CN218806496U - Fixed trailing edge sealing plate structure - Google Patents

Fixed trailing edge sealing plate structure Download PDF

Info

Publication number
CN218806496U
CN218806496U CN202222685209.9U CN202222685209U CN218806496U CN 218806496 U CN218806496 U CN 218806496U CN 202222685209 U CN202222685209 U CN 202222685209U CN 218806496 U CN218806496 U CN 218806496U
Authority
CN
China
Prior art keywords
plate
partition plate
wall surface
partition
feature
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
CN202222685209.9U
Other languages
Chinese (zh)
Inventor
应孝岩
卫改侠
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 First Aircraft Institute
Original Assignee
AVIC First Aircraft 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 First Aircraft Institute filed Critical AVIC First Aircraft Institute
Priority to CN202222685209.9U priority Critical patent/CN218806496U/en
Application granted granted Critical
Publication of CN218806496U publication Critical patent/CN218806496U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Building Environments (AREA)

Abstract

The application belongs to aviation front wing cabin obturating plate structure design field, in particular to fixed trailing edge obturating plate structure, include: a partition plate and an outer panel; the partition plates comprise a first partition plate, a second partition plate and a third partition plate; the outer side plate comprises a partition plate edge strip and a sealing plate, wherein a first crack is formed at the joint of the partition plate edge strip and the wall surface, and a second crack is formed at the joint of the sealing plate and the wall surface; a first special part is arranged between the first partition plate and the wall surface, the first special part comprises two mounting edges, one mounting edge is connected with the wall surface, and the other mounting edge is connected with the side wall of the first partition plate; a second special part is connected between the partition plate edge strip and the wall surface, and the second special part covers the first crack; the third special part is connected between the sealing plate and the wall surface; a third feature covers the second fracture; the wing flap and the baffle plate do not need to be disassembled, the construction is simple and convenient, and the repair result is effective after the installation through flight inspection.

Description

Fixed trailing edge sealing plate structure
Technical Field
The application belongs to the field of aviation flap cabin sealing plate structure design, and particularly relates to a fixed trailing edge sealing plate structure.
Background
Due to special function requirements of a certain type of airplane, a flap cabin adopts a sealing plate structure. During the outfield flight, the flap cabin sealing plate has cracks.
When the aircraft takes off or lands, the flap deflects downwards, the baffle deflects upwards, the flap cabin sealing plate, the baffle and the flap leading edge form a narrow slit channel together, and airflow flows from the lower wing surface to the upper wing surface through the slit channel. In the process, as the airflow is blocked under the flap, part of the high-speed airflow enters the inside of the flap cabin through the slot, and strong broadband pressure pulsation is formed. The pressure pulsation acts on a clapboard and a covering of the flap cabin. When a certain order of main vibration modes of the partition plate, the web plate and the skin fall within the frequency band range of air pressure pulsation, continuous excessive vibration is generated under continuous excitation of the pressure pulsation, and finally high-cycle fatigue damage of the sealing plate of the flap cabin is caused.
SUMMERY OF THE UTILITY MODEL
In order to solve the above problems, the present application provides a fixed trailing edge sealing plate structure, comprising:
a partition plate and an outer panel;
the bottom edge of the partition board is connected with the wall surface, and the edge bevel edge adjacent to the bottom edge is provided with a sealing plate to form a slope;
the partition plates comprise a first partition plate, a second partition plate and a third partition plate;
the outer side plate comprises a partition plate edge strip and a sealing plate, and the width of the sealing plate is greater than that of the partition plate edge strip;
the first partition board is connected with the partition board edge strip, and one end of the partition board edge strip is connected with the wall surface;
a sealing plate is connected between the second partition plate and the third partition plate, and one end of the sealing plate is connected with the wall surface;
the joint of the partition plate edge strip and the wall surface is provided with a first crack, and the joint of the sealing plate and the wall surface is provided with a second crack;
the method is characterized in that:
a first special part is arranged between the first partition plate and the wall surface, the first special part comprises two mounting edges, one mounting edge is connected with the wall surface, and the other mounting edge is connected with the side wall of the first partition plate; a second special part is connected between the partition plate edge strip and the wall surface, and the second special part covers the first crack; the third special part is connected between the sealing plate and the wall surface; a third feature covers the second fracture.
Preferably, the cracks at the first and second cracks are perforated with crack stoppers.
Preferably, the second special part is bonded with the edge strip of the separator through glue; the second special part is connected with the wall plate through the original hole position and the bolt of the wall plate.
Preferably, the second feature comprises a large end and a small end, the width of the second feature gradually increasing from the small end to the large end; the big end is connected with the wall plate, and the small end is connected with the partition plate edge strip.
Preferably, the third special part is connected with the sealing plate through a rivet and a drawing nail; the third special part is connected with the wall plate through bolts.
Preferably, the bolt is connected to the third feature through a through hole provided in the panel, said through hole comprising the through hole after removal of the rivet originally provided in the panel.
Preferably, the third special part is rectangular, and the third special part is provided with a plurality of mounting holes, wherein the mounting holes comprise original machine holes connected with the second partition plate and the third partition plate, and lower ends of the original machine holes connected with the wall plate, and newly-manufactured holes; the original machine hole is a hole formed in the position of the hole of the third special part in the second partition plate, the third partition plate and the wall plate.
Preferably, the third feature is provided with a spacer at the junction with the panel, said spacer being adapted to cushion the sagging of the panel which breaks the original seal.
Preferably, the outer surface of the third special part is sequentially coated with X06-1 iron red primer, H06-2 iron red primer and original machine finishing paint
The advantages of the present application include: this application need not to dismantle wing flap, baffling board, and the construction is simple and convenient, and the installation back is through flight inspection, and the repair result is effective, can in time to the board reinforcement of obturating, avoids around the structure because the bearing failure of obturating board, the crackle produces gradually, leads to the local structure of wing flap cabin to become invalid, influences the normal guarantee and the use of aircraft.
Drawings
FIG. 1 is a schematic view of the reinforcement of a seal according to a preferred embodiment of the present application;
FIG. 2 is a view AA of FIG. 1;
FIG. 3 is a view BB of FIG. 1;
FIG. 4 is a schematic connection diagram of a first feature;
FIG. 5 is a schematic connection diagram of a second feature;
FIG. 6 is a schematic view of a seal plate structure according to a preferred embodiment of the present application.
Detailed Description
In order to make the implementation objects, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the drawings in the embodiments of the present application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all embodiments of the present application. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present application, and should not be construed as limiting the present application. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application. Embodiments of the present application will be described in detail below with reference to the drawings.
The present application provides a fixed trailing edge seal plate structure, as shown in fig. 1-6, comprising:
a separator and an outer panel;
the bottom edge of the partition board is connected with the wall surface, and the edge bevel edge adjacent to the bottom edge is provided with a sealing plate to form a slope;
the partition plates comprise a first partition plate 11, a second partition plate 12 and a third partition plate 13;
the outer side plate comprises a partition plate edge strip 21 and a sealing plate 22, and the width of the sealing plate 22 is greater than that of the partition plate edge strip 21;
the first partition plate 11 is connected with a partition plate edge strip 21, and one end of the partition plate edge strip 21 is connected with the wall surface;
a sealing plate 22 is connected between the second partition plate 12 and the third partition plate 13, and one end of the sealing plate 22 is connected with the wall surface;
wherein, the joint of the partition plate edge strip 21 and the wall surface has a first crack, and the joint of the sealing plate 22 and the wall surface has a second crack;
a first special part 31 is arranged between the first partition plate 11 and the wall surface, the first special part 31 comprises two mounting edges, one mounting edge is connected with the wall surface, and the other mounting edge is connected with the side wall of the first partition plate 11; a second special part 32 is connected between the partition edge strip 21 and the wall surface, and the second special part 32 covers the first crack; the third special part 33 is connected between the sealing plate 22 and the wall surface; a third feature 33 covers the second fracture.
Preferably, the cracks at the first and second cracks are perforated with crack stoppers.
Preferably, the second feature 32 is adhesively bonded to the separator bead 21; the second feature 32 is bolted to the panel through the original hole site in the panel itself.
Preferably, the second feature 32 includes a large end and a small end, the width of the second feature 32 increasing from the small end to the large end; the large end is connected with the wall plate, and the small end is connected with the partition plate edge strip 21.
Preferably, the third feature 33 is connected to the closure panel 22 by rivets and pop-pins; the third feature 33 is bolted to the wall panel.
Preferably, the bolts are connected to the third feature 33 through holes provided in the panel, including the through holes after removal of the rivets originally provided in the panel.
Preferably, the third special part 33 is rectangular, and the third special part 33 has a plurality of mounting holes, wherein the mounting holes include original machine holes connected with the second partition plate and the third partition plate, and lower ends connected with the wall plate, and newly-made holes; the original machine holes are holes of the third special part 33 at the positions of the holes of the second partition plate, the third partition plate and the wall plate.
Preferably, the third feature 33 has a gasket at its junction with the wall panel, said gasket being adapted to cushion the sagging of the broken original seal plate on the flat wall panel.
Preferably, the third workpiece 33 is coated with an X06-1 iron red primer, an H06-2 iron red primer, and a prime machine finish in sequence.
The reinforcing step of the sealing plate is as follows:
(1) Drilling a crack stop hole with the diameter of 5mm at the tip of the crack, wherein the center of the crack stop hole is 2mm more than the tip of the crack which is observed visually;
(2) Polishing a skin paint layer on the surface of the repair area, and cleaning;
(3) Bonding a third special part 33 outside the skin, wherein the material: 1Cr18Ni9 Ti-delta 0.8. The glue is EC2216A/B. Before the special part 33 is bonded, the special part 33 is ensured to be bonded with the original sealing plate;
(4) And (3) decomposing the local rivets of the second partition plate and the original sealing plate in the sealing plate, decomposing the local rivets of the third partition plate and the original sealing plate at the same time, paying attention to protect the original machine structure and the fastener holes, and connecting the decomposed rivet holes with rivets 4A1-90-3.5 multiplied by 7 and pull nails CR 3223-04-02. The third special part 33 is connected with the original sealing plate by adopting a rivet 4A1-90-3 multiplied by 5 and a drawing nail CR 3223-04-02. The position of the newly manufactured rivet 4A 1-90-3X 5 is allowed to be partially adjusted, but it is necessary to ensure that the connecting margin is not less than 8mm. The local rivets of the original hinge and the original sealing plate are decomposed and are connected by bolts HB 1-103-4X 18, nuts 4A1-41-4 and washers 4A 1-180-4X 10X 1.5. The flat sealing plate is allowed to sink by using a gasket pad, and the gasket material LY 12-CZ-delta 1.2 has the size determined by the process and needs to ensure the edge distance of the fastener.
(5) Coating X06-1 on the outer surface of the reinforcing plate 1, then coating H06-2 iron red primer, and finally coating original machine finish on the surface.
Reinforcement of a partition panel bead
(1) And if the separator edge strip has first cracks, the separator crack edge strip is decomposed, and the separator edge strip is flattened to the crack-stopping hole. Filing, polishing and smoothing the surface, and then coating alodine;
(2) And rivets for connecting the edge strips of the partition boards with the longitudinal walls of the flap cabins. And (3) decomposing rivets connected with the hinges and the edge strips of the partition boards, and 2 adjacent rivets. Care is taken to protect the original machine structure and fastener holes;
(3) Connecting a second special part 32 and a first special part 31 at the edge strip respectively, wherein the material: 1Cr18Ni9 Ti-delta 0.8. The connecting fastener is changed into bolts HB 1-103-4X 14, HB 1-103-4X 18, nuts 4A1-41-4, gaskets 4A 1-180-4X 8X 1 and special gasket connection. The position of a newly manufactured bolt on the web is allowed to be locally adjusted, but the connection edge distance is ensured to be not less than 8mm.
(4) The skin at the hinge is allowed to sink by using a gasket pad, and the gasket material LY 12-CZ-delta 0.8 is determined by the process, so that the edge distance of the fastener is ensured. The joint of the wall plate and the first special part 31 is allowed to be padded, and the edge distance of a fastener needs to be ensured when the material LY 12-CZ-delta 0.8 of the padding is used;
(5) And coating the surface with finish paint of an original machine after assembly. All special parts and gaskets are allowed to be filed, and the filed surfaces of the gaskets are coated with alodine after being polished smooth.
The advantages of the present application include: this application need not to dismantle wing flap, baffling board, and the construction is simple and convenient, and the installation back is through flight inspection, and the repair result is effective, can in time be to the board reinforcement of obturating, avoids around the structure because the bearing failure of board of obturating, produce the crackle gradually, lead to wing flap cabin local structure to become invalid, influence the normal guarantee and the use of aircraft.
The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present application should be covered within the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.

Claims (9)

1. A fixed trailing edge seal plate structure comprising:
a partition plate and an outer panel;
the bottom edge of the partition board is connected with the wall surface, and the edge bevel edge adjacent to the bottom edge is provided with a sealing plate to form a slope;
the partition plates comprise a first partition plate (11), a second partition plate (12) and a third partition plate (13);
the outer side plate comprises a partition plate edge strip (21) and a sealing plate (22), and the width of the sealing plate (22) is larger than that of the partition plate edge strip (21);
the first partition plate (11) is connected with the partition plate edge strip (21), and one end of the partition plate edge strip (21) is connected with the wall surface;
a sealing plate (22) is connected between the second partition plate (12) and the third partition plate (13), and one end of the sealing plate (22) is connected with the wall surface;
wherein, the joint of the clapboard edge strip (21) and the wall surface is provided with a first crack, and the joint of the sealing plate (22) and the wall surface is provided with a second crack;
the method is characterized in that:
a first special part (31) is arranged between the first partition plate (11) and the wall surface, the first special part (31) comprises two mounting edges, one mounting edge is connected with the wall surface, and the other mounting edge is connected with the side wall of the first partition plate (11); a second special piece (32) is connected between the partition edge strip (21) and the wall surface, and the second special piece (32) covers the first crack; the third special part (33) is connected between the sealing plate (22) and the wall surface; a third feature (33) covers the second fracture.
2. The fixed trailing edge seal plate structure of claim 1, wherein the cracks at the first and second cracks are perforated with crack stop holes.
3. The fixed trailing edge seal plate structure of claim 1, wherein the second feature (32) is bonded to the spacer bead (21) by glue; the second feature (32) is connected to the panel by means of the holes in the panel itself and by means of bolts.
4. The fixed trailing edge seal panel structure of claim 3, wherein the second feature (32) includes a large end and a small end, the width of the second feature (32) increasing from the small end to the large end; the large end is connected with the wall plate, and the small end is connected with the partition plate edge strip (21).
5. The fixed trailing edge seal plate structure of claim 1, wherein the third feature (33) is connected to the seal plate (22) by rivets and pop-pins; the third feature (33) is bolted to the panel.
6. The fixed trailing edge seal plate structure of claim 5, wherein the bolts are connected to the third feature (33) through holes provided in the wall plate, the holes including the holes after removal of the rivets originally provided in the wall plate.
7. The fixed trailing edge seal panel structure of claim 5, wherein the third piece (33) is rectangular, the third piece (33) having a plurality of mounting holes, the mounting holes including original machine holes connected to the second and third partitions, lower ends connected to the wall panel, and newly formed holes; the original machine hole is a hole formed in the position of the hole of the third special part (33) in the second partition plate, the third partition plate and the wall plate.
8. The fixed trailing edge seal panel structure of claim 1, wherein the third feature (33) has a spacer at the connection to the panel, the spacer for backing up a depression in the panel that breaks the original seal.
9. The fixed trailing edge seal plate structure of claim 1, wherein the third feature (33) has an outer surface coated with an X06-1 iron red primer, an H06-2 iron red primer, and a base finish in that order.
CN202222685209.9U 2022-10-12 2022-10-12 Fixed trailing edge sealing plate structure Active CN218806496U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202222685209.9U CN218806496U (en) 2022-10-12 2022-10-12 Fixed trailing edge sealing plate structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222685209.9U CN218806496U (en) 2022-10-12 2022-10-12 Fixed trailing edge sealing plate structure

Publications (1)

Publication Number Publication Date
CN218806496U true CN218806496U (en) 2023-04-07

Family

ID=87248657

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202222685209.9U Active CN218806496U (en) 2022-10-12 2022-10-12 Fixed trailing edge sealing plate structure

Country Status (1)

Country Link
CN (1) CN218806496U (en)

Similar Documents

Publication Publication Date Title
CA2852243C (en) Apparatus and methods for extended hybrid laminar flow control
US5368258A (en) Arrangement for maintaining laminar air flow over gaps in aircraft engine nacelle surfaces
US8443575B1 (en) Composite access door
EP2886452B1 (en) Flow body, method for manufacturing a flow body and aircraft having such a flow body
US8974886B2 (en) Disbond resistant composite stiffener runout
EP2987720A1 (en) Hat stringer closeout fitting and method of making same
CN103241255A (en) Motor train unit body
US10532807B2 (en) Leading edge with laminar flow control and manufacturing method thereof
EP3233626B1 (en) Sound absorbers for airframe components
CN218806496U (en) Fixed trailing edge sealing plate structure
US20130228648A1 (en) Auxiliary power unit inlet
US3135486A (en) Airfoil construction and method for making the same
US3420477A (en) Integral fuel tank
CN205472143U (en) Closed silence elevator car
CN110065620A (en) A kind of composite walls board connecting structure
CN204310647U (en) A kind of lift car reducing running noises
CN213354881U (en) Fatigue test piece for airplane stringer wallboard
US7677496B2 (en) Stringer for an aircraft wing and a method of reinforcing thereof
CN110920913A (en) Double-oil-tank structure of reinforced wall plate made of composite material with high aspect ratio
CN218317290U (en) Aircraft wing flap terminal surface seal structure
CN210416560U (en) Connecting structure at joint of glass fiber reinforced plastic air duct
CN218292602U (en) Metal surface aluminum honeycomb decorative plate wall system
CN110901919B (en) Helicopter hangs acoustic cover
CN217260637U (en) Sound insulation structure is strengthened to aircraft cabin wall
CN114239150B (en) Airplane inflection connecting structure and anti-fatigue design method thereof

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant