Analysis of conditions favourable for seaplane transport system development in Europe. Review of FUSETRA aircrafts characteristics

Transcription

1 Future Seaplane Traffic Analysis of conditions favourable for seaplane transport system development in Europe. Review of aircrafts characteristics

2 Europe Area 10,180,000 km² Meridional extent km Parallel extent km Highest point 5,642 metres Lowest point - 28 metres Population 712,000,000 Population density 70/km² Countries 50 range of operation European Union Area 4,324,782 km² Population 497,198,740 Population density 114 Member states , Slide 1

3 All European airports location 2570 airports and landing fields 43 main passenger airports (large and medium Hubs) 450 Primary airports (commercial service airports) 1336 with paved runways 1270 airports 1300 landing fields 737 IFR airports One airport per 2850 km inhabitants per one airport , Slide 2

4 POOR < > GOOD Accessibility Multimodal potential accessibility measures transport infrastructure quality of modes (car,rail,air) , Slide 3

5 All European seaports location 1400 seaports , Slide 4

6 Seaplane operations Scenarios 1. Land seaport 2. Seaport seaport 3. Seaport land , Slide 5

7 A total overview of all European seaports Cumulative distribution function Distribution of distances from seaport to the nearest airport , Slide 6

8 A total overview of all European seaports Cumulative distribution function Distribution of distances between nearest seaports in Europe , Slide 7

9 A total overview of all European seaports Cumulative distribution function Distribution of distances from seaport to the nearest city (seaports accessibility) , Slide 8

10 A total overview of all European seaports Cumulative distribution function Number of cities within particular radius of seaports in Europe (seaports accessibility) , Slide 9

11 A total overview of all European seaports Total number of population Population within particular radius of seaport in Europe (seaports accessibility) , Slide 10

12 A total overview of all European seaports Average catchment area of seaports in Europe (seaports accessibility) , Slide 11

13 Europe is a special area with good features favoring the development of regional passenger air transportation system with using seaplanes: it has about 1,400 seaports, in the most densely populated regions, the nearest seaport lies within a distance of less than 40 km for more than 95 % of population (within less than 20 km for 80 % of population), for most European cities, the nearest seaport is located within 20 km (80 % of cities), there are many cities in the vicinity of the main European seaports (not fewer than 10 cities with population grater than within 50 km radius of each seaport) passengers can freely choose the most suitable seaport, a lot of European population (potential passengers) live close to seaport approximately inhabitants within 40 km radius of seaport, 20% of European (26% of EU) citizens lives in catchment areas of seaports Number of tourist viziting regions lies in catchment areas of seaports is not less than 130 mln , Slide 12

14 Review of aircrafts characteristics , Slide 13

15 Twin engine floatplane Single engine floatplane Twin (or single) engine amphibian? Twin engine amphibious floatplane Single engine amphibious floatplane Airplane(s) , Slide 14

16 Assumption: modification of existing land-based aircraft floatplane Base version amphibious floatplane , Slide 15

17 Assumption: modification of existing land-based aircraft floatplane amphibious floatplane Base version amphibian flying boat , Slide 16

18 MORRISON 6 Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 17

19 MORRISON 6 Payload-range diagram (calculated) , Slide 18

20 Cessna 172R Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 19

21 Cessna 172R Payload-range diagram (calculated) , Slide 20

22 Cessna 182T Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 21

23 Cessna 182T Payload-range diagram (calculated) , Slide 22

24 Cessna 206H Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 23

25 Cessna 206H Payload-range diagram (calculated) , Slide 24

26 Cessna 208 CARAVAN Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 25

27 Cessna 208 CARAVAN Payload-range diagram (calculated) , Slide 26

28 GA-8 Airvan Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 27

29 GA-8 Airvan Payload-range diagram (calculated) , Slide 28

30 EXPLORER 500T Category SPECIFICATIONS (calculated) Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 29

31 EXPLORER 500T Payload-range diagram (calculated) , Slide 30

32 T-101 GRACH SPECIFICATIONS (calculated) Category Base Amphibious floatplane Engine, [kw] Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 31

33 T-101 GRACH Payload-range diagram (calculated) , Slide 32

34 VulcanAir P68C Category SPECIFICATIONS (calculated) Base Amphibious floatplane Amphibian Engine, [kw] 2x157 2x157 2x157 Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 33

35 VulcanAir P68C Payload-range diagram (calculated) , Slide 34

36 Britten-Norman BN-2B Category SPECIFICATIONS (calculated) Base Amphibious floatplane Amphibian Engine, [kw] 2x224 2x224 2x224 Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 35

37 Britten-Norman BN-2B Payload-range diagram (calculated) , Slide 36

38 Britten-Norman BN-2T Category SPECIFICATIONS (calculated) Base Amphibious floatplane Amphibian Engine, [kw] 2x298 2x298 2x298 Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 37

39 Britten-Norman BN-2T Payload-range diagram (calculated) , Slide 38

40 HAI Y-12 Category SPECIFICATIONS (calculated) Base Amphibious floatplane Amphibian Engine, [kw] 2x462 2x462 2x462 Wing span, [m] Length overall, [m] Weight empty, [kg] Max. fuel weight, [kg] Max. payload, [kg] Max. T-O weight, [kg] Max. operating speed, [km/h] Service ceiling, [m] T-O to 15 m (on land), [m] T-O to 15 m (on water), [m] T-O run (on land), [m] T-O run (on water), [m] Range with max fuel, 45 min reserves, [km] , Slide 39

41 HAI Y-12 Payload-range diagram (calculated) , Slide 40

42 Max. T-O weight [kg] Single engine aircrafts Base Amphibious floatplane 0 Max. T-O weight of the base and amphibious floatplane versions , Slide 41

43 Relative empty weight Single engine aircrafts 0,8 0,7 0,6 0,5 0,4 0,3 0,2 0,1 0 Base Amphibious floatplane Relative empty weight of the base and amphibious floatplane versions Empty weight/max.t-o weight , Slide 42

44 Relative payload weight Single engine aircrafts 0,35 0,3 0,25 0,2 0,15 0,1 0,05 Base Amphibious floatplane 0 Relative payload weight of the base and amphibious floatplane versions payload weight / max.t-o weight , Slide 43

45 Relative T-O power, [kw/kg] Single engine aircrafts 0,2 0,18 0,16 0,14 0,12 0,1 0,08 0,06 0,04 0,02 0 Base Amphibious floatplane Relative T-O power of the base and amphibious floatplane versions T-O power / max.t-o weight , Slide 44

46 Relative T-O distance, base/amphibious floatplane Single engine aircrafts 0,72 0,7 0,68 0,66 0,64 0,62 0,6 0,58 Relative T-O distance of the base and amphibious floatplane versions T-O distance on land / T-O distance on water , Slide 45

47 Relative range, base/amphibious floatplane Single engine aircrafts 1,4 1,2 1 0,8 0,6 0,4 0,2 0 Relative range of the base and amphibious floatplane versions range of the base aircraft / range of the amphibious floatplane version , Slide 46

48 Max. T-O weight [kg] Twin engine aircrafts Base amphibious floatplane Amphibian VulcanAir P68C BN-2B BN-2T HAI Y-12 Max. T-O weight of the base, amphibious floatplane and amphibian versions , Slide 47

49 Relative empty weight Twin engine aircrafts 0,8 0,7 0,6 0,5 0,4 0,3 Base Amphibious floatplane Amphibian 0,2 0,1 0 VulcanAir P68C BN-2B BN-2T HAI Y-12 Relative empty weight of the base, amphibious floatplane and amphibian versions Empty weight/max.t-o weight , Slide 48

50 Relative payload weight Twin engine aircrafts 0,4 0,35 0,3 0,25 0,2 0,15 Base Amphibious floatplane Amphibian 0,1 0,05 0 VulcanAir P68C BN-2B BN-2T HAI Y-12 Relative payload weight of the base, amphibious floatplane and amphibian versions payload weight / max. T-O weight , Slide 49

51 Relative T-O power, [kw/kg] Twin engine aircrafts 0,25 0,2 0,15 0,1 Base Amphibious floatplane Amphibian 0,05 0 VulcanAir P68C BN-2B BN-2T HAI Y-12 Relative T-O power of the base, amphibious floatplane and amphibian versions T-O power / max. T-O weight , Slide 50

52 Relative T-O distance, amphibious floatplane and amphibian / base Twin engine aircrafts 1,6 1,4 1,2 1 0,8 0,6 Amphibious floatplane Amphibian 0,4 0,2 0 VulcanAir P68C BN-2B BN-2T HAI Y-12 Relative T-O distance of the base, amphibious floatplane and amphibian versions T-O distance on water / T-O distance on land , Slide 51

53 Relative range, base/amphibious floatplane or amphibian Twin engine aircrafts 1,2 1,15 1,1 1,05 Amphibious floatplane Amphibian 1 0,95 VulcanAir P68C BN-2B BN-2T HAI Y-12 Relative range of the base, amphibious floatplane and amphibian versions range of the base aircraft / range of the amphibious floatplane or amphibian version , Slide 52

54 Evaluation criteria Relative transport efficiency , Slide 53

55 Relative transport efficiency , Slide 54

56 DOC (Direct Operating Cost) , Slide 55

57 Ticket cost (estimated) , Slide 56

58 Contact: Department of Aircrafts and Aircraft Engines Faculty of Mechanical Engineering and Aeronautics Rzeszow University of Technology Address: ul. Powstancow Warszawy Rzeszow, POLAND phone: mobile: web: andemajk@prz.edu.pl , Slide 57

59 Thank You for your attention , Slide 58