# US 2013/0153739 A1 · Apparatuses and systems with vertically and longitudinally offset mounting flanges > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2013/0153739 A1 - Document ID: US20130153739A1 - Status: Published application - Kind: A1 - Application number: 13/327,355 - Filed: 2011-12-15 - Published: 2013-06-20 - Earliest claimed: 2011-12-15 - Assignees: United Technologies Corporation - Inventors: Joey Wong; Constantino V. Loffredo; Fernando K. Grant - Web page: https://patentgrep.com/patent/US20130153739A1 ## CPC - B64D 27/00: Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants - B64D 27/402: {comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant} - B64D 27/406: {Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links} - F02K 3/10: by after-burners (F02K3/105 takes precedence) - F23R 3/20: incorporating fuel injection means - F23R 3/283: {Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances} - B64D 27/16: of jet type - F05D 2240/91: on a stationary structure - F05D 2250/312: the axes being parallel to each other - F05D 2260/30: Retaining components in desired mutual position - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT - F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00) - F23R: GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS (fluidised bed combustion apparatus specially adapted for operation at superatmospheric pressures F23C10/16) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract A flanged apparatus includes an apparatus body and a flanged mount, which includes a support pylon, a first mounting flange and a second mounting flange. The support pylon includes a first pylon segment, a second pylon segment and a routing notch. The first pylon segment is cantilevered from the apparatus body, and extends to the first mounting flange. The second pylon segment is cantilevered from the first pylon support, and extends from the first mounting flange to the second mounting flange. The routing notch extends vertically between the first pylon segment and the second pylon segment. The first mounting flange and the second mounting flange extend laterally from the support pylon, and the first mounting flange is separated from the second mounting flange by a longitudinal distance and a vertical distance. ## Claims ### Claim 1 A flanged apparatus, comprising: an apparatus body; and a flanged mount comprising a support pylon, a first mounting flange and a second mounting flange, the support pylon comprising a first pylon segment that is cantilevered from the apparatus body, and that extends to the first mounting flange; a second pylon segment that is cantilevered from the first pylon support, and that extends from the first mounting flange to the second mounting flange; and a routing notch that extends vertically between the first pylon segment and the second pylon segment; wherein the first mounting flange and the second mounting flange extend laterally from the support pylon, and the first mounting flange is separated from the second mounting flange by a longitudinal distance and a vertical distance. ### Claim 2 (depends on 1) The flanged apparatus of claim 1, further comprising a second routing notch that extends vertically between the apparatus body and the first pylon segment. ### Claim 3 (depends on 2) The flanged apparatus of claim 2, wherein the flanged mount extends vertically between the apparatus body and a distal mount end, and longitudinally between a first mount side and a second mount side; and the second pylon comprises an outside surface that slopes from the first mount side to the distal mount end. ### Claim 4 (depends on 2) The flanged apparatus of claim 2, wherein the routing notch extends vertically between the apparatus body and the second pylon segment. ### Claim 5 (depends on 1) The flanged apparatus of claim 1, wherein the first pylon segment and the second pylon segment provide the support pylon with a hook-shaped geometry. ### Claim 6 (depends on 1) The flanged apparatus of claim 1, further comprising a second support pylon comprising a first pylon segment that is cantilevered from the apparatus body, and that extends to the first mounting flange; a second pylon segment that is cantilevered from the first pylon segment of the second support pylon, and that extends from the first mounting flange to the second mounting flange; and a second routing notch that extends vertically between the first pylon segment of the second support pylon and the second pylon segment of the second support pylon; wherein the first mounting flange and the second mounting flange extend laterally between the support pylon and the second support pylon. ### Claim 7 (depends on 6) The flanged apparatus of claim 6, wherein a channel extends vertically through the flanged mount, longitudinally between the first mounting flange and the second mounting flange and laterally between the support pylon and the second support pylon, and into the apparatus body. ### Claim 8 (depends on 7) The flanged apparatus of claim 7, wherein the flanged mount further comprises a first sidewall that extends vertically from the apparatus body to the first mounting flange and laterally between the support pylon and the second support pylon; and a second sidewall that extends laterally between the support pylon and the second support pylon; wherein the channel extends longitudinally between the first sidewall and the second sidewall. ### Claim 9 (depends on 1) The flanged apparatus of claim 1, wherein the apparatus body comprises a trailing edge box for a gas turbine engine augmentor. ### Claim 10 A flanged assembly, comprising: a first apparatus comprising an aperture extending vertically therethrough, the aperture comprising a first longitudinal length; and a flanged second apparatus comprising a flanged mount that mates with the aperture and extends vertically from an apparatus body, the flanged mount comprising a second longitudinal length, a support pylon, a first mounting flange and a second mounting flange, the support pylon comprising a first pylon segment that is cantilevered from the apparatus body, and that extends through the aperture to the first mounting flange; a second pylon segment that is cantilevered from the first pylon support, and that extends from the first mounting flange to the second mounting flange; and a routing notch that extends vertically between the first pylon segment and the second pylon segment; wherein the first mounting flange and the second mounting flange extend laterally from the support pylon, and the first mounting flange is separated from the second mounting flange by a longitudinal distance and a vertical distance; and wherein the second longitudinal length extends from respective outside ends of the first mounting flange and the second mounting flange, and is greater than the first longitudinal length. ### Claim 11 (depends on 10) The flanged assembly of claim 10, wherein the apparatus body comprises a third longitudinal length that is greater than the first longitudinal length. ### Claim 12 (depends on 10) The flanged assembly of claim 10, further comprising a second routing notch that extends vertically between the apparatus body and the first pylon segment. ### Claim 13 (depends on 12) The flanged assembly of claim 12, wherein the flanged mount extends vertically between the apparatus body and a distal mount end, and longitudinally between a first mount side and a second mount side; and the second pylon comprises an outside surface that slopes from the first mount side to the distal mount end. ### Claim 14 (depends on 12) The flanged assembly of claim 12, wherein the routing notch extends vertically between the apparatus body and the second pylon segment. ### Claim 15 (depends on 10) The flanged assembly of claim 10, further comprising a second support pylon comprising a first pylon segment that is cantilevered from the apparatus body, and that extends to the first mounting flange; a second pylon segment that is cantilevered from the first pylon segment of the second support pylon, and that extends from the first mounting flange to the second mounting flange; and a second routing notch that extends vertically between the first pylon segment of the second support pylon and the second pylon segment of the second support pylon; wherein the first mounting flange and the second mounting flange extend laterally between the support pylon and the second support pylon. ### Claim 16 (depends on 15) The flanged assembly of claim 15, wherein a channel extends vertically through the flanged mount, longitudinally between the first mounting flange and the second mounting flange and laterally between the support pylon and the second support pylon, and into the apparatus body. ### Claim 17 (depends on 16) The flanged assembly of claim 16, wherein the flanged mount further comprises a first sidewall that extends vertically from the apparatus body to the first mounting flange and laterally between the support pylon and the second support pylon; and a second sidewall that extends laterally between the support pylon and the second support pylon; wherein the channel extends longitudinally between the first sidewall and the second sidewall. ### Claim 18 (depends on 10) The flanged assembly of claim 10, wherein the first pylon segment and the second pylon segment provide the support pylon with a hook-shaped geometry. ### Claim 19 (depends on 10) The flanged assembly of claim 10, wherein the apparatus body comprises a trailing edge box for a gas turbine engine augmentor. ### Claim 20 (depends on 19) The flanged assembly of claim 19, wherein the first apparatus comprises a circumferentially extending augmentor duct case.