AU2021102588A4 - TOUCH DOWN AVIATION AND THRUST POWERED RUNWAY WITH IoT - Google Patents
TOUCH DOWN AVIATION AND THRUST POWERED RUNWAY WITH IoT Download PDFInfo
- Publication number
- AU2021102588A4 AU2021102588A4 AU2021102588A AU2021102588A AU2021102588A4 AU 2021102588 A4 AU2021102588 A4 AU 2021102588A4 AU 2021102588 A AU2021102588 A AU 2021102588A AU 2021102588 A AU2021102588 A AU 2021102588A AU 2021102588 A4 AU2021102588 A4 AU 2021102588A4
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- Prior art keywords
- runway
- aircraft
- landing
- takeoff
- point
- 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.)
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Links
- 238000000034 method Methods 0.000 claims description 11
- 230000000694 effects Effects 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 230000001419 dependent effect Effects 0.000 claims description 2
- 238000004891 communication Methods 0.000 abstract description 6
- 239000013078 crystal Substances 0.000 abstract description 4
- 238000010248 power generation Methods 0.000 abstract description 4
- 239000000463 material Substances 0.000 abstract description 3
- 238000012544 monitoring process Methods 0.000 abstract description 3
- 238000004134 energy conservation Methods 0.000 abstract description 2
- 230000002708 enhancing effect Effects 0.000 abstract 1
- 238000002826 magnetic-activated cell sorting Methods 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 description 5
- ALRKEASEQOCKTJ-UHFFFAOYSA-N 2-[4,7-bis(2-amino-2-oxoethyl)-1,4,7-triazonan-1-yl]acetamide Chemical compound NC(=O)CN1CCN(CC(N)=O)CCN(CC(N)=O)CC1 ALRKEASEQOCKTJ-UHFFFAOYSA-N 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 230000008520 organization Effects 0.000 description 2
- 239000000356 contaminant Substances 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 230000036642 wellbeing Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0004—Transmission of traffic-related information to or from an aircraft
- G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
- E01C9/00—Special pavings; Pavings for special parts of roads or airfields
-
- G—PHYSICS
- G16—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR SPECIFIC APPLICATION FIELDS
- G16Y—INFORMATION AND COMMUNICATION TECHNOLOGY SPECIALLY ADAPTED FOR THE INTERNET OF THINGS [IoT]
- G16Y20/00—Information sensed or collected by the things
- G16Y20/20—Information sensed or collected by the things relating to the thing itself
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/30—Wind power
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
Abstract
The LPWT can be installed on both sides of runway to acquire power during aircraft landing and
takeoff. Generally on runway, aircrafts movement will be around 400 nautical miles per hour.
During the movement very great air velocity will occur on the runway and the same will be
enough to drive small micro wind turbines to produce power. This power generated for the
runway can also be used in the taxi-way and other purposes. The second concept is the
touchdown point- which is the first point for the aircraft to touch the runway during landing. In
the existing system the touchdown point is analyzed manually and communication between the
pilot and monitoring room is very difficult to achieve on the runway which leads to angle
deviation from the point. Improper monitoring of the touchdown point can lead to collision of
aircraft on the runway. Existing communication system Aeronautical Mobile Airport
communication System (Aero MACS) are done with the high rate and safety enhancing
communication system in C- Band without getting accurate touchdown points. The proposed
communication system that have covered all the future needs of Air Traffic Control (ATC) and
Air Traffic Management (ATM) are controlled using the Embedded Micro Controller (EMC) and
automated for achieving the exact point of touch down. The power generation can also be done
with the touchdown point. If the accurate point of the touchdown zone is analyzed then with the
help of vibrations created during the landing and takeoff the power can be generated which is a
unique step for energy conservation system. This type of power generation is done by using the
piezoelectric material which uses a piezoelectric crystal to produce voltage for the runway and
taxi-way. Large amount of pressure is exerted on the runways during takeoff and landings. If the
piezoelectric clusters are placed here then this mechanical energy can be converted to electrical
energy. The efficiency of system can be improved by placing the stacked structures which
contains several layers of piezoelectric clusters and have the capacity to handle very huge
amount of pressure. The maximum takeoff weight for the airbus aircraft (A380) is 560 tones,
which can produce 224 KV, so if one considers the total number of landings in the runway a
large amount of energy could be produced. Nearly 8138 kWh energy could be produced which
can power up to 12207-16276 homes.
Description
TOUCH DOWN AVIATION AND THRUST POWERED RUNWAY WITH IoT
Field and background of this invention
In this invention relate by and large to evaluating runway surface condition during a methodology of an airplane, and all the more especially, encapsulations of the topic identify with a strategy and device to switch between contributions of various revealing arrangements for announced thrust powered runway surface data with IoT.
Summary of this invention
A technique and device for evaluating thrust powered runway with IoT surface conditions including: designing a runway surface handling module to measure: a first kind of revealed runway surface condition data, a second sort of a bunch of Runway Condition Assessment Matrix (RCAM) codes, and a third sort of a bunch of runway surface condition codes including: Snow Warning To Airmen (SNOWTAM) codes; choosing, in any event one of the principal, second or third sort of runway surface data to contribution to the runway surface preparing module, to gauge at any rate a slowing down distance and a slowing down activity of the airplane; accepting, by input, one of at any rate the primary, second or third sort runway surface data by the runway surface preparing module; and planning a runway surface condition, detailed or entered of the main, second or third sort of runway surface data, to a specific runway condition code to figure the a runway distance. In this invention Touch Down Aviation the landing and takeoff departure stages for airplane are likely viewed as the most basic and most noteworthy responsibility of flight stages. When executing, for instance, the last methodology, pilots should oversee different sorts of data to settle on right landing choices and eventually securely land the airplane. For instance, one kind of data, regularly gave electronically through voice interchanges is identified with the air terminal's runway condition for the pilot to conclude if to arrive on the air terminal. Touchdown aviation is essential to reduce accidents during end state of flying called landing. An innovative concept of employing piezo electric crystals arranged in matrix format on the runway touchdown zones (approximately 100meters ) Piezo crystal accepts the impact energy of an aircraft while touching runway and generates voltage accepts frictional energy while movement of an aircraft. Lucid information of landing is important to take decision on speed deceleration of aircraft by employing various brake methodology. The information to be obtained at fastest rate by the Air Traffic Control (ATC) room and must be communicated to the aircraft to control its actuators to reduce speed in accordance with the local wind speed, direction and pressure. Monitoring the movement of an aircraft after touchdown is essential to locate its physical position on the runway before calling another aircraft for landing. There were a total of 415 accidents worldwide during the period of 2010-2014. Of these accidents, 90 were classified as runway/taxiway excursions It should be noted that 409 (99 percent) of all accidents could be assigned an accident category or End State. It is essential to find out touchdown point of an aircraft to avoid accidents and to reduce communication delay during landing (End state of flying).
Presently thrust powered runway with IoT, it is the obligation of the air terminal administrators to survey the runway with IoT surface condition and report the runway condition to pilots in the accompanying methods of: (1) a runway surface condition and contaminant depth (Non RwyCC) where the air terminal administrators will assess the runway condition and report a runway
Surface condition like dry, wet, snow and so on alongside the pollutant profundity in instances of debased runways by means of the ATIS broadcast or with the NOTAM Runway surface condition; (2) a runway condition assessment matrix (RCAM) where the air terminal administrators are needed to evaluate the runway condition and report through the usage of the runway condition assessment matrix codes (RwyCC); and (3) a SNOWTAM (Non-RwyCC) which is an extraordinary arrangement NOTAM informing the presence, or evacuation, of risky conditions because of snow, ice, slush or standing water related with snow, slush and ice on the development territory, by utilizing a particular organization to reference each dangerous kind of condition. There are two types of landing techniques which is followed in the day today landing, they are, Cross- Wind Landing Technique and Wing-Low Technique. Highly Integrated Digital Electronic Control (HIDEC) is the integration of aircraft engine operations with air data and flight control systems to improve aircraft performance.
Description of this invention
An IoT strategy for surveying runway conditions to figure runway distances of an airplane while working with a landing or takeoff of the airplane at an air terminal wherein the runway is
dependent upon various runway surface conditions is given. The technique incorporates: designing a runway surface preparing module to measure in any event a first, second and third kind of runway surface data of a majority of sorts of runway surface data communicated via air
traffic control (ATC) wherein a transmission of information transmissions of the ATC include: a first sort of detailed runway surface condition data, a second sort of a bunch of Runway Condition Assessment Matrix (RCAM) codes, and a third sort of a bunch of runway surface condition codes including: Snow Warning To Airmen (SNOWTAM) codes; choosing, at any rate one of the primary, second or third sort of runway surface data to contribution to the runway surface handling module, to gauge at any rate a slowing down distance and a slowing down activity of the airplane; accepting, by input, one of at any rate the principal, second or third sort runway surface data by the runway surface handling module; and planning a runway surface
condition, announced or entered of the main, second or third sort of runway surface data, to a specific runway condition code to process the a runway distance. Research efforts led to the development of several control modes that demonstrated extended engine life, increased engine thrust, and lower fuel consumption .The major elements of HIDEC were a Digital Electronic Flight Control System (DEFCS), the engine-mounted DEECs, an on-board general purpose computer, and an integrated architecture allowing all components to "talk to each other." In this invention the strategy, further incorporates: entering the contribution by either manual activities of the pilot utilizing a realistic coupled to the runway surface handling module because of runway surface data imparted by voice transmissions to the pilot, or by contribution from IoT robotized reactions from a ground worker to information demands from the runway surface preparing module when landing or departure wherein the ground worker is electronically associated with the runway surface preparing module. Thrust powered Runway with IoT related accident (for example runway journeys) stay a safety risk for aircrafts. The contributing components incorporate poor braking down activity because of polluted runways or runways, joined with deficits in the exactness and idealness of detailing runway surface conditions. In 2017, The International Civil Aviation Organization (ICAO) set forth a worldwide runway wellbeing activity plan that required the inescapable sending of the ICAO design for surveying and announcing runway surface conditions as powerful moderation to runway attacks. The
Global Reporting Format (GRF) for announcing runway surface conditions, started in information from the Federal Aviation Authority (FAA) information of Take-off and Landing Performance Assessment (TALPA) and is considered material for far and wide use by 2020. The GRF gives a normalized detailing arrangement of runway surface conditions on wet and defiled runways which can then straightforwardly be associated with an airplane's exhibition for anticipating take-off and landing runway exhibitions (for example distances) of airplane. The air traffic control (ATC) might be an airport regulation station or some other ground-based area from which work force speaks with the airplane, including the ground-based staff and gear worried about checking and controlling air traffic inside a specific region. The ATC capacities to speak with the airplane to work with cost occasions, including accepting leeway demands from the airplane for client chose flight plan change alternatives, and imparting endorsement or disavowal to the airplane for a got freedom demand. The ATC is likewise illustrative of a flight activity control ground station, and may give different correspondences to the airplane, including however not restricted to: memorable flight course execution information, cost boundary information, terminal territory broadcast information, airport regulation transmission
information, current and chronicled climate information, current and notable NOTAM information, SNOWTAM information, runway surface condition data and the like. The power generation can also be done with the touchdown point. If the accurate point of the touchdown zone is analyzed then with the help of vibrations created during the landing and takeoff the power can be generated which is a unique step for energy conservation system. This type of power generation is done by using the piezoelectric material which uses a piezoelectric crystal to produce voltage for the runway and taxi-way. Large amount of pressure is exerted on the runways during takeoff and landings. If the piezoelectric clusters are placed here then this mechanical energy can be converted to electrical energy.
Claims (5)
1. In this invention, further containing: entering the contribution by either manual activities of the pilot utilizing a realistic IoT coupled to the runway surface handling module because of runway surface data communicated by voice transmissions to the pilot, or by contribution from robotized reactions from a ground worker to information demands from the runway surface preparing module when landing or departure wherein the ground worker is electronically associated with the runway surface preparing module.
2. The runway distance by the runway surface processing module for the landing or takeoff based dependent on extra runway surface data recovered from a ground worker including: wet, dry and polluted runway distance information from tables put away by the ground worker for revising the runway distance computations.
3. The runway distance by the runway surface processing module for the landing or takeoff using aircraft performance data from a performance database of the aircraft comprising: a calculated landing or takeoff weight of the aircraft.
4. Due to the automatic roll assist feature of the flight control system, as the aircraft neared the threshold, this cross-controlling not only deflected the ailerons, it also deployed the multi function spoilers on the right wing. A review of the flight data recorder information determined that the use of the wing-low technique caused spoiler deployment in the final segment of the approach.
5. The maximum takeoff weight for the airbus aircraft (A380) is 560 tones, which can produce 224 KV, so if one considers the total number of landings in the runway a large amount of energy could be produced. Nearly 8138 kWh energy could be produced which can power up to 12207 16276 homes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2021102588A AU2021102588A4 (en) | 2021-05-15 | 2021-05-15 | TOUCH DOWN AVIATION AND THRUST POWERED RUNWAY WITH IoT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2021102588A AU2021102588A4 (en) | 2021-05-15 | 2021-05-15 | TOUCH DOWN AVIATION AND THRUST POWERED RUNWAY WITH IoT |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2021102588A4 true AU2021102588A4 (en) | 2021-07-08 |
Family
ID=76662647
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2021102588A Ceased AU2021102588A4 (en) | 2021-05-15 | 2021-05-15 | TOUCH DOWN AVIATION AND THRUST POWERED RUNWAY WITH IoT |
Country Status (1)
Country | Link |
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AU (1) | AU2021102588A4 (en) |
-
2021
- 2021-05-15 AU AU2021102588A patent/AU2021102588A4/en not_active Ceased
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Date | Code | Title | Description |
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FGI | Letters patent sealed or granted (innovation patent) | ||
MK22 | Patent ceased section 143a(d), or expired - non payment of renewal fee or expiry |