• 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 dynamic air turbine control valve includes a sleeve, a body and a return housing. The sleeve defines a first output port disposed proximate a first end of the sleeve and defines a second output port disposed between the first output port and the first end. The body is contained radially in the sleeve and is movable between a first position and a second position. The return housing is coupled to the first end of the sleeve and defines a cavity that receives a biasing member that engages the body.
    公开号:FR3048677A1
    申请号:FR1751962
    申请日:2017-03-10
    公开日:2017-09-15
    发明作者:Stephen Michael Bortoli；William E Seidel
    申请人:Hamilton Sundstrand Corp；
    IPC主号:
    专利说明:

    DYNAMIC AIR TURBINE ACTUATOR SYSTEM TECHNOLOGICAL BACKGROUND
    The present disclosure relates to a dynamic air turbine actuator system having a dynamic air turbine control valve.
    Some aircraft are provided with an auxiliary power source which can be pneumatic. The auxiliary power source is sometimes referred to as a dynamic air turbine and is movable between a retracted position in which the dynamic air turbine is received in the fuselage of the aircraft and an extended position in which the dynamic air turbine is disposed. outside the fuselage of the plane. The dynamic air turbine is deployed and / or retracted by a dynamic air turbine actuator system.
    BRIEF DESCRIPTION
    [0003] According to one embodiment of the present disclosure, a dynamic air turbine actuator system is provided. The dynamic air turbine actuator system includes an actuator assembly and a dynamic air turbine control valve. The actuator assembly is configured to selectively allow the deployment and retraction of a dynamic air turbine. The dynamic air turbine control valve is hydraulically connected to the actuator assembly and includes a sleeve and a body. The sleeve has a first output port disposed proximate a first end of the sleeve and has a second output port disposed between the first output port and the first end. The body is contained radially in the sleeve. The body has a first seal plate disposed proximate the first end of the sleeve and has a second seal plate disposed proximate a second end of the sleeve.
    [0004] According to another embodiment of the present disclosure, a dynamic air turbine control valve is provided. The dynamic air turbine control valve includes a sleeve, a body and a return housing. The sleeve has a sleeve body defining an internal bore. The sleeve body extends between a first end and a second end and defines a first output port disposed proximate the first end and defines a second output port disposed between the first output port and the first end. The body is contained radially in the internal bore and is movable between a first position and a second position. The return housing is coupled to the first end of the sleeve and defines a cavity that receives a biasing member that engages the body and prestresses the body to the first position.
    In one aspect, a dynamic air turbine actuator system comprises: an actuator assembly configured to selectively deploy and retract a dynamic air turbine; and a dynamic air turbine control valve hydraulically connected to the actuator assembly, the dynamic air turbine control valve comprising: a sleeve having a first output port disposed proximate a first end of the sleeve and having a second output port disposed between the first output port and the first end, and a body contained radially in the sleeve, the body having a first seal plate disposed proximate the first end of the sleeve and having a second end plate. seal disposed near a second end of the sleeve.
    [0006] The dynamic air turbine actuator system may include the following limitations, isolated or in combination: • the first gasket plate defines a first plurality of sealing splines. The second seal plate defines a second plurality of sealing splines. The dynamic air turbine control valve further comprises: a return housing coupled to the first end of the sleeve, the return housing defining a cavity which receives a biasing member which engages the body and prestresses the body to a first position which corresponds to a retracted position of the dynamic air turbine. • When the body is in the first position, the first seal plate blocks the first output port and the second output port. The first output port has a first output port diameter and the second output port has a second output port diameter that is smaller than the first output port diameter.
    According to one aspect, a dynamic air turbine control valve comprises: a sleeve having a body defining an internal bore, the body extending between a first end and a second end, the body defining a first port of outlet disposed proximate the first end and defining a second output port disposed between the first output port and the first end; a body contained radially in the internal bore, the body being movable between a first position and a second position; and a return housing coupled to the first end of the sleeve, the return housing defining a cavity that receives a biasing member that engages the body and prestresses the body to the first position.
    The dynamic air turbine control valve may include the following limitations, isolated or in combination: the first output port and the second output port are disposed between a first sealing groove and a second spline; sealing defined by the sleeve. Where the first output port has a first output port diameter and the second output port has a second output port diameter. O the second output port diameter is smaller than the first output port diameter. Wherein the body comprises a first body portion that engages the biasing member and a second body portion disposed opposite the first body portion. The second body portion defines a first seal plate having a first plurality of flutes. O when the body is in the first position, the first seal plate blocks the second output port and the first output port. O when the body moves from the first position to the second position, the second output port is exposed prior to the exposure of the first output port. The second body portion defines a second seal plate having a second plurality of grooves, the second seal plate being disposed proximate the second end of the sleeve.
    BRIEF DESCRIPTION OF THE DRAWINGS
    The foregoing and other features and advantages of the present disclosure will become apparent from the following detailed description when considered in conjunction with the accompanying drawings in which: [0010] Figure 1 is a side view of a dynamic air turbine actuator system; [0011] Fig. 2 is a side view of a dynamic air turbine control valve in a first position; Figure 3 is a side view of a dynamic air turbine actuator valve moving to a second position; and [0013] Fig. 4 is a side view of a dynamic air turbine actuator valve in a second position.
    DETAILED DESCRIPTION
    Referring now to the figures, for which the invention will be described with reference to specific embodiments, without limiting them, it will be understood that the embodiments described are only an illustration of the invention. which can be made of various other forms. Various elements of the described embodiments may be combined or omitted to form other embodiments of the invention. The figures are not necessarily scaled; some features may be exaggerated or understated to show the details of particular components. Therefore, the specific structural and functional details described herein should not be construed as limiting, but merely as a representative basis for teaching the skilled person to use the present invention in a variety of ways.
    Throughout the present specifications, the terms "fix", "fixation", "connected", "coupled", "coupling", "mounting" or "mounting" must be interpreted as meaning that a component or element The structural element is in some way connected to or in contact with another element, either directly or indirectly by means of at least one structural element involved or integral with the other structural element.
    Referring to Figure 1, a dynamic air turbine actuator system 10 is shown. The dynamic air turbine actuator system 10 is operatively connected to a dynamic air turbine at a first end and is connected to an aircraft structure at a second end. The dynamic air turbine is movable between a retracted position and a deployed position by the action of the dynamic air turbine actuator system 10. The dynamic air turbine, when in the deployed position, interacts with an air flow. moving air to provide electrical power or hydraulic power to an aircraft. The dynamic air turbine, when in the retracted position, does not provide power to the aircraft. The dynamic air turbine actuator system 10 includes an actuator assembly 12, a latch assembly 14, and a dynamic air turbine control valve 16 hydraulically or hydraulically connected to the actuator assembly 12.
    The actuator assembly 12 is configured to move the dynamic air turbine selectively between the deployed position and the retracted position. During a retraction event, during which the dynamic air turbine moves from the deployed position to the retracted position, a hydraulic system 20 provides hydraulic pressure to the dynamic air turbine control valve 16 and ultimately to the Actuator assembly 12. Providing hydraulic pressure to the dynamic air turbine control valve 16 causes the dynamic air turbine to move to the retracted position in the aircraft. Towards the end of the retraction event, the hydraulic pressure is released on the dynamic air turbine control valve 16, if the release of the hydraulic pressure would not be precisely controlled, the latch assembly 14 might not be remain locked and the dynamic air turbine could be inadvertently redeployed. The configuration of the dynamic air turbine control valve 16 is configured to control the rate of release of the hydraulic pressure to inhibit the inadvertent redeployment of the dynamic air turbine.
    Referring to Figures 2 to 4, the control valve of the dynamic air turbine 16 comprises an actuator housing 30 which receives a sleeve 32, a body 34, a return housing 36 and a lining housing 38 The sleeve 32 comprises a sleeve body 40 which extends between a first end 42 and a second end 44. The sleeve body 40 comprises an outer surface 50, an inner surface 52 disposed opposite the outer surface 50 and a internal bore 54 which is defined by the inner surface 52 of the sleeve body 40.
    The outer surface 50 defines a first sealing groove 60, a second sealing groove 62, a third sealing groove 64 and a fourth sealing groove 66. The first sealing groove 60 is arranged to near the first end 42 of the sleeve body 40. The second sealing groove 62 is disposed between the first sealing groove 60 and the third sealing groove 64. The third sealing groove 64 is disposed between the second sealing groove 62 and the second sealing groove 64. sealing groove 62 and the fourth sealing groove 66. The fourth sealing groove 66 is disposed near the second end 44 of the sleeve body 40. Each sealing groove is configured to receive a sealing member , such as an O-ring, or the equivalent. Each sealing member is configured to engage an inner surface of the actuator housing 30 and a portion of the outer surface 50.
    The sleeve body 40 defines a first output port 70 and a second output port 72. The first output port 70 and the second output port 72 are hydraulically connected to the hydraulic system 20 and are configured to provide pressure. to the interior components of the dynamic air turbine control valve 16. The first output port 70 is disposed near the first end 42 of the sleeve body 40. The first outlet port 70 extends from the outer surface. 50 to the inner surface 52. The first output port 70 is disposed between the first sealing groove 60 and the second sealing groove 62. The first output port 70 is disposed closer to the second spline 60. Sealing 62 as the first sealing groove 60. The first output port 70 has a first output port diameter. The second output port 72 is spaced from the first output port 70. The second output port 72 is disposed between the first output port 70 and the first end 42 of the sleeve body 40. The second output port 72 extends from the outer surface 50 to the inner surface 52. The second output port 72 is disposed between the first sealing groove 60 and the second sealing groove 62. The second output port 72 is disposed over next to the first sealing groove 60 as the second sealing groove 62. The second output port 72 has a second output port diameter which is smaller than the first output port diameter. The first output port diameter is greater than the second output port diameter.
    The body 34 is contained radially in the sleeve 32. The body 34 is received in the internal bore 54 of the sleeve body 40. The body 34 is movable between a first position (as shown in Figure 2) which corresponds to a position in which the dynamic air turbine actuator system 10 is in retraction or in a powered position and a second position (as shown in Fig. 4) which corresponds to a dormant position of the actuator system of a dynamic air turbine 10 in which the dynamic air turbine actuator system 10 is retracted, deployed or being deployed. The selective supply of hydraulic pressure by the hydraulic system 20 to the dynamic air turbine control valve 16 causes the translation of the body 34 between the first position and the second position.
    The body 34 includes a first body portion 80 and a second body portion 82. The first body portion 80 extends through the sleeve 32 and is received in the return housing 36. The first body portion 80 comprises a flange or a peripheral edge 90. The peripheral edge 90 has a diameter which is greater than a diameter of the internal bore 54 of the sleeve body 40 of the sleeve 32. The peripheral edge 90 is dimensioned so that one end of the first body portion 80 does not extend into the inner bore 54 of the sleeve body 40 of the sleeve 32 as the body 34 moves toward or is in the second position.
    The second body portion 82 is disposed opposite the first body portion 80. The second body portion 82 defines a first gasket plate 92 and a second gasket plate 94. The first gasket plate 92 is extends from an outer surface of the second body portion 82 to the inner surface 52 of the sleeve body 40. The first seal plate 92 is disposed between a first end of the body 34 and a second end of the body 34. Seal 92 defines a first plurality of sealing splines 100. The first plurality of sealing splines 100 extend around a circumference of the first gasket plate 92. The first plurality of sealing splines 100 is configured to assist to establish a pressure balance between the opposite faces of the body 34.
    The second seal plate 94 is disposed near the second end of the body 34. The second seal plate 94 extends from the outer surface of the second body portion 82 to the inner surface 52 of the sleeve body. 40. The second seal plate 94 defines a second plurality of sealing splines 102. The second plurality of sealing splines 102 extends around a circumference of the second gasket plate 94. The second plurality of splines 102 Sealing 102 is configured to help establish a pressure balance between opposing faces of the body 34.
    The return housing 36 extends into the actuator housing 30. The return housing 36 is coupled to the first end 42 of the sleeve body 40 of the sleeve 32. The return housing 36 defines a cavity 110 which receives a prestressing element 112. The prestressing element 112 is configured to engage the peripheral edge 90 of the first body portion 80 of the body 34. The prestressing element 112 is configured to prestress the body 34 to the second position.
    The packing housing 38 extends into the actuator housing 30. The seal housing 38 is coupled to the second end 44 of the sleeve body 40 of the sleeve 32. The seal housing 38 includes a tray 120 having a retraction liner assembly 122 which selectively provides hydraulic pressure from the hydraulic system 20 to at least the second end 44 of the sleeve body 40 of the sleeve 32 to move the body 34 from the second position to the first position. The retraction liner assembly 122 allows the transfer of pressure to move the body 34.
    The hydraulic pressure of the retraction liner assembly 122 will reach the dynamic air turbine control valve 16 through a port 74 disposed between the retraction liner assembly 122 and the liner housing 38 proximate the the second end 44 of the sleeve body 40. There is thus a hole between 122 and 38. High hydraulic pressure is provided through the port 74 and the body 34 is forcibly placed in the first position as shown in FIG. Movement of the body 34 displaces the dynamic air turbine control valve 16 to cause retraction of the dynamic air turbine actuator.
    While the body 34 is in the first position, as shown in Figure 2, the first seal plate 92 blocks the first output port 70 and the second output port 72 to inhibit the output of the hydraulic pressure. of the inner bore 54 of the sleeve 32. The retraction liner assembly 122 presses to block the supply of hydraulic pressure to the dynamic air turbine control valve 16 and opens a dynamic air turbine control valve return. in response to the departure of a retraction event from the dynamic air turbine. When the retraction liner assembly 122 closes or stops providing hydraulic pressure through port 74, the hydraulic pressure at the end of the body 34 near the second end 44 of the sleeve body 40 will decrease and will flow through the retraction liner assembly 122. The hydraulic pressure drop causes the prestressing member 112 to press against the first body portion 80 to assist movement of the body 34 from the position shown in FIG. the position illustrated in Figure 3 to the position in Figure 4. When the body 34 moves to the second position, as shown in Figure 3, the first joint plate 92 discovers, exposes or unblocks the second port 72 to begin releasing the hydraulic pressure of the inner bore 54 of the sleeve body 40 of the sleeve 32. The second output port 72 is exposed before the first port Exit 70 is exposed. Opening or exposing the second output port 72 begins to reduce the hydraulic pressure at a first rate.
    When the body 34 continues to move to the second position, as shown in Figure 4, the first joint plate 92 discovers, exposes or unblocks the first output port 70 to further release the hydraulic pressure of the internal bore 54 of the sleeve body. Opening or exposing the first output port 70 reduces the hydraulic pressure to a second flow rate that is greater than the first flow rate. Opening the second output port 72 before the first output port 70 reduces an impact velocity of a lock piston that is associated with the latch assembly 14. The reduction of the impact velocity of the The lock associated with the latch assembly 14 decreases the force of the lock piston to ensure that the latch assembly 14 remains locked and the dynamic air turbine remains retracted.
    If the present disclosure has been described in detail with respect to only a limited number of embodiments, it will be readily understood that the present disclosure is not limited to these disclosed embodiments. On the contrary, the present disclosure may be modified to incorporate any number of variants, modifications, substitutions or equivalent arrangements not heretofore described, but which are within the spirit and scope of the present invention. In addition, although various embodiments of the present disclosure have been described, it should be understood that aspects of the present disclosure may include only some of the described embodiments. Therefore, the present disclosure should not be construed as limited by the foregoing description.
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    A dynamic air turbine actuator system, comprising: an actuator assembly configured to selectively deploy and retract a dynamic air turbine; and a dynamic air turbine control valve hydraulically connected to the actuator assembly, the dynamic air turbine control valve comprising: a sleeve having a first output port disposed proximate a first end of the sleeve and having a second output port disposed between the first output port and the first end, and a body contained radially in the sleeve, the body having a first seal plate disposed proximate the first end of the sleeve and having a second end plate. seal disposed near a second end of the sleeve.
    [2" id="c-fr-0002]
    The dynamic air turbine actuator system of claim 1, wherein the first seal plate defines a first plurality of sealing splines.
    [3" id="c-fr-0003]
    The dynamic air turbine actuator system of claim 2, wherein the second seal plate defines a second plurality of sealing splines.
    [4" id="c-fr-0004]
    The dynamic air turbine actuator system of claim 2, wherein the dynamic air turbine control valve further comprises: a return housing coupled to the first end of the sleeve, the return housing defining a cavity which receives a biasing member which engages the body and prestresses the body to a first position which corresponds to a retracted position of the dynamic air turbine.
    [5" id="c-fr-0005]
    The dynamic air turbine actuator system of claim 4, wherein, when the body is in the first position, the first seal plate blocks the first output port and the second output port.
    [6" id="c-fr-0006]
    The dynamic air turbine actuator system of claim 2, wherein the first output port has a first output port diameter and the second output port has a second output port diameter that is smaller than the first output port diameter. output port diameter.
    [7" id="c-fr-0007]
    A dynamic air turbine control valve, comprising: a sleeve having a body defining an internal bore, the body extending between a first end and a second end, the body defining a first output port disposed proximate the first end and defining a second output port disposed between the first output port and the first end; a body contained radially in the internal bore, the body being movable between a first position and a second position; and a return housing coupled to the first end of the sleeve, the return housing defining a cavity that receives a biasing member that engages the body and prestresses the body to the first position.
    [8" id="c-fr-0008]
    The dynamic air turbine control valve according to claim 7, wherein the first output port and the second output port are disposed between a first sealing groove and a second sealing spline defined by the sleeve.
    [9" id="c-fr-0009]
    The dynamic air turbine control valve of claim 7, wherein the first output port has a first output port diameter and the second output port has a second output port diameter.
    [10" id="c-fr-0010]
    The dynamic air turbine control valve of claim 9, wherein the second output port diameter is smaller than the first output port diameter.
    [11" id="c-fr-0011]
    The dynamic air turbine control valve of claim 7, wherein the body comprises a first body portion that engages the biasing member and a second body portion disposed opposite the first body portion. .
    [12" id="c-fr-0012]
    The dynamic air turbine control valve of claim 11, wherein the second body portion defines a first gasket plate having a first plurality of flutes.
    [13" id="c-fr-0013]
    The dynamic air turbine control valve of claim 12, wherein, when the body is in the first position, the first seal plate blocks the second output port and the first output port.
    [14" id="c-fr-0014]
    The dynamic air turbine control valve of claim 13, wherein, as the body moves from the first position to the second position, the second output port is exposed prior to exposure of the first output port.
    [15" id="c-fr-0015]
    The dynamic air turbine control valve of claim 14, wherein the second body portion defines a second seal plate having a second plurality of grooves, the second seal plate being disposed proximate the second end of the sleeve. .
    类似技术:
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    同族专利:
    公开号 | 公开日
    FR3048677B1|2020-12-11|
    US20170261017A1|2017-09-14|
    US9976579B2|2018-05-22|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4993781A|1989-09-21|1991-02-19|The Boeing Company|Antijam brake-metering valve and method for its use|
    BRPI0519955A2|2005-02-11|2009-04-07|Bell Helicopter Textron Inc|actuator control system; video control system; and control method of said actuator|
    US9193472B2|2012-06-06|2015-11-24|Hamilton Sundstrand Corporation|Electromechanical actuator lubrication system for ram air turbine|EP2399926A1|2010-06-22|2011-12-28|Justus-Liebig-Universität Giessen|Peptides incorporating 3-aminoadamantane carboxylic acids enhance synaptic plasticity and act as neurogenic agents|
    EP3112270B1|2015-06-29|2019-09-04|Hamilton Sundstrand Corporation|Unlocking mechanism for ram air turbine actuator|
    EP3575645A1|2018-06-01|2019-12-04|Hamilton Sundstrand Corporation|Device for pilot valve|
    US20210254639A1|2020-02-14|2021-08-19|Hamilton Sundstrand Corporation|Hydraulic control valves for ram air turbine stow actuators|
    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 |
    2019-12-20| PLSC| Publication of the preliminary search report|Effective date: 20191220 |
    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
    US15/067,853|US9976579B2|2016-03-11|2016-03-11|Ram air turbine actuator system|
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