upper end guide piece is provided with the connecting plate, the connecting plate is connected with a wind tunnel body, the center of the upper end guide piece is provided with a sliding groove, and the upper portion of the sliding body is connected with the upper end guide piece through the sliding groove. The device has excellent bearing capacity and positioning accuracy, can bear huge load of a large wind tunnel, has excellent rigidity characteristic, and ensures that the axial degree axis of the wind tunnel is maintained within the range of 0.002 ℃.

Description

Guide support device for wind tunnel body
Technical Field
The invention relates to a guide support device for a wind tunnel, and belongs to the technical field of aerodynamic wind tunnel tests.
Background
The wind tunnel is a large-scale structure for simulating the flow test environment of an aircraft, the flow field quality has high requirements, the power section generally has an independent fixed foundation, in order to enable the airflow direction to coincide with the power direction, the size of the wind tunnel structure is large, the wind tunnel body needs to bear the effects of gravity, pressure and temperature load at the same time, in order to ensure that the wind tunnel has good flow field quality and structural characteristics, a support needs to be installed under the wind tunnel body, and for the bearing of gravity, a bridge support is generally adopted.
Therefore, it is desirable to provide a guiding support device for a wind tunnel body to solve the above technical problems.
Disclosure of Invention
The invention solves the problem that the wind tunnel is difficult to bear the lateral force of a large wind tunnel when the wind tunnel is installed in the traditional bridge bearing form. The following presents a simplified summary of the invention in order to provide a basic understanding of some aspects of the invention. It should be understood that this summary is not an exhaustive overview of the invention. It is not intended to determine the key or critical elements of the present invention, nor is it intended to limit the scope of the present invention.
The technical scheme of the invention is as follows:
the utility model provides a wind-tunnel is guide support device for hole body, includes lower connecting plate, lower extreme guide, upper end guide, connecting plate and gliding mass, and lower connecting plate is connected with pre-buried steel sheet, is connected with the gliding mass through lower extreme guide on the lower connecting plate, and the upper portion of upper end guide is provided with the connecting plate, and connecting plate and wind-tunnel hole body coupling, the center of upper end guide is provided with the spout, and the upper portion of gliding mass is passed through the spout and is connected with the upper end guide.
Preferably: the spout is the ladder groove, and the connecting plate is the arc that corresponds the setting with the wind-tunnel cave body.
Preferably: the wind tunnel is an annular wind tunnel, the number of the guide support devices for the wind tunnel body is 2, and the guide support devices for the wind tunnel body are respectively arranged at the lower part of the wind tunnel second crank and the wind tunnel fourth crank.
Preferably, the following components: the installation flatness of the lower connecting plate is not more than 1/1000.
Preferably, the following components: the sliding body and the sliding groove are in clearance fit, the clearance is less than 0.05mm, and the sliding body and the sliding groove are subjected to rust-proof and wear-resistant treatment.
Preferably: and determining the height of the sliding chute according to the slippage of the position of the corresponding hole in the finite element calculation result. Preferably: when finite element calculation is carried out, firstly, a wind tunnel body model is established in an ANSYS DesgignModulator, grids are divided in ANSYS Mechanical software, constraints and loads are loaded according to working condition load conditions to form a finite element calculation model, the model is solved, a displacement cloud chart in a result is checked, and the position of a support is found and component values of deformation in all directions of the support are checked.
The invention has the following beneficial effects:
the device has excellent bearing capacity and positioning accuracy, can bear the huge load (the maximum load can reach 190 tons of force) of a large wind tunnel, has excellent rigidity characteristic, and ensures that the axial degree axis of the wind tunnel is maintained within the range of 0.002 ℃;
the device hardly bears the gravity, so that the interference of the guide device on the bearing of the gravity support is avoided, and the quality of a wind tunnel flow field is guaranteed;
the device has low cost and longer life cycle;
the device has reasonable design and reliable rigidity and strength.
Drawings
Fig. 1 is a schematic structural view of a guide support device for a wind tunnel body according to the present invention;
FIG. 2 is a perspective view of a guide support device for a wind tunnel body according to the present invention;
FIG. 3 is a layout view of a guide support device for a wind tunnel body;
FIG. 4 is an overall deformation cloud chart of a wind tunnel under rated load;
FIG. 5 is a displacement cloud chart of a guiding support device for a wind tunnel body under the action of a rated side load (190 tons of force);
FIG. 6 is a stress cloud chart of a guiding support device for a wind tunnel body under the action of a rated side load (190 tons of force);
in the figure, 1-a lower connecting plate, 2-a lower end guide part, 3-an upper end guide part, 4-a connecting plate, 5-a sliding groove, 6-a sliding body, 7-a wind tunnel axis, 8-a wind tunnel body, 9-a pre-buried steel plate, 10-a guide support, 11-a gravity support, 12-a wind tunnel two-crank, 13-a wind tunnel four-crank, 14-a wind tunnel one-crank, 15-a first diffusion section, 16-a parking chamber, 17-a stabilizing section, 18-a wind tunnel three-crank, 19-a heat exchanger, 20-a second diffusion section and 21-a short axis direction.
Detailed Description
In order that the objects, aspects and advantages of the invention will become more apparent, the invention will be described by way of example only, and with reference to the accompanying drawings. It is to be understood that this description is made only by way of example and not as a limitation on the scope of the invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
The first embodiment is as follows: the embodiment is described with reference to fig. 1 to 6, and the guide support device for the wind tunnel body of the embodiment comprises a lower connecting plate 1, a lower end guide 2, an upper end guide 3, a connecting plate 4 and a sliding body 6, wherein the lower connecting plate 1 is in bolt connection with an embedded steel plate 9, the lower connecting plate 1 is fixedly connected with the sliding body 6 through the lower end guide 2, the upper part of the upper end guide 3 is provided with the connecting plate 4, after the central line of the connecting plate 4 is adjusted, the connecting plate 4 is welded with the outer shell of the wind tunnel body 8, the center of the upper end guide 3 is provided with a sliding chute 5, and the upper part of the sliding body 6 is in sliding connection with the upper end guide 3 through the sliding chute 5; the upper end guide part 3 is connected with the wind tunnel body through the connecting plate 4, the lower end guide part 2 is connected with a civil foundation, the sliding body 6 can move up and down under the action of the sliding chute 5, which is essentially equivalent to providing a lateral surface constraint and a lateral surface constraint to bear lateral loads and bending moments generated by pressure and temperature; a rib plate is arranged between the lower end guide part 2 and the lower connecting plate 1, and a rib plate is arranged between the upper end guide part 3 and the connecting plate 4, so that the rigidity and the strength of the device are ensured, and the device cannot generate overlarge elastic displacement; the device has excellent bearing capacity and positioning accuracy, can bear the huge load (the maximum load can reach 190 tons of force) of a large wind tunnel, has excellent rigidity characteristic, and ensures that the 7-axis degree of the wind tunnel axis is maintained within the range of 0.002 degrees; the wind tunnel axis 7 axis degree is verified by carrying out finite element structure simulation calculation results, and the specific method is as follows: firstly, establishing a simulation model in finite element software (ANSYS), dividing grids and assigning material attributes by adopting a form of entity units, applying 190-ton force load to a guide support, and applying fixed constraint to the bottom surface of the guide support to obtain the deformation condition and the displacement condition of the guide support, wherein the calculation result shows that as shown in figure 5, under the action of the 190-ton force lateral load, the maximum deformation of the support is only 0.01mm, the displacement of the support is very small under the action of a rated lateral load, and the guide support is proved to have excellent rigidity performance; when the deformation of the support is lower than 0.1mm under the load, the deflection angle of the wind tunnel axis under the side load can be ensured to be less than 0.002 degrees; similarly, the results of the finite element simulation of the structure are verified, as shown in fig. 6, the maximum stress of the guide support structure is 103.3MPa and is lower than the allowable material stress 178MPa under the action of the 190 ton force side load, which indicates that the guide support can bear the 190 ton force side load and has excellent bearing capacity;
the sliding groove 5 is a stepped groove, and the connecting plate 4 is in an arc shape which corresponds to the outer shell of the wind tunnel body; the sliding body 6 can not collide with the connecting plate 4 when sliding in the sliding groove 5, so that the influence on the wind tunnel body is reduced; the device hardly bears the gravity, so that the guide device is prevented from interfering the bearing of the gravity support 11; the special-shaped connecting plate 4 is designed through a special shape, the upper edge of the special-shaped connecting plate 4 is an arc-shaped plate with the same radius as the wind tunnel body shell, and the special-shaped connecting plate can be matched and installed with the wind tunnel to fit with the wind tunnel body shape and realize stable connection; the reason why the device does not bear the gravity is that, as shown in figure 5, a larger gap exists between the sliding body 6 and the sliding chute 5 in the gravity direction, and the load in the gravity direction cannot be transferred between the upper part and the lower part of the guide support, because the wind tunnel is a multi-support system, the number of supports bearing the load in the gravity direction is large, the more the supports are, the higher the difficulty of accurately predicting the bearing distribution of the supports is, and meanwhile, the more the interference generated between the supports under the action of temperature load is, so that the guide support does not bear the load in the gravity direction, the interference on other gravity supports can be avoided, and the safety of the wind tunnel support is favorably ensured;
the wind tunnel is an annular wind tunnel, the number of the guide support devices for the wind tunnel body is 2, the guide support devices for the wind tunnel body are respectively arranged at the central axis position of the lower part of the second crank 12 of the wind tunnel and the central axis position of the lower part of the fourth crank 13 of the wind tunnel, and the position indicated by the guide support 10 shown in the attached figure 3 is the installation position of the guide support devices for the wind tunnel body; beside the guide support 10, there are two gravity supports 11 which only bear gravity and are arranged as shown in fig. 3; because the wind tunnel is of a square structure, the wind tunnel two-corner 12, the wind tunnel one-corner 14, the first diffusion section 15, the parking chamber 16, the stabilizing section 17, the wind tunnel four-corner 13, the wind tunnel three-corner 18, the heat exchanger 19 and the second diffusion section 20 are sequentially connected to form a square wind tunnel, the gravity support 11 is arranged under the action of pressure and temperature, the corner of the wind tunnel can generate large lateral displacement, the lateral displacement of the tunnel body structure is limited by the device, the lateral displacement refers to the translation of the short axis direction 21 of the wind tunnel, as shown in figure 3, the device can limit the lateral freedom degree of the tunnel body and the rotation freedom degree in the horizontal plane, the freedom degrees in other directions are released, the gravity at the bottom of the two-corner of the wind tunnel can not generate interference on the support bearing, and the flow field quality of the wind tunnel is guaranteed;
the installation flatness of the lower connecting plate 1 is not more than 1/1000; the excellent positioning precision is realized mainly through two aspects, namely, the mounting flatness of the connecting plate is not more than 1/1000, the clearance of the fit clearance between the sliding body 6 and the side wall of the sliding chute 5 is extremely small (less than 0.05 mm), the higher flatness can ensure that the guide support does not generate larger deflection angle errors, and the smaller clearance can ensure that the guide support does not have larger lateral translation errors;
the sliding body 6 and the sliding groove 5 are in clearance fit, the clearance is less than 0.05mm, and the sliding body 6 and the sliding groove 5 are subjected to rust-proof and wear-resistant treatment; the device has a long life cycle, the replacement cost of a general large wind tunnel support is high, and abrasion is a main reason for the failure of the guide support, so that on one hand, the generation of friction force is reduced through high-precision processing and assembly, and on the other hand, wear-resistant treatment is carried out on the contact surface, so that the support is ensured to have a long life cycle; the reason is that the slide body 6 and the chute 5 are subjected to rust-proof and wear-resistant treatment, and the guide support needs to slide under the condition of bearing pressure, so that the reduction of flatness and the increase of gaps caused by rust and wear are main causes of support failure, and after the rust-proof and wear-resistant treatment, the service life of the support can be greatly prolonged, and the maintenance cost is reduced;
determining the height of the sliding chute 5 according to the slippage of the position of the corresponding hole in the finite element calculation result, and obtaining a displacement cloud chart shown in the attached figure 4;
the finite element calculation and displacement viewing are briefly described as follows: firstly, establishing a shell model of the wind tunnel in an ANSYS DesgignModulator, dividing grids in ANSYS Mechanical software, loading constraints and loads according to working condition load conditions to form a finite element calculation model, solving the model, checking a displacement cloud chart in a result, finding a support position and checking component values of deformation of the support in all directions; the load and the slippage at the installation position of the device are accurately evaluated, the length and the thickness of the sliding chute 5 and the sliding body 6 are designed according to the load information in the result, the two key parameters directly influence the rigidity performance and the strength performance of the support, and reasonable numerical values are designed to ensure that the device has reliable rigidity and strength; meanwhile, according to the deformation information in the finite element calculation result, the length allowance of the sliding groove 5 can be designed accordingly, the sliding body 6 is prevented from moving out of the sliding groove 5, and the rigidity loss and the strength risk are prevented.
It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments according to the present application. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise.
The relative arrangement of the components and steps, the numerical expressions and numerical values set forth in these embodiments do not limit the scope of the present invention unless specifically stated otherwise. Meanwhile, it should be understood that the sizes of the respective portions shown in the drawings are not drawn in an actual proportional relationship for the convenience of description. Techniques, methods, and apparatus known to those of ordinary skill in the relevant art may not be discussed in detail but are intended to be part of the specification where appropriate. In all examples shown and discussed herein, any particular value should be construed as merely illustrative, and not limiting. Thus, other examples of the exemplary embodiments may have different values. It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, further discussion thereof is not required in subsequent figures.
In the description of the present invention, it is to be understood that the orientation or positional relationship indicated by the orientation words such as "front, rear, upper, lower, left, right", "lateral, vertical, horizontal" and "top, bottom", etc. are usually based on the orientation or positional relationship shown in the drawings, and are only for convenience of description and simplicity of description, and in the case of not making a reverse description, these orientation words do not indicate and imply that the device or element being referred to must have a specific orientation or be constructed and operated in a specific orientation, and therefore, should not be considered as limiting the scope of the present invention; the terms "inner and outer" refer to the inner and outer relative to the profile of the respective component itself.
Spatially relative terms, such as "above … …," "above … …," "above … …," "above," and the like, may be used herein for ease of description to describe one device or feature's spatial relationship to another device or feature as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if a device in the figures is turned over, devices described as "above" or "on" other devices or configurations would then be oriented "below" or "under" the other devices or configurations. Thus, the exemplary term "above … …" can include both an orientation of "above … …" and "below … …". The device may be otherwise variously oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
It should be noted that the terms "first," "second," and the like in the description and claims of this application and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used is interchangeable under appropriate circumstances such that the embodiments of the application described herein are capable of operation in other sequences than those illustrated or described herein.
It should be noted that, in the above embodiments, as long as the technical solutions can be aligned and combined without contradiction, those skilled in the art can exhaust all possibilities according to the mathematical knowledge of the alignment and combination, and therefore, the present invention does not describe the technical solutions after alignment and combination one by one, but it should be understood that the technical solutions after alignment and combination have been disclosed by the present invention.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (7)

1. The utility model provides a wind-tunnel is direction support device for the tunnel body which characterized in that: the wind tunnel connecting device comprises a lower connecting plate (1), a lower end guide piece (2), an upper end guide piece (3), a connecting plate (4) and a sliding body (6), wherein the lower connecting plate (1) is connected with a pre-buried steel plate, the lower connecting plate (1) is connected with the sliding body (6) through the lower end guide piece (2), the upper portion of the upper end guide piece (3) is provided with the connecting plate (4), the connecting plate (4) is connected with a wind tunnel body, the center of the upper end guide piece (3) is provided with a sliding groove (5), and the upper portion of the sliding body (6) is connected with the upper end guide piece (3) through the sliding groove (5).
2. The guide support device for the wind tunnel body according to claim 1, wherein: the sliding groove (5) is a stepped groove, and the connecting plate (4) is arc-shaped and corresponds to the wind tunnel body.
3. The guide support device for the wind tunnel body according to claim 1, wherein: the wind tunnel is an annular wind tunnel, the number of the guide support devices for the wind tunnel body is 2, and the guide support devices for the wind tunnel body are respectively arranged at the lower part of the second corner of the wind tunnel and the lower part of the fourth corner of the wind tunnel.
4. The guide support device for the wind tunnel body according to claim 1, wherein: the installation flatness of the lower connecting plate (1) is not more than 1/1000.
5. The guide support device for the wind tunnel body according to claim 1, wherein: the sliding body (6) and the sliding groove (5) are in clearance fit, the clearance is less than 0.05mm, and the sliding body (6) and the sliding groove (5) are subjected to rust-proof and wear-resistant treatment.
6. The guide support device for the wind tunnel body according to claim 1, wherein: and determining the height of the sliding chute (5) according to the slippage corresponding to the position of the hole in the finite element calculation result.
7. The guide support device for the wind tunnel body according to claim 6, wherein: when finite element calculation is carried out, firstly, a wind tunnel body model is established in an ANSYS DesgignModulator, grids are divided in ANSYS Mechanical software, constraints and loads are loaded according to working condition load conditions to form a finite element calculation model, the model is solved, a displacement cloud chart in a result is checked, and the position of a support is found and component values of deformation in all directions of the support are checked.
CN202210995810.XA 2022-08-19 2022-08-19 Guide support device for wind tunnel body Active CN115077847B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210995810.XA CN115077847B (en) 2022-08-19 2022-08-19 Guide support device for wind tunnel body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210995810.XA CN115077847B (en) 2022-08-19 2022-08-19 Guide support device for wind tunnel body

Publications (2)

Publication Number Publication Date
CN115077847A true CN115077847A (en) 2022-09-20
CN115077847B CN115077847B (en) 2022-11-15

Family

ID=83244857

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210995810.XA Active CN115077847B (en) 2022-08-19 2022-08-19 Guide support device for wind tunnel body

Country Status (1)

Country Link
CN (1) CN115077847B (en)

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3224941C1 (en) * 1982-07-03 1984-01-05 Daimler-Benz Ag, 7000 Stuttgart Device for measuring the air resistance of vehicles
CN102494863A (en) * 2011-11-15 2012-06-13 中国航天空气动力技术研究院 Device used for testing height of hypersonic wind tunnel continuous variable projection
CN108362467A (en) * 2017-12-29 2018-08-03 中国空气动力研究与发展中心设备设计及测试技术研究所 The vertical spatial fluid pressure drive device of half flexible jet pipe of continous way transonic wind tunnel
CN108680331A (en) * 2018-05-17 2018-10-19 中国航空工业集团公司沈阳空气动力研究所 A kind of adjustable half flexible jet pipe of branched side wall
CN110306678A (en) * 2019-07-16 2019-10-08 中航工程集成设备有限公司 A kind of connection structure of prefabricated board and braced frame
CN111307400A (en) * 2020-03-31 2020-06-19 中国空气动力研究与发展中心低速空气动力研究所 Back support device for wind tunnel ground effect test
CN210834083U (en) * 2018-07-26 2020-06-23 河北工业大学 Intelligent wind tunnel with variable cross section of test section
CN113551867A (en) * 2021-07-19 2021-10-26 中国空气动力研究与发展中心高速空气动力研究所 Schlieren instrument support system for wind tunnel test
CN215213497U (en) * 2021-07-24 2021-12-17 魏磊 Coal mining tunneling channel reinforcing equipment
CN114166458A (en) * 2021-11-30 2022-03-11 中国航天空气动力技术研究院 Wind tunnel body part suspension system and method
CN114235326A (en) * 2021-11-30 2022-03-25 中国航天空气动力技术研究院 Free piston shock tunnel quality buffer mechanism
CN114608795A (en) * 2022-05-11 2022-06-10 中国飞机强度研究所 Wind tunnel system resonance boundary determining method for airplane blowing test
CN114894425A (en) * 2022-07-13 2022-08-12 中国航空工业集团公司沈阳空气动力研究所 Large-scale transonic wind tunnel semi-flexible wall spray pipe

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3224941C1 (en) * 1982-07-03 1984-01-05 Daimler-Benz Ag, 7000 Stuttgart Device for measuring the air resistance of vehicles
CN102494863A (en) * 2011-11-15 2012-06-13 中国航天空气动力技术研究院 Device used for testing height of hypersonic wind tunnel continuous variable projection
CN108362467A (en) * 2017-12-29 2018-08-03 中国空气动力研究与发展中心设备设计及测试技术研究所 The vertical spatial fluid pressure drive device of half flexible jet pipe of continous way transonic wind tunnel
CN108680331A (en) * 2018-05-17 2018-10-19 中国航空工业集团公司沈阳空气动力研究所 A kind of adjustable half flexible jet pipe of branched side wall
CN210834083U (en) * 2018-07-26 2020-06-23 河北工业大学 Intelligent wind tunnel with variable cross section of test section
CN110306678A (en) * 2019-07-16 2019-10-08 中航工程集成设备有限公司 A kind of connection structure of prefabricated board and braced frame
CN111307400A (en) * 2020-03-31 2020-06-19 中国空气动力研究与发展中心低速空气动力研究所 Back support device for wind tunnel ground effect test
CN113551867A (en) * 2021-07-19 2021-10-26 中国空气动力研究与发展中心高速空气动力研究所 Schlieren instrument support system for wind tunnel test
CN215213497U (en) * 2021-07-24 2021-12-17 魏磊 Coal mining tunneling channel reinforcing equipment
CN114166458A (en) * 2021-11-30 2022-03-11 中国航天空气动力技术研究院 Wind tunnel body part suspension system and method
CN114235326A (en) * 2021-11-30 2022-03-25 中国航天空气动力技术研究院 Free piston shock tunnel quality buffer mechanism
CN114608795A (en) * 2022-05-11 2022-06-10 中国飞机强度研究所 Wind tunnel system resonance boundary determining method for airplane blowing test
CN114894425A (en) * 2022-07-13 2022-08-12 中国航空工业集团公司沈阳空气动力研究所 Large-scale transonic wind tunnel semi-flexible wall spray pipe

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
赖欢等: "0.3m低温连续式跨声速风洞结构设计", 《实验流体力学》 *

Also Published As

Publication number Publication date
CN115077847B (en) 2022-11-15

Similar Documents

Publication Publication Date Title
CN102901595B (en) Method for measuring hinge moment of control surface
CN108169015B (en) Tail rotor flexible beam torque loading test device
CN102589804B (en) Satellite attitude transformation device for testing quality characteristics of satellite
CN106769013A (en) A kind of loading inertia test apparatus of motor-driven cylinder
CN115077847B (en) Guide support device for wind tunnel body
US7966865B2 (en) Method for balancing radical projections detached from a rotating assembly
CN103407579B (en) A kind of major diameter airframe test loads fixture
CN103056799B (en) Positioner
CN204116134U (en) A kind of rolling bearing radial rigidity test fixture
CN113720707A (en) Design method for large-deformation loading point of structural fatigue test
CN107228127B (en) Air bearing
CN205173895U (en) Hydraulic actuator support
CN105303003B (en) A kind of optimization method for disk brake push rod position
CN113310827B (en) Multidirectional loading test device for driving axle housing of commercial vehicle
CN113532789B (en) Device for improving calibration uncertainty of half-mode balance and application
CN205978135U (en) Preloading device of bearing assembly and bearing
CN112556626B (en) Assembly method based on multi-nail-hole matched positioning
CN115753096A (en) Nuclear power station main pump thrust bearing test bed and assembling method thereof
CN207188739U (en) A kind of big temperature difference working condition mould is guide locating device provided with chamfered edge guide pillar guide pin bushing
CN112711809B (en) Control surface load screening method
CN109752155B (en) Fixed boundary freedom degree release system for static test of structural part
CN211292352U (en) Horizontal tensile frame test device
CN202770618U (en) Automobile wind tunnel test model strutting arrangement
CN111366121A (en) Method for recovering precision of old welding fixture
CN106828871B (en) A kind of heat insulation structural

Legal Events

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