Dual induction jet DIJ
Patent Information
- Application Number
- GB2023013650
- Authority / Receiving Office
- GB · GB
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2023-09-07
- Publication Date
- 2025-03-12
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Abstract
Description
• Description of a DU - means Dual Induction Jet • Fig 1 - shows Cylindrical Body 1A • A DU shares the shape Gas Turbine • A DU body 1A has scoops 2A to catch airflow into ducts 2 • Intake Ducts 2 have safety guards 2A
Claims
1. Air drawn into body 1A-9 by blades 1-4, build pressure against^, thrust - Plate 6.
2. A vortex is caused and forced through Jet 10 in thrust - Plate6. (Claim 1)3. Air passing out of Jet 10 (Claim 2) and through blades 2-4, causes the vortex to draw in air through ducts 2 in its wake.
4. The Vortex of air is forced in the narrowing body 1A by blades 2-4, to be collected by blades 3-4 and forced out of body 8, has clean cool air.
5. An accurate shutter thrust test of identical size and RPM of a model gas-turbine and DU. The latter recorded 108.5% more thrust.Application No: GB2313650.0Examiner: Mr Ilya GribanovClaims searched: 1-5Date of search: 14 March 2024Patents Act 1977: Search Report under Section 17Documents considered to be relevant:Category Relevant to claims Identity of document and passage or figure of particular relevance A - US 5463866 A (BOEING) - see the figures A - US 7216475 B2 (GEN ELECTRIC) - see the figures A - CN 102678333 A (UNIV HARBIN) - see the figuresCategories:X Document indicating lack of novelty or inventive step A Document indicating technological background and / or state of the art. Y Document indicating lack of inventive step if P Document published on or after the declared priority date but combined with one or more other documents of same category. before the filing date of this invention. & Member of the same patent family E Patent document published on or after, but with priority date earlier than, the filing date of this application.Field of Search:International Classification:Subclass Subgroup Valid From B64D 0027 / 30 01 / 01 / 2024 B64D 0035 / 00 01 / 01 / 2006 F02C 0007 / 055 01 / 01 / 2006 F02K 0001 / 38 01 / 01 / 2006 F02K 0001 / 46 01 / 01 / 2006 F02K 0003 / 04 01 / 01 / 2006 F02K 0003 / 065 01 / 01 / 2006
Citation Information
Patent Citations
Imported protective net cover
CN102678333A
Supersonic jet engine installation and method with sound suppressing nozzle
US5463866A
Aft FLADE engine
US7216475B2