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GB2071589A - Aircraft Wheel - Google Patents

Aircraft Wheel Download PDF

Info

Publication number
GB2071589A
GB2071589A GB7934962A GB7934962A GB2071589A GB 2071589 A GB2071589 A GB 2071589A GB 7934962 A GB7934962 A GB 7934962A GB 7934962 A GB7934962 A GB 7934962A GB 2071589 A GB2071589 A GB 2071589A
Authority
GB
United Kingdom
Prior art keywords
wheel
receptors
aircraft
rotate
landing
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.)
Withdrawn
Application number
GB7934962A
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
Priority to GB7934962A priority Critical patent/GB2071589A/en
Publication of GB2071589A publication Critical patent/GB2071589A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface  the elements being rotated before touch-down

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

Figures A and B show a wheel having receptors jutting out to receive the power of the windflow that previously used to slip by and was not tapped. Now the receptors use the air flow and convert it to use by making the wheel to rotate in the required direction prior to landing on any runway. <IMAGE>

Description

SPECIFICATION The Dynamic Wheel The idea of the above wheel is to give the aircraft a safe landing without a burst tyre or undue wear and tear. The invention of wind receptors will automatically turn the wheel to reduce the impact on touch down. Some times the wheel could turn the opposite way which could cause a screach or a burst tyre. With the new invention the proceeding receptors dictate the direction the wheel should rotate to enhance a smooth landing without undue friction. The invention is called the "DYNAMIC WHEEL".
Claims
1. An aircraft wheel having means to cause itself to rotate in the correct direction required for landing.
2. An aircraft wheel as in (1) wherein 'air' receptors cuplike in shape are provided to rotate the wheel under the influence of the incident of air flow in flight.
3. An aircraft wheel substantially as herein before described with reference to the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (3)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION The Dynamic Wheel The idea of the above wheel is to give the aircraft a safe landing without a burst tyre or undue wear and tear. The invention of wind receptors will automatically turn the wheel to reduce the impact on touch down. Some times the wheel could turn the opposite way which could cause a screach or a burst tyre. With the new invention the proceeding receptors dictate the direction the wheel should rotate to enhance a smooth landing without undue friction. The invention is called the "DYNAMIC WHEEL". Claims
1. An aircraft wheel having means to cause itself to rotate in the correct direction required for landing.
2. An aircraft wheel as in (1) wherein 'air' receptors cuplike in shape are provided to rotate the wheel under the influence of the incident of air flow in flight.
3. An aircraft wheel substantially as herein before described with reference to the accompanying drawings.
GB7934962A 1979-10-09 1979-10-09 Aircraft Wheel Withdrawn GB2071589A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7934962A GB2071589A (en) 1979-10-09 1979-10-09 Aircraft Wheel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7934962A GB2071589A (en) 1979-10-09 1979-10-09 Aircraft Wheel

Publications (1)

Publication Number Publication Date
GB2071589A true GB2071589A (en) 1981-09-23

Family

ID=10508380

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7934962A Withdrawn GB2071589A (en) 1979-10-09 1979-10-09 Aircraft Wheel

Country Status (1)

Country Link
GB (1) GB2071589A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2242401A (en) * 1990-03-29 1991-10-02 Clive Murray Coker Aircraft wheel and means to reduce tyre wear on landing
US5213285A (en) * 1992-04-10 1993-05-25 Stanko John J Rotating aircraft tire/landing gear apparatus
USD1012615S1 (en) * 2022-01-07 2024-01-30 Li Yang All in one toddler cup with snack container, straw and handle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2242401A (en) * 1990-03-29 1991-10-02 Clive Murray Coker Aircraft wheel and means to reduce tyre wear on landing
US5213285A (en) * 1992-04-10 1993-05-25 Stanko John J Rotating aircraft tire/landing gear apparatus
USD1012615S1 (en) * 2022-01-07 2024-01-30 Li Yang All in one toddler cup with snack container, straw and handle

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)