• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A crossbar for use in a rocker mechanism comprising a first section, a second section, and an average section between the first section and the second section. The middle section includes a flange with a through hole. The first section has a first diameter, the second section has a second diameter and the middle section has a third diameter. The third diameter being larger than at least one of the first diameter and the second diameter.
    公开号:FR3048678A1
    申请号:FR1751963
    申请日:2017-03-10
    公开日:2017-09-15
    发明作者:Stephen Michael Bortoli；Paul Henry Verstrate
    申请人:Hamilton Sundstrand Corp；
    IPC主号:
    专利说明:

    TRANSVERSE BAR FOR ACTUATOR ROCKER MECHANISM
    EMERGENCY WIND
    CONTEXT
    The object of the invention disclosed here generally relates to the emergency wind turbine actuators and more specifically the transverse bars used in a rocking mechanism for an emergency wind turbine actuator (RAT).
    [0002] RATs are commonly used in modern aircraft to provide a secondary and / or emergency power source in case of failure or failure of the main power source. A typical RAT includes a turbine that remains inside the aircraft until it is used. If additional power is required, a hatch in the fuselage of the aircraft will open and the actuator will deploy the RAT turbine into the air stream. The air stream will rotate the turbine and the rotational torque of the turbine is transferred through a transmission to be converted into electric current by a generator. A RAT can also be used to drive a hydraulic pump.
    [0003] A rocker mechanism within the RAT actuator may also act as a centering mechanism to initiate the activation process. Upon receipt of an electrical command, solenoids pull on a cross bar to move the rocker mechanism past its central position, which then allows the actuator to operate and deploy the RAT. The cross bar receives the charge from the solenoids and also a counter charge from the internal components of the actuator. Therefore, a cross bar can support the load. while being easy to install and maintain, will provide both cost and reliability benefits. SUMMARY [0004] According to one embodiment, a crossbar for use in a rocker mechanism of an emergency wind turbine actuator is described. The crossbar includes a first section, a second section, and an average section between the first section and the second section. The middle section includes a flange with a through hole. The first section has a first diameter, the second section has a second diameter and the middle section has a third diameter. The third diameter being larger than at least one of the first diameter and the second diameter.
    [0005] In addition to one or more of the features described above, or as an alternative, other embodiments of the crossbar may include the fact that the middle section includes a clearance notch.
    According to another embodiment, a rocking mechanism of an emergency wind turbine actuator is described. The rocker mechanism includes a clevis and a crossbar operably connected to the yoke. The crossbar having a first section, a second section, and an average section between the first section and the second section. The middle section includes a flange with a through hole. The rocker mechanism also includes a screw cap placed in the through hole. The screw cap fixes the crossbar to the screed.
    [0007] In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may include the fact that the first section has a first diameter, the second section has second diameter and the middle section has a third diameter. The third diameter being larger than at least one of the first diameter and the second diameter.
    [0008] In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may include the fact that the middle section includes a clearance slot.
    [0009] In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may include the fact that the yoke includes a first set of parallel pivot holes, a second set of parallel pivot holes, a set of parallel through holes and a blind hole Helicoil.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may comprise a locking piston operatively connected to the yoke through a link, the link being operably connected to the first set of parallel pivot holes through a pivot axis, wherein the pivot axis is fixed in the first set of parallel pivot holes by the flange.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may comprise a support functionally connected to the yoke at the second set of holes. parallel pivot, through a biasing mechanism.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may include the fact that the screw cap fixed the crossbar to the yoke to through the blind hole Helicoil.
    According to another embodiment, a method of manufacturing a rocking mechanism of an emergency wind turbine actuator is described. The method includes forming a cross bar having a first section, a second section, and an average section between the first section and the second section. The method also includes forming a flange at the middle section, the flange having a through hole. The method also includes inserting a cross bar into a set of parallel through holes within a yoke, so that the flange is leaning against one side of the yoke. The method also includes installing a screw cap into the through hole of the flange to secure the cross bar to the yoke.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the method may include the fact that the clevis comprises a first set of parallel pivot holes, a second set of parallel pivot holes and a blind hole Helicoil.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the method may include operatively connecting a lock piston to the yoke through a link, the link being operatively connected to the first set of parallel pivot holes through a pivot axis, wherein the pivot axis is fixed in the first set of parallel pivot holes by the flange.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the rocker mechanism may include functionally connecting a support to the clevis at the second set of parallel pivot holes, through a biasing mechanism.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the method may include the fact that the screw cap fixes the cross bar to the yoke through the blind hole Helicoil.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the method may include the fact that the middle section includes a clearance slot.
    In addition to one or more of the features described above, or as an alternative, other embodiments of the method may include forming a flange by machining the middle section of the crossbar.
    The aforementioned features and elements may be combined in various combinations without exclusivity, except in case of express indication to the contrary. These features and elements, as well as the operation thereof, will become more clearly apparent in light of the following description and accompanying drawings. However, it should be understood that the following description and drawings are illustrative and exemplary and not limiting.
    BRIEF DESCRIPTION OF THE DRAWINGS
    The foregoing and other features and advantages of the present disclosure are apparent in light of the following detailed description taken in conjunction with the following accompanying drawings, in which: [0022] Figure 1 is a perspective view of a aircraft that can incorporate the embodiments of the present disclosure; Figure 2 is a perspective view of an emergency wind turbine module (RAT) which may incorporate the embodiments of the present disclosure; Figure 3 is a cross-sectional side view of an actuator used in the RAT module of Figure 2, according to one embodiment of the present disclosure; Figure 4 is an enlarged cross-sectional top view of the actuator of Figure 3, in accordance with one embodiment of the present disclosure; Figure 5 is a diagram of a rocker mechanism used in the actuator of Figure 3, according to an embodiment of the present disclosure; FIG. 6 is a diagram of an alternative rocking mechanism that can be used in the actuator of FIG. 3; Fig. 7 is a diagram of a cross bar used in the rocker mechanism of Fig. 5, according to one embodiment of the present disclosure; Fig. 8 is a diagram of an alternative cross bar used in the rocker mechanism of Fig. 6; Figure 9 is a cross-sectional diagram of a crossbar module and a clevis used in the tilting mechanism of Figure 5, in accordance with one embodiment of the present disclosure; and [0031] FIG. 10 is a cross-sectional diagram of a crossbar and alternate clevis module used in the rocker mechanism of FIG. 6.
    The detailed description explains the embodiments of the present disclosure, with the advantages and features, as an example with reference to the drawings.
    DETAILED DESCRIPTION
    Referring now to FIGS. 1 and 2, FIG. 1 illustrates a perspective view of an aircraft 2 which may incorporate the embodiments of the present disclosure. Figure 2 illustrates a perspective view of an emergency wind turbine module (RAT) 40 which may incorporate the embodiments of the present disclosure. The aircraft 2 comprises a fuselage 4 extending from a nose portion 6 to a tail portion 8 through a body portion 10. The body portion 10 encloses an aircraft cabin 14 which includes a compartment for the Crew 15 and a passenger compartment 16. The body portion 10 supports a first wing 17 and a second wing 18. The first wing 17 extends from a first root portion 20 to a first tip portion 21 through a first wing part 23. The first wing part 23 comprises a leading edge 25 and a trailing edge 26. The second wing 18 extends from a second root portion (not shown) to a second tip portion 31 to The second wing portion 33 comprises a leading edge 35 and a trailing edge 36. The tail portion 8 comprises a stabilizer 38.
    The aircraft 2 comprises an emergency wind turbine module (RAT) 40 mounted in the fuselage 4 or in the nose part 6. In case of need for additional electrical and / or hydraulic power, a hatch 54 in the fuselage 4 of the aircraft will open and an actuator 50 will operate to deploy the RAT module 40 in the air stream. As shown in FIG. 2, the RAT module 40 may comprise a turbine module 42, a gearbox module 44, a shaft module 48, a generator 46 and the actuator 50. When the turbine module 42 rotates , the rotational torque is transferred from the turbine module 42, through the speed box module 44, to a transmission shaft (not shown) in the strut module 48 and then to the generator 46. The generator 46 may be an electric generator, a hydraulic pump or at the same time an electric generator and a hydraulic pump.
    Referring now to FIGS. 3 and 4. FIG. 3 illustrates a cross-sectional side view of an actuator 50 used in the RAT module 40 of FIG. 2, in accordance with an embodiment of the present disclosure. Figure 4 illustrates an enlarged cross-sectional top view of the actuator 50 of Figure 3, in accordance with one embodiment of the present disclosure. In the illustrated embodiment, the actuator 50 comprises a rocker mechanism 100, solenoids 60 and a rod end 52. The rocker mechanism 100 may comprise a lock piston 110, a link 120, a yoke 200, crossbar 300 and a support 140. The rocker mechanism 100 functions as a centralized mechanism. The solenoids 60 pull on the transverse portion 300 to move the rocker mechanism 100 beyond its central position. Once the rocker mechanism 100 moves beyond its central position, the link 120 shifts and subsequently allows the blocking piston 110 to translate in the X direction. The blocking piston 110 was originally preloaded to translate into the X direction but was previously prevented from translating by the link 120. The movement of the lock piston 110 activates the actuator 50, and therefore, when the lock piston 110 completes its movement, the actuator 50 begins to translate the The end of the bar 52 will move and / or retract the RAT (eg, RAT 40 as shown in FIG. The force generated by the solenoids 60 imparts a large bending load on the crossbar 300. In addition, the preload on the lock piston 110 also imparts a large bending load on the cross bar 300. These forces can cause the bar to bend. 300 if it is not thick enough.
    Referring now to Figures 5 and 7, Figure 5 illustrates a schematic diagram of a rocker mechanism 100 used in the actuator 50 of Figure 3, in accordance with an embodiment of the present disclosure. Figure 7 illustrates a schematic of a crossbar 300 used in the latch mechanism 100 of Figure 5, according to one embodiment of the present disclosure. The rocker mechanism 100 comprises a yoke 200 and a transverse bar 300 operably connected to the yoke 200. The cross bar 300 having a first section 310, a second section 320 and an average section 330 between the first section 310 and the second section 310 section 320. The first section 310 has a first diameter D1, the second section 320 has a second diameter D2 and the middle section 330 has a third diameter D3. In addition, the middle section 330 includes a flange 340. The flange 340 may be formed by tooling the middle section 330 of the crossbar 300. In addition, the flange 340 may be rigidly connected to the middle section 330. In one embodiment, the flange 340 may be rigidly connected to the middle section by a weld at a junction 370. As illustrated, the flange 340 also includes a through hole 350. The middle section 330 also includes a notch 360. The clearance notch 360 allows the crossbar 300 to avoid hitting the link 120 when the locking piston 110 translates. The yoke 200 includes a first set of parallel pivot holes 210, a second set of parallel pivot holes 220, a set of parallel through holes 230 and a blind hole Helicoil 240. The toggle mechanism 100 may also include a connected support 140. in operation at the yoke 200 at the second set of parallel pivot holes 220, through a biasing mechanism 130. In one embodiment, the biasing mechanism 130 may be a spring.
    In the illustrated embodiment, the rocker mechanism 100 also comprises a screw cap 160 placed in the through hole 350. The screw cap 160 sets the crossbar 300 to the set of parallel through holes 230 of the yoke 200 The screw cap 160 fixes the crossbar 300 to the yoke 200 via the blind hole Helicoil 240. The screw cap 160 prevents the crossbar 300 from rotating in the yoke 200. If the cross bar 300 has bent due to heavy loads, and that it then rotates in the yoke 200, the central position can change for various rotational positions of the crossbar 300. In order to prevent the crossbar from bending, various changes have been incorporated into the crossbar 300 of Figure 7 versus alternative crossbar models.
    Referring now also to FIGS. 6 and 8, in addition to FIGS. 5 and 7. FIG. 6 illustrates a diagram of an alternative rocking mechanism 102 that may be used in the actuator 50 of FIG. FIG. 8 illustrates a diagram of an alternative crossbar 302 used in the reciprocating mechanism 102 of FIG. 6. Comparing the crossbar 300 of FIG. 7 with the reciprocating crossbar 302 of FIG. 8, it can be seen that the diameter (D1, D2 and D3) of the crossbar 300 is greater than the diameter D4 of the alternative crossbar 302. Having a larger diameter allows the cross bar 300 to withstand greater flex loads. In addition, the third diameter D3 may be larger than at least one of the first diameter D1 and the second diameter D2. Having a larger diameter in the central portion allows the crossbar 300 to be stronger where it is needed most. By cons, the alternative crossbar 302 comprises a notch 390 near the central portion of the alternative crossbar 302, which gives a smaller diameter D5. The smaller diameter D5 creates a point of weakness near the center of the alternative cross bar 302, where the bending loads are often high.
    Other differences in the crossbar 300 relative to the alternative crossbar 302 can be seen with the addition of the flange 340 on the crossbar 300. The flange 340 allows the pivot axis 184 connecting the link 120 to the yoke 200 to remain in the first set of parallel pivot holes 210 of the yoke 200. The pivot pin 184 can be threaded into a blind hole of the first set of parallel pivot holes 210 and then the flange 340 will cover the pivot axis 184 on the other hole. As shown in FIG. 6, the reciprocating mechanism 102 required a separate piece, called a retaining ring 188, to maintain the pivot axis 184 in its place.
    Referring now to FIGS. 9 and 10. FIG. 9 illustrates a cross-sectional diagram of a crossbar module 300 and clevis 200 used in the flip-flop mechanism 100 of FIG. carrying out the present disclosure. FIG. 10 illustrates a cross-sectional diagram of a crossbar module 302 and an alternate clevis 202 used in the rocker mechanism 102 of FIG. 6. In order to reduce Y-direction movement, the cross bar 300 is attached to the yoke 200 via the screw cap 160, so that the flange 340 abuts the yoke 200, as shown. The screw cap 160 is in the through hole 350 of the flange 340 and is screwed into the yoke 200 at the blind hole Helicoil 240. As shown in Fig. 10, the thickness of the reciprocating crossbar 302 is reduced to level of the notch 390, to receive a locking screw 190, which reduces the movement in the Y direction. The screw cap 160, the flange 340 and the blind hole Helicoil 240 in Figure 9 eliminates the need to reduce the thickness of the transverse bar 200 in the middle section 330, in contrast to the reciprocating cross bar 302. Advantageously, a thicker diameter at the middle section 330 helps to reinforce the crossbar 300 and make it more resistant when folded and / or fractured than the alternative transverse bar 302. But also, advantageously, the flange 340 of the transverse bar 300 eliminates the need for a retaining ring 188, which was necessary for the reciprocating crossbar 302 and the alternative clevis 202 of the module of FIG. 10. The elimination of the retaining ring 188 and the set screw 190 reduces the number of parts and simplifies the module.
    While the present disclosure has been described in detail in connection with only a limited number of embodiments, it will be readily understood that the present disclosure is not limited to these described embodiments. Instead, the present disclosure may be modified to incorporate any number of variations, alterations, substitutions, combinations and sub-combinations or equivalent arrangements not heretofore described, but which correspond to the spirit and scope of this disclosure. In addition, while various embodiments of the present disclosure have been described, it will be understood that aspects of the present disclosure may include only some of the described embodiments.
    权利要求:
    Claims (9)
    [1" id="c-fr-0001]
    CLAIMS: What is claimed:
    A crossbar for use in a tilting mechanism of an emergency wind turbine actuator, comprising: a first section; a second section; and a middle section between the first section and the second section, the middle section comprises a flange having a through hole; wherein the first section has a first diameter, the second section has a second diameter and the average section has a third diameter, the third diameter being larger than at least one of the first diameter and the second diameter.
    [2" id="c-fr-0002]
    The crossbar of claim 1, wherein: the middle section comprises a clearance notch.
    [3" id="c-fr-0003]
    A rocking mechanism of an emergency wind turbine actuator, comprising: a clevis; a cross bar operatively connected to the yoke, the cross bar having a first section, a second section and a middle section between the first section and the second section, the middle section comprises a flange having a through hole; and a screw cap placed in the through hole, the screw cap fixing the crossbar to the yoke.
    [4" id="c-fr-0004]
    The rocker mechanism of claim 3, wherein: the first section has a first diameter, the second section has a second diameter and the average section has a third diameter, the third diameter being larger than at least one first diameter and second diameter.
    [5" id="c-fr-0005]
    The rocker mechanism of claim 3, wherein: the middle section comprises a relief slot.
    [6" id="c-fr-0006]
    The rocker mechanism of claim 3, wherein: the yoke comprises a first set of parallel pivot holes, a second set of parallel pivot holes, a set of parallel through holes and a blind hole Helicoil.
    [7" id="c-fr-0007]
    The rocker mechanism of claim 6, further comprising: a lock piston operatively connected to the yoke through a link, the link being operably connected to the first set of parallel pivot holes through a pivot axis, wherein pivot axis is fixed in the first set of parallel pivot holes by the flange.
    [8" id="c-fr-0008]
    The rocker mechanism of claim 7, further comprising: a support operably connected to the yoke at the second set of parallel pivot holes through a biasing mechanism.
    [9" id="c-fr-0009]
    The rocker mechanism of claim 7, wherein: the screw cap secures the crossbar to the yoke via the blind hole Helicoil.
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    同族专利:
    公开号 | 公开日
    FR3048678B1|2020-09-11|
    US10829240B2|2020-11-10|
    US20170259934A1|2017-09-14|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US9976636B2|2015-04-22|2018-05-22|Hamilton Sundstrand Corporation|Locking mechanisms for ram air turbines|
    US10385784B2|2016-03-11|2019-08-20|Hamilton Sundstrand Corporation|Clevis link for toggle mechanism of ram air turbine actuator|
    US9821919B2|2016-03-11|2017-11-21|Hamilton Sundstrand Corporation|Ejection jack having a toggle assembly|
    US10829240B2|2016-03-11|2020-11-10|Hamilton Sundstrand Corporation|Cross rod for toggle mechanism of ram air turbine actuator|US10829240B2|2016-03-11|2020-11-10|Hamilton Sundstrand Corporation|Cross rod for toggle mechanism of ram air turbine actuator|
    EP3348486A1|2017-01-14|2018-07-18|Hamilton Sundstrand Corporation|Release mechanism|
    EP3741681A1|2019-05-24|2020-11-25|Hamilton Sundstrand Corporation|Locking and unlocking mechanism|
    法律状态:
    2018-02-19| PLFP| Fee payment|Year of fee payment: 2 |
    2019-02-20| PLFP| Fee payment|Year of fee payment: 3 |
    2020-02-20| PLFP| Fee payment|Year of fee payment: 4 |
    2021-02-19| PLFP| Fee payment|Year of fee payment: 5 |
    2022-02-18| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    US15/068,103|US10829240B2|2016-03-11|2016-03-11|Cross rod for toggle mechanism of ram air turbine actuator|
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