WO2011046687A1 - Damage impactor - Google Patents

Damage impactor Download PDF

Info

Publication number
WO2011046687A1
WO2011046687A1 PCT/US2010/047985 US2010047985W WO2011046687A1 WO 2011046687 A1 WO2011046687 A1 WO 2011046687A1 US 2010047985 W US2010047985 W US 2010047985W WO 2011046687 A1 WO2011046687 A1 WO 2011046687A1
Authority
WO
WIPO (PCT)
Prior art keywords
actuator
damage
assembly
lift
impactor
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.)
Ceased
Application number
PCT/US2010/047985
Other languages
French (fr)
Inventor
Donald E. Powers
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of WO2011046687A1 publication Critical patent/WO2011046687A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/30—Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force, e.g. by falling weight
    • G01N3/307—Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force, e.g. by falling weight generated by a compressed or tensile-stressed spring; generated by pneumatic or hydraulic means
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00—Vibration-testing of structures; Shock-testing of structures
    • G01M7/08—Shock-testing
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0058—Kind of property studied
    • G01N2203/0076—Hardness, compressibility or resistance to crushing
    • G01N2203/0087—Resistance to crushing

Definitions

  • This invention relates to destructive testing, and more particularly to a damage impactor.
  • a damage impactor which is comprised of a housing defining a passage, an impact assembly, an actuator assembly, and an engagement assembly.
  • the impact assembly comprises a guide rod comprising an impact head, and a bias mechanism to bias the guide rod in a first direction.
  • the actuator assembly comprises an actuator, and an actuator rod coupled to the actuator.
  • the engagement assembly selectively couples the impact assembly to the actuator assembly by driving the actuator rod in the first direction to an engagement position where the engagement assembly couples the actuator rod to the guide rod, retracting the actuator rod in a second direction, opposite the first direction, to a release position; and releasing the guide rod from the actuator rod.
  • an engagement assembly to couple a first moveable shaft to a second moveable shaft.
  • the engagement assembly comprises a plurality of lift jaw members pivotably mounted to a distal end of the first shaft, and pivotable between a first position in which the lift jaw members engage a lift ring on the second shaft and a second position in which the lift jaw members disengage from a lift ring on the second shaft, a clamp ring to retain the lift jaw members into the first position, and a release ring to disengage the lift jaw members from the clamp ring.
  • a method to apply an impact damage to a surface In one embodiment the method comprises positioning a damage impactor proximate to a surface.
  • the damage impactor comprises a housing defining a passage, an impact assembly comprising a guide rod comprising an impact head, a bias mechanism to bias the guide rod in a first direction, an actuator assembly, comprising an actuator, an actuator rod coupled to the actuator, and an engagement assembly to selectively couple the impact assembly to the actuator assembly.
  • the method further comprises activating the actuator assembly to drive the actuator rod in the first direction to an engagement position where the engagement assembly couples the actuator rod to the guide rod to retract the actuator rod in a second direction, opposite the first direction, to a release position, and release the guide rod from the actuator rod.
  • FIG. 1 is a schematic illustration of a damage impactor in accordance with some embodiments.
  • FIG. 2 is a schematic illustration of an engagement assembly for a damage impactor, according to embodiments.
  • FIG. 3 is a schematic illustration of an engagement assembly for a damage impactor, according to embodiments.
  • FIG. 4 is a flowchart illustrating operations in a method to use a damage impactor, according to embodiments.
  • a damage impactor 100 is depicted.
  • the damage impactor comprises a housing 110, an impact assembly 120, an actuator assembly 140, and an engagement assembly 160 to selectively couple the impact assembly 120 to the actuator assembly 140.
  • the housing 110 comprises a plurality of support arms 116 mounted to the housing 110.
  • the impact assembly 120 comprises a guide rod 122 comprising an impact head 124 mounted on a distal end of the guide rod 122, and a bias mechanism 126 to bias the guide rod in a first direction, i.e., in a direction toward the impact head 124.
  • the bias mechanism 126 comprises a compression spring which biases the impact assembly in the first direction. The compression spring is compressed between a first reaction plate 128 and a second reaction plate 130. The first reaction plate 128 remains in a substantially fixed position in the housing 110.
  • the second reaction plate 130 is attached to a distal end of guide rod 122, between the end of guide rod 122 and impact head 124, all of which are moveable within the housing 110.
  • the interior surface of the housing 110 comprises a plurality of guides 112 which guide second reaction plate 130 in position as it moves within the housing 110.
  • the guides 112 comprise narrow strips running axially on the interior of the housing 110 which are formed from a material which facilitates the movement of the second reaction plate 130 within the housing, e.g., Teflon®, or the like.
  • the impactor assembly 120 further comprises a stroke limit plate
  • the compression spring 126 has a spring constant that measures between 250 Lbf/inch and 750 Lbf/inch, and preferably about 500 Lbf/inch. The various spring constants allow different ranges of impact energies to be achieved with the same apparatus and with better accuracy.
  • the actuator assembly 140 extends and retracts the actuator rod 144 within the housing 110.
  • the actuator assembly 140 comprises an actuator 142 and an actuator rod 144 coupled to the actuator 142.
  • the actuator may be implemented as one or more of a hydraulic actuator, a pneumatic actuator, an electromagnetic actuator, or the like.
  • the particular implementation of the actuator will be a function of design parameters, e.g., the amount of force required to retract the compression spring 126 to achieve a desired energy level.
  • the actuator 142 may be embodied as a hydraulic actuator.
  • the engagement assembly 160 operates to selectively couple the impact assembly 120 to the actuator assembly 140.
  • the engagement assembly 160 comprises a plurality of lift jaw members 162 pivotably mounted to a pivot block 168 on the distal end of the actuator rod 144, and pivotable between a first position in which the lift jaw members 162 engage a lift ring 180 on the guide rod 122 and a second position in which the lift jaw members 162 disengage from a lift ring 180 on the guide rod 122.
  • the plurality of lift jaw members 162 comprise a key- shaped lower outer surface 164.
  • the lift ring 180 comprises a key- shaped inner surface 182, such that the when the lift jaw 162 engages the lift ring, the key-shaped outer surface of the lift jaw members 162 engages with the key- shaped inner surface 182 of the lift ring 180.
  • the engagement assembly 160 further comprises a clamp ring 170 to retain the lift jaw members 162 into the first position, and a release ring 190 to disengage the lift jaw members 162 from the clamp ring 170.
  • the plurality of lift jaw members 162 further comprise a key- shaped upper outer surface 166 such that the clamp ring 170 engages the key- shaped upper surface 166 with a friction fit, when the actuator rod 144 is fully extended to the engagement position, thereby locking the lift jaw members 166 to the lift ring 180.
  • the release ring 190 functions to block motion of the clamp ring
  • the position of the release ring 190 is adjustable, such that the retraction stroke length of the impactor assembly is variable.
  • the clamp ring 190 is disposed on a mount 194 that is mounted on threads 192 on the housing, such that the position of clamp ring 190 can be adjusted by rotating the mount 194 with respect to the threads.
  • a top plate 196 provides the means to physically adjust the position of release ring 190. In this embodiment the outer circumference of the top plate 196 is knurled to improve the ability to spin the threaded mount 194.
  • the particular materials from which the damage impactor 100 are formed are not critical and are primarily a function of design necessity to support the forces generated by the compression spring 126.
  • the various components of the damage impactor 100 are formed from steel or another suitable metal.
  • the particular size of the impactor 100 and its components is not critical.
  • the dimensions of the impactor are primarily a function of design necessity in order to encompass the apparatus to afford functionality and safety considerations.
  • the damage impactor 100 measures approximately 75 inches in height, and 6 inches in diameter, and supports a stroke length of between 3 inches and 12 inches, such that the impactor can deliver an impact force between 800 foot-pounds and 2000 footpounds via the impact head 124.
  • Fig. 4 is a flowchart illustrating operations in a method to use a damage impactor, according to embodiments.
  • the damage impactor 100 is positioned proximate the surface to be tested such that the impact head is in contact with the surface before the actuator assembly retracts the actuator rod.
  • the damage impactor 100 may be positioned at any angle with respect to the surface, and at any angle with respect to the Earth.
  • the damage impactor 100 may be secured in place by rigging the support arms 116 to external support members.
  • the position of the release ring may be adjusted to adjust the force on the compression spring. As described above, this adjustment may be accomplished by rotating the mount 194 with respect to the threads 192 on the housing.
  • the actuator assembly 140 is activated. As described above, the actuator 142 may be a hydraulic actuator. Activating the actuator assembly drives the actuator rod 144 in a first direction toward the distal end of the damage impactor 100 to an engagement position where the engagement assembly 160 engages (operation 420) the actuator rod 144 and the guide rod 122.
  • the engagement assembly reaches the engagement position the plurality of lift jaw members 162 are forced into position to engage the lift ring on the impactor guide rod 122 by engaging the clamping ring 170 with the upper surface 166 of the lift jaws.
  • the actuator rod 144 continues to extend in the distal direction, the clamping ring 170 is forcefully driven onto the top surfaces of the lift jaw members 166, creating a friction fit locking the clamping ring 170 onto the upper surface of the lift jaw members 166.
  • the actuator rod 144 is then retracted (operation 420) in a second direction, opposite the first direction. As the actuator rod 144 retracts the upper surface 166 of the lift jaw members 162 engages the lower surface 182 of the lift ring, such that the lower surface 164 of the lift jaw members 162 is engaged with the surface 182 of the lift ring 180.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

A damage impactor comprises a housing (110) defining a passage, an impact assembly (120), an actuator assembly, and an engagement assembly (160).The impact assembly comprises a guide rod comprising an impact head (124), and a bias mechanism to bias the guide rod in a first direction. The actuator assembly comprises an actuator, and an actuator rod (144) coupled to the actuator. The engagement assembly (160) selectively couples the impact assembly to the actuator assembly by driving the actuator rod in the first direction to an engagement position where the engagement assembly couples the actuator rod to the guide rod, retracting the actuator rod in a second direction, opposite the first direction, to a release position and releasing the guide rod from the actuator rod. Other embodiments are also disclosed.

Description

DAMAGE IMPACTO
FIELD OF THE DISCLOSURE
[0001] This invention relates to destructive testing, and more particularly to a damage impactor.
BACKGROUND
[0002] Various applications require impact damage assessment of one or more components. By way of example, composite materials for use in aircraft require impact testing to demonstrate that the materials remain safe to fly after low velocity/high energy impact damage has occurred. Such impact damage often requires substantial energy levels (i.e., in excess of 2,000 ft-lbs) to be imparted at virtually any angle, on any surface. Thus, apparatus and methods for impact damage testing may find utility.
SUMMARY
[0003] In various aspects, apparatus and methods for damage testing are provided. In one aspect there is provided a damage impactor which is comprised of a housing defining a passage, an impact assembly, an actuator assembly, and an engagement assembly. In one embodiment the impact assembly comprises a guide rod comprising an impact head, and a bias mechanism to bias the guide rod in a first direction. The actuator assembly comprises an actuator, and an actuator rod coupled to the actuator. The engagement assembly selectively couples the impact assembly to the actuator assembly by driving the actuator rod in the first direction to an engagement position where the engagement assembly couples the actuator rod to the guide rod, retracting the actuator rod in a second direction, opposite the first direction, to a release position; and releasing the guide rod from the actuator rod.
[0004] In another aspect there is provided an engagement assembly to couple a first moveable shaft to a second moveable shaft. In one embodiment, the engagement assembly comprises a plurality of lift jaw members pivotably mounted to a distal end of the first shaft, and pivotable between a first position in which the lift jaw members engage a lift ring on the second shaft and a second position in which the lift jaw members disengage from a lift ring on the second shaft, a clamp ring to retain the lift jaw members into the first position, and a release ring to disengage the lift jaw members from the clamp ring. [0005] In yet another aspect there is provided a method to apply an impact damage to a surface. In one embodiment the method comprises positioning a damage impactor proximate to a surface. In one embodiment the damage impactor comprises a housing defining a passage, an impact assembly comprising a guide rod comprising an impact head, a bias mechanism to bias the guide rod in a first direction, an actuator assembly, comprising an actuator, an actuator rod coupled to the actuator, and an engagement assembly to selectively couple the impact assembly to the actuator assembly. The method further comprises activating the actuator assembly to drive the actuator rod in the first direction to an engagement position where the engagement assembly couples the actuator rod to the guide rod to retract the actuator rod in a second direction, opposite the first direction, to a release position, and release the guide rod from the actuator rod.
[0006] The features, functions and advantages discussed herein can be achieved independently in various embodiments described herein or may be combined in yet other embodiments, further details of which can be seen with reference to the following description and drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0007] The detailed description is described with reference to the accompanying figures.
[0008] Fig. 1 is a schematic illustration of a damage impactor in accordance with some embodiments.
[0009] Fig. 2 is a schematic illustration of an engagement assembly for a damage impactor, according to embodiments.
[0010] Fig. 3 is a schematic illustration of an engagement assembly for a damage impactor, according to embodiments.
[001 1] Fig. 4 is a flowchart illustrating operations in a method to use a damage impactor, according to embodiments.
DETAILED DESCRIPTION
[0012] Described herein are exemplary apparatus and methods for impact damage testing. In the following description, numerous specific details are set forth to provide a thorough understanding of various embodiments. However, it will be understood by those skilled in the art that the various embodiments may be practiced without the specific details. In other instances, well-known methods, procedures, components, and circuits have not been illustrated or described in detail so as not to obscure the particular embodiments.
[0013] Referring to Figs. 1-3, one embodiment of a damage impactor will be described. Referring first to Fig. 1 , a damage impactor 100 is depicted. In the embodiment depicted in Fig. 1, the damage impactor comprises a housing 110, an impact assembly 120, an actuator assembly 140, and an engagement assembly 160 to selectively couple the impact assembly 120 to the actuator assembly 140. In one embodiment the housing 110 comprises a plurality of support arms 116 mounted to the housing 110.
[0014] In the embodiment depicted in Figs. 1-3, the impact assembly 120 comprises a guide rod 122 comprising an impact head 124 mounted on a distal end of the guide rod 122, and a bias mechanism 126 to bias the guide rod in a first direction, i.e., in a direction toward the impact head 124. In the embodiment depicted in Fig. 1, the bias mechanism 126 comprises a compression spring which biases the impact assembly in the first direction. The compression spring is compressed between a first reaction plate 128 and a second reaction plate 130. The first reaction plate 128 remains in a substantially fixed position in the housing 110. The second reaction plate 130 is attached to a distal end of guide rod 122, between the end of guide rod 122 and impact head 124, all of which are moveable within the housing 110. The interior surface of the housing 110 comprises a plurality of guides 112 which guide second reaction plate 130 in position as it moves within the housing 110. In one embodiment the guides 112 comprise narrow strips running axially on the interior of the housing 110 which are formed from a material which facilitates the movement of the second reaction plate 130 within the housing, e.g., Teflon®, or the like.
[0015] The impactor assembly 120 further comprises a stroke limit plate
132 which is fixedly mounted to the proximal end of guide rod 122 opposite of the impact head and which serves to limit the stroke length of the impact assembly. In some embodiments the compression spring 126 has a spring constant that measures between 250 Lbf/inch and 750 Lbf/inch, and preferably about 500 Lbf/inch. The various spring constants allow different ranges of impact energies to be achieved with the same apparatus and with better accuracy.
[0016] The actuator assembly 140 extends and retracts the actuator rod 144 within the housing 110. In the embodiment depicted in Fig. 1, the actuator assembly 140 comprises an actuator 142 and an actuator rod 144 coupled to the actuator 142. The actuator may be implemented as one or more of a hydraulic actuator, a pneumatic actuator, an electromagnetic actuator, or the like. The particular implementation of the actuator will be a function of design parameters, e.g., the amount of force required to retract the compression spring 126 to achieve a desired energy level. In the embodiment depicted in Fig. 1, the actuator 142 may be embodied as a hydraulic actuator.
[0017] The engagement assembly 160 operates to selectively couple the impact assembly 120 to the actuator assembly 140. Referring to Figs. 1-3, the engagement assembly 160 comprises a plurality of lift jaw members 162 pivotably mounted to a pivot block 168 on the distal end of the actuator rod 144, and pivotable between a first position in which the lift jaw members 162 engage a lift ring 180 on the guide rod 122 and a second position in which the lift jaw members 162 disengage from a lift ring 180 on the guide rod 122. In the depicted embodiment, the plurality of lift jaw members 162 comprise a key- shaped lower outer surface 164. Similarly, the lift ring 180 comprises a key- shaped inner surface 182, such that the when the lift jaw 162 engages the lift ring, the key-shaped outer surface of the lift jaw members 162 engages with the key- shaped inner surface 182 of the lift ring 180.
[0018] The engagement assembly 160 further comprises a clamp ring 170 to retain the lift jaw members 162 into the first position, and a release ring 190 to disengage the lift jaw members 162 from the clamp ring 170. As best illustrated in Fig. 2, the plurality of lift jaw members 162 further comprise a key- shaped upper outer surface 166 such that the clamp ring 170 engages the key- shaped upper surface 166 with a friction fit, when the actuator rod 144 is fully extended to the engagement position, thereby locking the lift jaw members 166 to the lift ring 180.
[0019] The release ring 190 functions to block motion of the clamp ring
170 as the actuator rod 144 is retracted, such that the jaw members 162 are disengaged from the lift jaw 180. As illustrated in Fig. 3, in one embodiment the position of the release ring 190 is adjustable, such that the retraction stroke length of the impactor assembly is variable. In the embodiment depicted in Fig. 3, the clamp ring 190 is disposed on a mount 194 that is mounted on threads 192 on the housing, such that the position of clamp ring 190 can be adjusted by rotating the mount 194 with respect to the threads. A top plate 196 provides the means to physically adjust the position of release ring 190. In this embodiment the outer circumference of the top plate 196 is knurled to improve the ability to spin the threaded mount 194.
[0020] The particular materials from which the damage impactor 100 are formed are not critical and are primarily a function of design necessity to support the forces generated by the compression spring 126. In one embodiment the various components of the damage impactor 100 are formed from steel or another suitable metal.
[0021] Similarly, the particular size of the impactor 100 and its components is not critical. The dimensions of the impactor are primarily a function of design necessity in order to encompass the apparatus to afford functionality and safety considerations. In one embodiment the damage impactor 100 measures approximately 75 inches in height, and 6 inches in diameter, and supports a stroke length of between 3 inches and 12 inches, such that the impactor can deliver an impact force between 800 foot-pounds and 2000 footpounds via the impact head 124.
[0022] Having described features of the damage impactor, operation of the damage impactor will now be described with reference to Fig. 4, which is a flowchart illustrating operations in a method to use a damage impactor, according to embodiments. Referring to Fig. 4, at operation 405 the damage impactor 100 is positioned proximate the surface to be tested such that the impact head is in contact with the surface before the actuator assembly retracts the actuator rod. The damage impactor 100 may be positioned at any angle with respect to the surface, and at any angle with respect to the Earth. The damage impactor 100 may be secured in place by rigging the support arms 116 to external support members.
[0023] At operation 410 the position of the release ring may be adjusted to adjust the force on the compression spring. As described above, this adjustment may be accomplished by rotating the mount 194 with respect to the threads 192 on the housing. [0024] At operation 415 the actuator assembly 140 is activated. As described above, the actuator 142 may be a hydraulic actuator. Activating the actuator assembly drives the actuator rod 144 in a first direction toward the distal end of the damage impactor 100 to an engagement position where the engagement assembly 160 engages (operation 420) the actuator rod 144 and the guide rod 122. As the engagement assembly reaches the engagement position the plurality of lift jaw members 162 are forced into position to engage the lift ring on the impactor guide rod 122 by engaging the clamping ring 170 with the upper surface 166 of the lift jaws. As the actuator rod 144 continues to extend in the distal direction, the clamping ring 170 is forcefully driven onto the top surfaces of the lift jaw members 166, creating a friction fit locking the clamping ring 170 onto the upper surface of the lift jaw members 166.
[0025] The actuator rod 144 is then retracted (operation 420) in a second direction, opposite the first direction. As the actuator rod 144 retracts the upper surface 166 of the lift jaw members 162 engages the lower surface 182 of the lift ring, such that the lower surface 164 of the lift jaw members 162 is engaged with the surface 182 of the lift ring 180.
[0026] Retracting the actuator rod 144 and the guide rod 122 compresses the spring 126, thereby loading the damage impactor with a spring force. Continued retraction causes the clamp ring 170 to contact the release ring 190. The clamp ring 170 is moveable relative to the actuator rod 144. The release ring 190 limits the motion of the clamp ring 170, thereby allowing the actuator rod 144 and the attached lift jaw members 162 to break free from the clamp ring 170. This, in turn, allows the lift jaw members 162 to pivot on the pivot block 168 such that the lift block 180 is released from the lift jaw members 162, thereby disengaging the actuator rod 144 from the guide rod 122. At this point the energy stored in the compression spring 126 is released, and the compression spring 126 drives the guide rod 122 and the impact head 124 toward the surface of the object being tested. The operations depicted in Fig. 4 may be repeated in order to implement multiple impact tests of the surface.
[0027] Reference in the specification to "one embodiment" or "some embodiments" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least an implementation. The appearances of the phrase "in one embodiment" in various places in the specification may or may not be all referring to the same embodiment.
[0028] Although embodiments have been described in language specific to structural features and/or methodological acts, it is to be understood that claimed subject matter may not be limited to the specific features or acts described. Rather, the specific features and acts are disclosed as sample forms of implementing the claimed subject matter.

Claims

CLAIMS What is claimed is:
1. A damage impactor, comprising:
a housing defining a passage;
an impact assembly, comprising:
a guide rod comprising an impact head;
a bias mechanism to bias the guide rod in a first direction;
an actuator assembly, comprising:
an actuator;
an actuator rod coupled to the actuator; and
an engagement assembly to selectively couple the impact assembly to the actuator assembly,
wherein the actuator assembly:
drives the actuator rod in the first direction to an engagement position at which the engagement assembly couples the actuator rod to the guide rod;
retracts the actuator rod in a second direction, opposite the first direction, to a release position; and
releases the guide rod from the actuator rod.
2. The damage impactor of claim 1, wherein the housing comprises:
one or more guides disposed within in the body.
3. The damage impactor of claim 1, wherein the bias mechanism comprises a compression spring which biases the impact assembly in the first direction.
4. The damage impactor of claim 3, wherein the impact assembly comprises: a first reaction plate and a second reaction plate; and
a stroke limit plate.
5. The damage impactor of claim 1 , wherein the engagement assembly 160 comprises:
a plurality of lift jaw members pivotably mounted to a distal end of the actuator rod, and pivotable between a first position in which the lift jaw members engage a lift ring on the guide rod and a second position in which the lift jaw members disengage from a lift ring on the guide rod;
a clamp ring to retain the lift jaw members into the first position; and a release ring to disengage the lift jaw members from the clamp ring.
6. The damage impactor of claim 5, wherein:
the plurality of lift jaw members comprise a key-shaped lower outer surface; and
the lift ring comprises a key-shaped inner surface, such that the when the lift jaw engages the lift ring, the key-shaped outer surface of the lift jaw members engages with the key-shaped inner surface of the lift ring.
7. The damage impactor of claim 6, wherein:
the plurality of lift jaw members further comprise a key-shaped upper outer surface; and
the clamp ring engages the key-shaped upper surface when the actuator rod is retracted from the engagement position, thereby locking the lift jaw members to the lift ring.
8. The damage impactor of claim 7, wherein the release ring blocks motion of the clamp ring as the actuator rod is retracted, such that the jaw members are disengaged from the lift jaw.
9. The damage impactor of claim 8, wherein the position of the release ring relative to the distal end of the actuator rod is adjustable.
10. The method of claim 9, further comprising a plurality of support arms mounted to the housing.
11. A method to apply an impact damage to a surface, comprising:
positioning a damage impactor of any of claims 1 through 10 proximate the surface;
activating the actuator assembly to:
drive the actuator rod in the first direction to an engagement position where the engagement assembly couples the actuator rod to the guide rod;
retract the actuator rod in a second direction, opposite the first direction, to a release position; and
release the guide rod from the actuator rod.
PCT/US2010/047985 2009-10-16 2010-09-07 Damage impactor Ceased WO2011046687A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/580,363 US8210024B2 (en) 2009-10-16 2009-10-16 Damage impactor
US12/580,363 2009-10-16

Publications (1)

Publication Number Publication Date
WO2011046687A1 true WO2011046687A1 (en) 2011-04-21

Family

ID=43402068

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2010/047985 Ceased WO2011046687A1 (en) 2009-10-16 2010-09-07 Damage impactor

Country Status (2)

Country Link
US (1) US8210024B2 (en)
WO (1) WO2011046687A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014148614A1 (en) 2013-03-22 2014-09-25 富士フイルム株式会社 Organic thin film transistor
CN111189727A (en) * 2020-01-13 2020-05-22 长安大学 Test device and method for testing material damage

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103308267A (en) * 2012-03-16 2013-09-18 鸿富锦精密工业(深圳)有限公司 Impact testing device
KR101665965B1 (en) * 2014-08-08 2016-10-14 코리아테스팅 주식회사 Servo Actuator for Crash Test
CN108120628B (en) * 2018-01-25 2024-07-23 中国商用飞机有限责任公司北京民用飞机技术研究中心 Impact damage prefabrication device
US11067474B2 (en) 2019-07-29 2021-07-20 American Honda Motor Company, Inc. Methods and systems for controlling impact
CN117871290A (en) * 2023-12-26 2024-04-12 中国飞机强度研究所 Impact damage introduction positioning device and test method
CN119269648B (en) * 2024-10-14 2025-03-18 江苏省特种设备安全监督检验研究院 Fiber winding gas cylinder damage detection device based on acoustic emission characteristic of composite material

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB989944A (en) * 1963-03-25 1965-04-22 Bergwerksverband Gmbh Apparatus for testing the hardness of solid bodies
FR1517447A (en) * 1966-04-04 1968-03-15 Dow Chemical Co Method and apparatus for determining impact resistance
FR2323140A1 (en) * 1975-09-03 1977-04-01 Wood Slimp Gmbh METHOD AND APPARATUS FOR MEASURING THE MECHANICAL RESISTANCE OF A WOODEN BODY
JPS6190037A (en) * 1984-10-09 1986-05-08 Takenaka Komuten Co Ltd Method and device for measuring compressive strength of concrete
US5983701A (en) * 1997-06-13 1999-11-16 The Royal Institution For The Advancement Of Learning Non-destructive evaluation of geological material structures
DE10009987A1 (en) * 2000-03-01 2001-09-06 Heinz Kreiskorte Test device for generating shock and impact loads, has mass that strikes test object via striking head, when mass accelerates to test speed via the supply of compressed air in cylinder
WO2008006822A1 (en) * 2006-07-10 2008-01-17 Astrium Sas Device for generating impacts with a structure

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3157070A (en) * 1961-06-26 1964-11-17 Norman C Nourse Impact machine
JPS6090037A (en) 1983-10-21 1985-05-21 Chiyoda Chem Eng & Constr Co Ltd Preparation of carbon monoxide absorbing and separating agent
US4682490A (en) * 1985-01-31 1987-07-28 Adelman Roger A Impact test instrument
US5048320A (en) * 1986-08-28 1991-09-17 Mitsui Engineering & Shipbuilding Co., Ltd. Method and apparatus for impact-type inspection of structures
GB8910443D0 (en) * 1989-05-06 1989-06-21 Howell Mark I Improvements relating to apparatus for and methods of detecting faults and other characteristics of buried foundation piles
US4967587A (en) * 1989-10-20 1990-11-06 Combustion Engineering, Inc. Impact calibration tool
US5823703A (en) * 1996-12-17 1998-10-20 General Motors Corporation Shaft coupling
CA2366030A1 (en) * 2001-12-20 2003-06-20 Global E Bang Inc. Profiling system

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB989944A (en) * 1963-03-25 1965-04-22 Bergwerksverband Gmbh Apparatus for testing the hardness of solid bodies
FR1517447A (en) * 1966-04-04 1968-03-15 Dow Chemical Co Method and apparatus for determining impact resistance
FR2323140A1 (en) * 1975-09-03 1977-04-01 Wood Slimp Gmbh METHOD AND APPARATUS FOR MEASURING THE MECHANICAL RESISTANCE OF A WOODEN BODY
JPS6190037A (en) * 1984-10-09 1986-05-08 Takenaka Komuten Co Ltd Method and device for measuring compressive strength of concrete
US5983701A (en) * 1997-06-13 1999-11-16 The Royal Institution For The Advancement Of Learning Non-destructive evaluation of geological material structures
DE10009987A1 (en) * 2000-03-01 2001-09-06 Heinz Kreiskorte Test device for generating shock and impact loads, has mass that strikes test object via striking head, when mass accelerates to test speed via the supply of compressed air in cylinder
WO2008006822A1 (en) * 2006-07-10 2008-01-17 Astrium Sas Device for generating impacts with a structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014148614A1 (en) 2013-03-22 2014-09-25 富士フイルム株式会社 Organic thin film transistor
CN111189727A (en) * 2020-01-13 2020-05-22 长安大学 Test device and method for testing material damage

Also Published As

Publication number Publication date
US8210024B2 (en) 2012-07-03
US20110088449A1 (en) 2011-04-21

Similar Documents

Publication Publication Date Title
US8210024B2 (en) Damage impactor
JP3706380B2 (en) Elastic rope
CN103389197B (en) Horizontal impact testing stand driving means and bidirectional multifunctional horizontal impact testing stand
CN108415449B (en) A device for deployment, recovery and tension control of tethers in space satellite systems
CN113732773A (en) Spring floating pre-clamping structure
CN118896859A (en) An automatic testing device for modal experiments of thin-walled cylindrical shell structures
CN107764506A (en) A kind of anti-impact device and method for being applied to balance in intermittent wind tunnel
US3786550A (en) Fastener applying tool
CN112388292B (en) A self-positioning nut tightening device and operation method thereof
CN121083354A (en) Device applied to wind power flange automatic drilling and application method
CA2564336C (en) Self-locking braking device for rotary shafts, and relevant applications
CN120133555A (en) A turning device for processing metal shaft parts
CN116279878A (en) climbing work platform
CN106239118A (en) Pulling shaft tightening device
CN118408815A (en) A wide temperature range sample clamping device for Hopkinson pressure bar
CN119077336A (en) Auxiliary assembly mechanism for universal joint drive shaft
CN204936719U (en) The tire uniformity testing system of mechanical lock clamping and positioning device and this device of application
CN219507459U (en) Self-locking lifting device
CN210414580U (en) Feeding and discharging mechanical arm
CN121376212B (en) A linear servo testing device
JP2013049129A5 (en)
CN217976473U (en) Special manual barring gear of wind turbine generator system
CN112649194A (en) Ball screw pair loading test device and test method
CN105479396A (en) Lining drawing machine
CN119642887B (en) NPR anchor cable constant resistance body running speed and displacement measuring device

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 10754828

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 10754828

Country of ref document: EP

Kind code of ref document: A1