BYPASS TURBOFAN ENGINE COMPRISING A NACELLE EQUIPPED WITH A TRANSLATIONALLY-MOBILE THRUST-REVERSAL SYSTEM AND WITH A FAN CASE EQUIPPED WITH SUPPORTS

Abstract

A method for connecting two components is proposed where a pressure acting on an adhesive between two join partners is supported by an auxiliary body which rests on a cutout of one of the components. Both components to be connected together and the auxiliary body are covered by a vacuum film and once the air has been sucked out, the compressive force is generated below the vacuum film.

Claims

1. A method for connecting two components, comprising the steps: arranging a first component on a tool surface, arranging a second component, which comprises a cutout, on the first component to include an adhesive, placing an auxiliary body covering the cutout onto the second component, covering the second component, the auxiliary body and at least one closure region of the first component surrounding the second component with a vacuum film, evacuating a space surrounded by the first component and the vacuum film, and removing the vacuum film once the adhesive has hardened.

2. The method according to claim 1, additionally comprising the step of heating a space between the first component and the second component in which the adhesive is situated.

3. The method according to claim 1, additionally comprising a step of introducing a reinforcing element between the first component and the second component, wherein the adhesive is trapped between the first component and the reinforcing element and between the reinforcing element and the second component.

4. The method according to claim 1, wherein the first component comprises a first cutout, wherein the second component comprises a second cutout and wherein the second component is placed onto the first component in such a manner that the first cutout and the second cutout are oriented in alignment with one another.

5. The method according to claim 1, additionally comprising a step of clamping the auxiliary body on a mold by means of an element exerting a tensile force or a compressive force.

6. The method according to claim 5, wherein the clamping includes a screwing-in of a bolt through an opening arranged in the auxiliary body.

7. The method according to claim 1, wherein the clamping includes the pressing of the auxiliary body onto the second component with an actuator.

8. The method according to claim 7, wherein the actuator is coupled with a vacuum source which is used for evacuation.

9. The method according to claim 1, wherein the second component comprises a flange which runs around the cutout at least in regions and extends from the second component in a direction remote from the first component, wherein the auxiliary body is placed onto the flange.

10. A system for connecting two components, comprising: a mold, an auxiliary body, a vacuum film, a vacuum source, and an adhesive, wherein the mold comprises a tool surface for receiving a first component, wherein the auxiliary body is realized for a purpose of being placed onto a second component and in this case covering a cutout of the second component, wherein the vacuum film is realized for a purpose of covering the second component placed onto the first component to include the adhesive, the auxiliary body placed onto the second component, and at least one closure region of the first component surrounding the second component, and wherein the vacuum source is couplable with at least one opening in the vacuum film or in the mold so that a space surrounded by the first component and the vacuum film is evacuatable.

11. The system according to claim 10, wherein the auxiliary body comprises a slidable coating.

12. The system according to claim 10, wherein a surface of the mold comprises a threaded bore, wherein the auxiliary body comprises an opening which aligns with the threaded bore when the first component, the second component and the auxiliary body are positioned as provided, and wherein the system additionally comprises a bolt with a thread which corresponds to the threaded bore for clamping the auxiliary body to the mold.

13. The system according to claim 10, additionally comprising an actuator for pressing the auxiliary body onto the second component.

14. The system according to claim 13, additionally comprising a force regulating unit which is coupled with the actuator and is realized for a purpose of identifying a force acting on the auxiliary body by the actuator and adjusting it to a predetermined value.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0031] Further features, advantages and application possibilities of the present invention are produced from the following description of the exemplary embodiments and the Figures. In this case, all described and/or graphically shown features, independently of their composition in the individual claims or the references thereto, also form the object of the invention per se and in arbitrary combination. In addition, identical reference symbols stand for identical or similar objects in the Figures.

[0032] FIG. 1 shows a sectional representation of a system according to the invention for connecting two components.

[0033] FIG. 2 shows a sectional representation of a modified system for connecting components.

[0034] FIG. 3 shows a sectional representation of a further modified system for connecting components.

[0035] FIG. 4 shows a schematic, block-based representation of a method for connecting components.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0036] FIG. 1 shows a sectional representation of a system 2 for connecting a first component 4 and a second component 6. A mold 8 comprises a tool surface 10 onto which the first component 4 is placed. In this representation, the tool surface 10 is realized in a solid, i.e., continuous, manner. This could, however, also be modified as long as it is ensured that an arrangement located thereon is air-tight and evacuatable.

[0037] The first component 4 is, for example, a fuselage shell of a passenger aircraft which comprises a first cutout 12 at the position shown. This is, for example, a window cutout and is round, oval or extensively rectangular with rounded corners. The second component 6 is a window frame which is to be subsequently located inside in the finished aircraft fuselage and has a second cutout 14 which is aligned with the first cutout 12.

[0038] The second component 6 additionally comprises a flange 16 which runs around the second cutout 14 and extends from the second component 6 in a direction remote from the first component 4. The flange 16 follows, for instance, an edge of the first cutout 12 and, as a result, can be a portion of a lateral surface of a hollow cylinder or of a hollow cone.

[0039] For connecting the first component 4 and the second component 6, the second component 6 comprises a contact surface 18 which lies, for example, radially outside the flange 16. The contact surface 18 serves for producing a surface contact between the second component 6 and the join partner. This is shown here, for example, in the form of a reinforcing element 20 which is used for thickening an edge surface 21 of the first component 4 running around the first cutout 12. The contact surface 18 is consequently glued to the reinforcing element 20 which is glued in the meantime to the edge surface 21. The reinforcing element 20, however, can also be omitted should a thickening not be necessary. The contact surface 18 is consequently then glued to the edge surface 21.

[0040] In the example shown, a layer of adhesive is present in each case between the first component 4 and the reinforcing element 20 and between the reinforcing element 20 and the second component 6. This could be realized as a thermosetting adhesive.

[0041] A vacuum film 22, which could be glued onto the first component 4 and in this case cover the second component 6 entirely, is used for pressing the components 4 and 6 onto one another. The adhesive is acted upon with pressure after evacuation in order to optimize the quality of the adhesion. As, however, the second component 6 comprises the second cutout 14, on account of the limited contact surface it cannot be expected that a sufficient compressive force can be produced by purely placing the vacuum film 22 in position.

[0042] In order to increase this, an auxiliary body 24 which is placed onto the flange 16 and, in this case, covers the second cutout 14 entirely, is provided. The auxiliary body 24 comprises, as an example, a circumferential groove 25 which is adapted to the form of the flange 16. The groove 25 can be placed onto the flange 16 in a flush manner.

[0043] The complete arrangement of mold 8, first component 4, second component 6 and auxiliary body 24 is covered by the vacuum film 22. This film extends up to a closure region 23 which is clearly located outside the second component 6. After the space located below this film is evacuated, the entire surface, which is determined by an outer contour of the second component 6, acts to generate a compressive force in the direction of the mold 8. The auxiliary body 24 results in introducing a comparatively large compressive force onto the flange 16 so that the adhesive which is located radially outside is loaded with a predetermined compressive force and is consequently exposed to a desired pressure.

[0044] A vacuum source 26, which is shown schematically as a block, can be coupled with an opening 28 of the vacuum film 22 and can suck air out of an interior 30 below the vacuum film 22. The opening 28 can be aligned with a through bore 32 of the auxiliary body 24. As an alternative to this, such an opening could also be integrated in the mold 8. As a result of the evacuation, the vacuum film 22 tightens against all components located below it and presses them in the direction of the tool surface 10. The adhesive is consequently exposed to a desired pressure.

[0045] The connection between the two components 4 and 6 can consequently be effected outside an autoclave. In particular, larger components are able to be processed with such a system.

[0046] Should, however, the pressure achieved by the system 2 not yet be sufficient, the auxiliary body 24 could be additionally clamped. A modified system 34 shown in FIG. 2, in which a schematically represented actuator 36 is also provided in addition to the components in FIG. 1, could be used for this purpose. This actuator acts on the auxiliary body 24. The actuator 36 can be a hydraulic or pneumatic actuator and can be supplied with a fluid which is acted upon with pressure. The force exerted by the actuator 36 can be adjusted by regulating the pressure applied to the actuator 36. As an alternative to this, the actuator 36 can also comprise a spindle gear which is coupled with an electric motor. Fluid lines and electrical lines which are necessary for the operation of the actuator 36 are not shown for the sake of simplicity.

[0047] It is also conceivable for the actuator 36 to be coupled with a force regulating unit 38 which delimits a force exerted on the auxiliary body 24 by the actuator 36. A force measuring device, which measures the force exerted onto the auxiliary body 24 and actuates the actuator 36 in dependence thereof, can be provided for this purpose.

[0048] As shown in FIG. 3 by way of a modified system 40, it is also possible to use a bolt 42 which extends into a threaded bore 44 of the mold 8 and is guided through a corresponding opening 46 of the auxiliary body 24. It is possible to adjust an additional compressive force acting on the second component 6 by screwing the bolt 42 through the opening 46 into the threaded bore 44. In a particularly preferred manner, it is possible to adjust the additional compressive force in a precise manner by using a torque wrench at a screw head 48 of the bolt 42.

[0049] Finally, FIG. 4 shows a schematic, block-based representation of a method 50 for connecting two components 4 and 6. The method 50 comprises the step of arranging 52 the first component 4 on the tool surface 10. The second component 6, which comprises the cutout 14, is then placed onto the first component 4 to include an adhesive 54. The auxiliary body 24 covering the second cutout 14 is placed 56 onto the second component 6. In addition, the second component 6, the auxiliary body 24 and at least one closure region of the first component 4 surrounding the second component 6 are covered 58 with the vacuum film 22. The space 30 enclosed by the first component 4 and the vacuum film 22 is then evacuated 60. Once the adhesive has hardened, the vacuum film 22 is removed 62. As an option, the auxiliary body can also be clamped 64 prior to being covered 58. In addition, after the covering 58, a space between the first component 4 and the second component 6, in which the adhesive is situated, can be heated 66. As another option, it is possible to introduce 68 the reinforcing element 20 between the first component 4 and the second component 6 so that reinforcing in particular of an edge region about the first cutout 12 is effected.

[0050] In addition, it must be pointed out that comprising does not exclude any other elements or steps, and a or an does not exclude a plurality.

[0051] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.

LIST OF REFERENCES

[0052] 2 System [0053] 4 First component [0054] 6 Second component [0055] 8 Mold [0056] 10 Tool surface [0057] 12 First cutout [0058] 14 Second cutout [0059] 16 Flange [0060] 18 Contact surface [0061] 20 Reinforcing element [0062] 21 Edge surface [0063] 22 Vacuum film [0064] 23 Closure region [0065] 24 Auxiliary body [0066] 25 Groove [0067] 26 Vacuum source [0068] 28 Opening [0069] 30 Interior [0070] 32 Through bore [0071] 34 System [0072] 36 Actuator [0073] 38 Force regulating unit [0074] 40 System [0075] 42 Bolt [0076] 44 Threaded bore [0077] 46 Opening [0078] 48 Screw head [0079] 50 Method [0080] 52 Arrange the first component [0081] 54 Arrange the second component [0082] 56 Place the auxiliary body in position [0083] 58 Cover with vacuum film [0084] 60 Evacuate [0085] 62 Remove the vacuum film [0086] 64 Clamp the auxiliary body [0087] 66 Heat [0088] 68 Introduce the reinforcing element