GB809948A - Improvements in or relating to whirling arm apparatus - Google Patents

Improvements in or relating to whirling arm apparatus

Info

Publication number
GB809948A
GB809948A GB1852956A GB1852956A GB809948A GB 809948 A GB809948 A GB 809948A GB 1852956 A GB1852956 A GB 1852956A GB 1852956 A GB1852956 A GB 1852956A GB 809948 A GB809948 A GB 809948A
Authority
GB
United Kingdom
Prior art keywords
model
annular
fan
electric motor
housing
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
GB1852956A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB809948A publication Critical patent/GB809948A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Toys (AREA)

Abstract

809,948. Whirling arm apparatus. COOKE, W. D. Nov. 30, 1956 [June 15, 1956], No. 18529/56. Divided out of 809,947. Class 4. Whirling arm apparatus comprises a member mounted to rotate an aerodynamic model about an axis, and a centrifugal fan mounted to rotate about the axis in the sense opposite to that of the model so as to set up an air flow with spiral streamlines through which the model moves. Fig. 1 shows a section of a housing 1 containing an electric motor 5 driving a hollow shaft 3 to which is fixed the fan 9 having blades 11. An annular air intake 14 surrounds the fan so as to form therewith an annular gap in which the model 19 moves. Air from the fan is sucked into intake 14 and along an annular duct 15 to a flared outlet 16 by ejector devices 17 fed by pipes 26 from a distributor 32 and pump 30 driven by an electric motor 7. The model 19 is supported by a radial arm (not shown) on a hollow shaft 4 driven by an electric motor 6. Shaft 4 also supports a pitot head on an arm 20. Electrical power supply cables and leads from test instruments e.g. strain gauges on the model, pass along a central tube 2. Shock waves rising from the model between lines A and B pass out of the housing through an annular aperture 24, the pipes 26 being of suitable cross-section. Shock waves moving down from the model between lines C and D are reflected by annular surfaces 27, 28 to pass out of the housing through an annular aperture 23, struts 25 of suitable cross-section being provided.
GB1852956A 1956-03-27 1956-06-15 Improvements in or relating to whirling arm apparatus Expired GB809948A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB951956A GB809947A (en) 1956-03-27 1956-03-27 Improvements in or relating to helicopters

Publications (1)

Publication Number Publication Date
GB809948A true GB809948A (en) 1959-03-04

Family

ID=9873540

Family Applications (2)

Application Number Title Priority Date Filing Date
GB951956A Expired GB809947A (en) 1956-03-27 1956-03-27 Improvements in or relating to helicopters
GB1852956A Expired GB809948A (en) 1956-03-27 1956-06-15 Improvements in or relating to whirling arm apparatus

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB951956A Expired GB809947A (en) 1956-03-27 1956-03-27 Improvements in or relating to helicopters

Country Status (1)

Country Link
GB (2) GB809947A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118010292A (en) * 2024-04-09 2024-05-10 中国空气动力研究与发展中心高速空气动力研究所 Sub-transonic progressive direct connection wind tunnel test model supporting device and design method

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3568955A (en) * 1968-12-24 1971-03-09 James E Mcdevitt Blowhard vtol aircraft
GB2123780A (en) * 1982-05-05 1984-02-08 Francis Williamson Improvements to aircraft
CN115683541B (en) * 2023-01-05 2023-03-14 中国空气动力研究与发展中心高速空气动力研究所 Multi-channel pulse micro-jet generator for flow control of large S-bend air inlet channel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118010292A (en) * 2024-04-09 2024-05-10 中国空气动力研究与发展中心高速空气动力研究所 Sub-transonic progressive direct connection wind tunnel test model supporting device and design method

Also Published As

Publication number Publication date
GB809947A (en) 1959-03-04

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