AU5072699A - Hydroplane - Google Patents

Hydroplane Download PDF

Info

Publication number
AU5072699A
AU5072699A AU50726/99A AU5072699A AU5072699A AU 5072699 A AU5072699 A AU 5072699A AU 50726/99 A AU50726/99 A AU 50726/99A AU 5072699 A AU5072699 A AU 5072699A AU 5072699 A AU5072699 A AU 5072699A
Authority
AU
Australia
Prior art keywords
hydroplane
interceptors
aft
hull
deadrise
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.)
Granted
Application number
AU50726/99A
Other versions
AU753993B2 (en
Inventor
Jury Mikhailovich Bannikov
Anatoly Sergeevich Klyagin
Viktor Azarievich Lukashevsky
Konstantin Khristoforovich Marbashev
Alexei Leonidovich Maximov
Sergei Anatolievich Porodnikov
Andrei Anatolievich Sorokin
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.)
Zakrytoe Aktsionernoe Obschestvo "otdelenie Morskikh Sistem Okb Im Po Sukhogo"
Original Assignee
Zakrytoe Aktsionernoe Obschestvo "otdelenie Morskikh Sistem Okb Im Po Sukhogo"
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
Priority claimed from RU98114297/28A external-priority patent/RU2131822C1/en
Priority claimed from RU98113193/28A external-priority patent/RU2131373C1/en
Application filed by Zakrytoe Aktsionernoe Obschestvo "otdelenie Morskikh Sistem Okb Im Po Sukhogo" filed Critical Zakrytoe Aktsionernoe Obschestvo "otdelenie Morskikh Sistem Okb Im Po Sukhogo"
Publication of AU5072699A publication Critical patent/AU5072699A/en
Application granted granted Critical
Publication of AU753993B2 publication Critical patent/AU753993B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water
    • B63H11/10Marine propulsion by water jets the propulsive medium being ambient water having means for deflecting jet or influencing cross-section thereof
    • B63H11/103Marine propulsion by water jets the propulsive medium being ambient water having means for deflecting jet or influencing cross-section thereof having means to increase efficiency of propulsive fluid, e.g. discharge pipe provided with means to improve the fluid flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/18Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydroplane type
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/18Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydroplane type
    • B63B1/22Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydroplane type with adjustable planing surfaces

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Feedback Control In General (AREA)
  • Earth Drilling (AREA)

Description

1 HYDROPLANE Field of Invention This invention relates to the shipbuilding field and, in particular to the construction of hydroplane or planing craft provided with extendable interceptors. Prior Art There are hydroplanes or planing crafts that are known to have a hull with a deadrise bottom and controllable aft and forward interceptors (spoilers) mounted in recesses arranged in the bottom. The high speed craft described in patent RU 2096240 of 1997, has a hull with a deadrise bottom provided with a forward and aft transverse planing steps and extendable interceptors that are mounted behind these steps and divided symmetrically into portside and starboard-side sections. An automatic interceptor control system permits the interceptors to be used as pitch and roll control elements. However, the optimization of speed and seakeeping performance of the known craft, improvement of its operational efficiency and enhancement of comfort level for passengers and crew can only be achieved due to the operation of the control system. Generally, these hydroplanes use a propeller as a propulsive device, which is connected to the main engine located in the central or aft section of the hull by means of shaftlines supported by shaft brackets (Inventor's Certificate SU 1025574). The disadvantages of the known hydroplane are an increased drag due to projecting parts of the shaftline and rudders as well as considerable space inside the hydroplane taken up by the main engines, shaftlines and auxiliary equipment. There is a planing craft that is known to have a water-jet propulsive device that provides better efficiency at higher speeds compared to the craft fitted with propellers (SU 200452). However, this craft does not use interceptors that would considerably improve its speed and seakeeping performance. Summary of Invention The present invention permits to combine the advantages of interceptors with those of waterjets on hydroplane, the resultant effect of using each of these components being 2 suplemented by an aitinal effect obtinable at a certain arrangement of interceptors relative to the water-jet intake openings in the hydroplane's bottom. According to the invention, a hydroplane has a hull with a deadrise bottom and an extendable interceptors and is provided with one or more water-jets at the aft part of the hydroplane, the water intake openings of water-jets being arranged in the hull's bottom fonvard of the interceptors. A hydroplane may also be provided with bow (forward) interceptors. The bottom may have an aft and a forward transverse planing steps with interceptors, in this particular case, mounted behind the steps. The deadrise angle of the bottom may vary along the hydroplane's length, the optimum angle range being 60 to 12 at the forward step and 00 to 60 at the aft step. Brief Description of the Drawings The invention will n ow be described in more detail with reference to an exemplifying embodiment thereof and also with reference to the accompanying drawing in which Figure 1 is a schematic side view of an inventive hydroplane Figure 2 is a schematic bottom view of an inventive hydroplane Figure 3 is a schematic stern view of an inventive hydroplane Proportions between individual components and structural e shown in the drawings are modified for better representation. The detailed description of the invention The hydroplane illustrated in Figure 1 has a hull 1 with a deadrise bottom 2 and an interceptors 3 and 4 (for portside and starboard-side respectively) that are capable of moving out of a slot in the bottom (not shown) or from behind the aft tranvierse Nlaning step 5 The hydroplane is provided with one (or more) water-jet 6 mounted at the aft end of the hydroplane, the intake opening 7 of the water-jet 6 being arranged in the bottom 2 of the hull 1 forward of the interceptors 3 and 4 as shown in Figre 2. The hydroplane may also be fitted with forward interceptors 8 and 9 that are located behind the forward transverse step 10, port and starboard. The forward, or bow step 10 is arranged on the hull's bottom fonvard of its center of gravity 1. If necessary tintrptr and 9 can be divided into sections (not shown in the drawings) that are then controlled 3 individually to compensate for pitch and roll motions in a seaway. The aft interceptors 3 and 4 and the forward interceptors 8 and 9 if fitted (see Figures 2 and 3) are constructed with a sharp outer edge, which secures a continuous flow separation at the edge. The deadrise angle of the bottom varies along the hydroplane's length from 60 to 120 at the forward step 8 to 0' to 6' at the aft step 4. Optimum deadrise angles for each planing step of a specific hydroplane are determined from model tank tests. The increase of deadrise angles over the above-stated maximum values will result in a lower drag-lift ratio for the hydroplane while their decrease beyond the above-stated ranges will somewhat improve it but will also cause problems for stable planing and increase vertical accelerations experienced during the ride in a seaway. The bottom surface of the hydroplane forward of each planing step has symmetrical flat areas that coincide with the areas of the bottom surface wetted during the planing mode of operation, as determined from the model tests. The flat areas 12 forward of the forward planing step are of triangular or trapezoidal shape. The flat areas 13 forward of the aft planing step may also have a trapezoidal shape but more often their outline is of more complicated form. To provide a minimum drag of the hydroplane, the travels of the forward and aft interceptors or their sections are determined depending of the speed of the hydroplane. The optimum relationship is determined from the model tests with subsequent refining based on the results of full-scale trials. Travel of the individual interceptors or their sections is controlled by an automatic control system that provides for an increased motion stability and better maneuverability of the hydroplane in the calm sea conditions and for roll and pitch motions damping and reduction of vertical accelerations when riding in a seaway. During reverse running or stem-to mooring operations the interceptors are retracted to a position within the planing steps (or into the bottom slots) to protect them from damage. When the hydroplane is riding with the interceptors 3 and 4 projected some distance beyond the aft planing step 5 (or the respective slot), an area of increased pressure is generated immediately ahead of the interceptors. It is within this area of increased pressure that the water-jet intake opening 7 is located, which location permits to take in water under higher pressure and thus to enhance the operating efficiency of water jets (6).

Claims (4)

1. A hydroplane having a hull with a deadrise bottom and aft extendable interceptors and provided with a propulsive device mounted at the aft end of the hydroplane, characterized in hat the propulsive device is of water-jet type and in that its water intake opening is arranged in the bottom of the hull forward of the interceptors.
2. The hydroplane according to Claim 1,characterized in that the hydroplane has forward interceptors; in that the hydroplane's bottom has an aft and a forward transverse planing steps and in that the interceptors are mounted behind the steps.
3. The hydroplane according to Claim 2, characterized in that the deadrise angle of the hydroplane's bottom is in the range from 6' to 12' at the forward step and from 00 to 6' at the aft step.
4. The hydroplane according to Claim 3, characterized in that the bottom surface before each step has symmetrical flat areas, the flat areas before the forward step being of triangular or trapezoidal shape.
AU50726/99A 1998-07-15 1999-07-09 Hydroplane Ceased AU753993B2 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
RU98114297/28A RU2131822C1 (en) 1998-07-15 1998-07-15 Planing vessel
RO98114297 1998-07-15
RU98113193/28A RU2131373C1 (en) 1998-07-15 1998-07-15 Planing vessel
RO98113193 1998-07-15
PCT/RU1999/000223 WO2000003914A1 (en) 1998-07-15 1999-07-09 Hydroplane

Publications (2)

Publication Number Publication Date
AU5072699A true AU5072699A (en) 2000-02-07
AU753993B2 AU753993B2 (en) 2002-10-31

Family

ID=26653965

Family Applications (1)

Application Number Title Priority Date Filing Date
AU50726/99A Ceased AU753993B2 (en) 1998-07-15 1999-07-09 Hydroplane

Country Status (5)

Country Link
EP (1) EP1104739A4 (en)
CN (1) CN1123483C (en)
AU (1) AU753993B2 (en)
EE (1) EE200100028A (en)
WO (1) WO2000003914A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102501942B (en) * 2011-11-01 2014-06-25 大连理工大学 Spoiler of ship

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU407783A1 (en) * 1971-12-28 1973-12-10 Gliding ship
GB1510105A (en) * 1974-04-17 1978-05-10 Emi Ltd Printing
GB2060505B (en) * 1979-10-11 1984-11-28 Walker H Watercraft
SU1025574A1 (en) 1982-01-25 1983-06-30 Предприятие П/Я А-1271 Gliding speedboat
SU1113301A1 (en) * 1983-01-18 1984-09-15 Предприятие П/Я А-1271 High-speed screw propeller ship
EP0290170B1 (en) * 1987-04-28 1993-12-15 Ulf Harry Stanford Vessel with improved hydrodynamic performance
SU1837520A1 (en) * 1988-10-04 1995-09-20 Е.Б. Ануфриев Ship's hull
KR970006351B1 (en) * 1991-04-01 1997-04-25 토니크로프트 가일즈 컴파니 인코퍼레이티드 Mono hull fast ship
SE502671C2 (en) * 1994-12-23 1995-12-04 Marine Technology Dev Ltd Device and method for dynamic trimming of a fast-moving, planing or semi-planing hull
RU2108258C1 (en) * 1996-03-25 1998-04-10 Центральное морское конструкторское бюро "Алмаз" High-speed vessel
RU2096240C1 (en) 1996-03-25 1997-11-20 Центральное морское конструкторское бюро "Алмаз" High-speed vessel

Also Published As

Publication number Publication date
CN1123483C (en) 2003-10-08
WO2000003914A1 (en) 2000-01-27
AU753993B2 (en) 2002-10-31
CN1316961A (en) 2001-10-10
EE200100028A (en) 2002-06-17
EP1104739A1 (en) 2001-06-06
EP1104739A4 (en) 2002-11-27

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FGA Letters patent sealed or granted (standard patent)