GB557434A - Testing apparatus for ascertaining the balance of the blades of air screws - Google Patents

Testing apparatus for ascertaining the balance of the blades of air screws

Info

Publication number
GB557434A
GB557434A GB953142A GB953142A GB557434A GB 557434 A GB557434 A GB 557434A GB 953142 A GB953142 A GB 953142A GB 953142 A GB953142 A GB 953142A GB 557434 A GB557434 A GB 557434A
Authority
GB
United Kingdom
Prior art keywords
blade
spindle
balance
block
carrier
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.)
Expired
Application number
GB953142A
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.)
Avery Weigh Tronix Ltd
Original Assignee
W&T Avery Ltd
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 W&T Avery Ltd filed Critical W&T Avery Ltd
Priority to GB953142A priority Critical patent/GB557434A/en
Publication of GB557434A publication Critical patent/GB557434A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00Testing static or dynamic balance of machines or structures
    • G01M1/12Static balancing; Determining position of centre of gravity

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Balance (AREA)

Abstract

557,434. Testing balance. AVERY, Ltd., W. & T., and BOWEN, E. July 9, 1942, No. 9531. [Class 106 (ii)] [Also in Group XX] An apparatus for testing the balance, the centre of gravity or predetermined turning moment of an air screw comprises a rotatable blade carrier adjustable to admit of a test in both a horizontal and vertical disposition and means for interconnecting the carrier with a weighing apparatus. A carrier block d has seceured to one face a counterbalancing arm e with adjustable weight e<SP>1</SP> and to the opposite face a part for receiving a hub d<SP>1</SP> which in turn receives the butt of an air screw blade f. The carrier block d may turn about a spindle g in one with coaxial knife edges e<SP>2</SP> in bearings c. The block may be clamped to the spindle by friction between a fibre shoe h and the spindle, the friction being regulated by a screw and spring j, j<SP>1</SP>. The spindle g is extended at right angles at one end to form a lever k which is connected by a link l to the lever system m of a weighing apparatus n reading plus or minus each side of "zero". The blade f and arm e may be arranged either horizontally as shown or vertically, a locking pin o engaging a hole o<SP>1</SP> (not shown) or o<SP>2</SP> to lock the device in one or other position while adjustments are made. A pointer d<SP>2</SP> reading against a mark a<SP>1</SP> indicates when balance is attained. The end of the lever k may be gripped and held by a spring grip p<SP>3</SP>, q operated from a handle p through spindle p<SP>1</SP> and toothed gear and cam. In use, a standard blade is secured to the block and the weight e<SP>1</SP> moved to effect balance, the pointer n<SP>1</SP> being adjusted to zero. The blade to be tested is substituted for the standard and the grip p<SP>3</SP> released so that the pointer n<SP>1</SP> may indicate the differences. The block and blade are then turned through 90 degrees and the experiment repeated with the blade in a vertical position. For the initial calibration, an arm from which are supported base weights may be used secured in the position of the blade.
GB953142A 1942-07-09 1942-07-09 Testing apparatus for ascertaining the balance of the blades of air screws Expired GB557434A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB953142A GB557434A (en) 1942-07-09 1942-07-09 Testing apparatus for ascertaining the balance of the blades of air screws

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB953142A GB557434A (en) 1942-07-09 1942-07-09 Testing apparatus for ascertaining the balance of the blades of air screws

Publications (1)

Publication Number Publication Date
GB557434A true GB557434A (en) 1943-11-19

Family

ID=9873795

Family Applications (1)

Application Number Title Priority Date Filing Date
GB953142A Expired GB557434A (en) 1942-07-09 1942-07-09 Testing apparatus for ascertaining the balance of the blades of air screws

Country Status (1)

Country Link
GB (1) GB557434A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5187976A (en) * 1991-08-16 1993-02-23 The Babcock & Wilcox Company Mass-moment weighing beam
US5195363A (en) * 1991-08-16 1993-03-23 The Babcock & Wilcox Company Automated mass-moment weighing system for jet engine blades
EP2233904A1 (en) * 2009-03-25 2010-09-29 Siemens Aktiengesellschaft Arrangement to determine a static moment of a blade
EP2657670A1 (en) * 2012-04-24 2013-10-30 Siemens Aktiengesellschaft Reference standard for calibrating a moment weight scale
CN105644801A (en) * 2014-11-14 2016-06-08 江西昌河航空工业有限公司 Adjustment method for helicopter rotor single blade interchange

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5187976A (en) * 1991-08-16 1993-02-23 The Babcock & Wilcox Company Mass-moment weighing beam
US5195363A (en) * 1991-08-16 1993-03-23 The Babcock & Wilcox Company Automated mass-moment weighing system for jet engine blades
EP2233904A1 (en) * 2009-03-25 2010-09-29 Siemens Aktiengesellschaft Arrangement to determine a static moment of a blade
EP2657670A1 (en) * 2012-04-24 2013-10-30 Siemens Aktiengesellschaft Reference standard for calibrating a moment weight scale
CN105644801A (en) * 2014-11-14 2016-06-08 江西昌河航空工业有限公司 Adjustment method for helicopter rotor single blade interchange
CN105644801B (en) * 2014-11-14 2017-08-25 江西昌河航空工业有限公司 A kind of method of adjustment of lifting airscrew interchange

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